Piper Aircraft Corporation Malibu Mirage PA-46-350P Airplane Maintenance Manual Download Page 654

Page: 654 / 1956

PAGE 4
Feb 28/07

3H14

29-10-00

PIPER AIRCRAFT, INC.

PA-46-350P, MALIBU MIRAGE

MAINTENANCE MANUAL

(7)

Remove small O-rings under filters and large O-ring on upper manifold.

(8)

Remove pressure relief valves from upper manifold.

NOTE: Follow steps (9) thru (13) as needed to remove pressure switches and manifolds.

(9)

Remove pressure switches. Discard O-rings.

(10) Remove elbow and restrictor fitting by loosening nut(s), unscrewing elbow(s) from lower

manifold, and discarding O-ring(s).

NOTE: Upper and lower manifolds must be replaced as a set in pump serial numbers 156 and

up. These can be distinguished by gold color instead of gray in earlier models. Refer to
PA-46-350P Parts Catalog.

(11) Remove and discard large O-ring from upper manifold if not already performed in step (10).

Hydraulic Pump (Parker Hannifin)

Figure 3

Effectivity
4636001 thru 4636313

Summary of Contents for Malibu Mirage PA-46-350P

Page 1: ...PART NUMBER 761 876 February 28 2007 1A1 AIRPLANE MAINTENANCE MANUAL CARD 1 OF 9 PA 46 350P S N s 4636001 AND UP PIPER AIRCRAFT INC ...

Page 2: ...1A2 Published by Technical Publications Piper Aircraft Inc 2926 Piper Drive Vero Beach Florida 32960 U S A Member General Aviation Manufacturers Association ...

Page 3: ...2 3 4 5 and 6 CR981223 December 23 1998 1 2 3 4 5 and 6 PR000201 February 1 2000 1 2 3 4 5 and 6 PR010515 May 15 2001 1 CR050730 July 30 2005 1 2 3 4 5 6 7 and 8 PR060207 February 7 2006 1 2 3 4 5 6 7 and 8 CR070228 February 28 2007 1 2 3 4 5 6 7 8 and 9 COMPLETE REVISION OF MAINTENANCE MANUAL 761 876 Revisions appear in all Aerofiche Cards Accordingly discard your entire existing Aerofiche Card S...

Page 4: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 1 Feb 28 07 AEROFICHE EFFECTIVITY 1A4 THIS PAGE INTENTIONALLY BLANK ...

Page 5: ...Feb 28 07 Intro Table of Contents 1 Feb 28 07 2 Feb 28 07 Introduction 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 Index 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHA...

Page 6: ...PAGE 2 Feb 28 07 INTRO LIST OF EFFECTIVE PAGES 1A6 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 7: ...A9 Effectivity 2 1A10 Serial Number Explanation 2 1A10 Assignment of Subject Material 2 1A10 Pagination 3 1A11 Aerofiche Effectivity 3 1A11 Identifying Revised Material 3 1A11 Indexing 3 1A11 List of Effective Pages 3 1A11 Warnings Cautions and Notes 3 1A11 Accident Incident Reporting 4 1A12 Supplementary Publications 4 1A12 Piper Publications 4 1A12 Vendor Publications 4 1A12 Chapter Section Inde...

Page 8: ...PAGE 2 Feb 28 07 1A8 INTRO CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 9: ...GENUINE PIPER AIRCRAFT PARTS OR PIPER AIRCRAFT APPROVED PARTS OBTAINED FROM PIPER APPROVED SOURCES IN CONNECTION WITH THE MAINTENANCE AND REPAIR OF PIPER AIRPLANES Genuine PIPER parts are produced and inspected under rigorous procedures to ensure airworthiness and suitability for use in PIPER airplane applications Parts purchased from sources other than PIPER even though identical in appearance ma...

Page 10: ...ane are broken down into subsystems These sub systems are identified by the second element of the standard numbering system The element 40 of the number 28 40 01 concerns itself with the indicating section of the fuel system C Unit Subject The individual units within a sub system section may be identified by the third element of the standard numbering system The element 01 of the number 28 40 01 i...

Page 11: ...his set 8 Identifying Revised Material A revision to a page is defined as any change to the printed matter that existed previously Revisions additions and deletions are identified by a vertical line i e change bar along the left hand margin of the page opposite only that portion of the printed matter that was changed A change bar in the left hand margin opposite the footer i e chapter section subj...

Page 12: ...s Catalog P N 761 878 2 Periodic Inspection Report Form P N 767 011 3 Progressive Inspection Manual 50 hour P N 767 013 B Vendor Publications WARNING FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION S WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT MAY RENDER THE AIRCRAFT UNAIRWORTHY 1 AIR CONDITIONING COMPRESSOR Vendor Address Sanden International USA Inc PH 972 442 8400...

Page 13: ...cialty Systems PH 330 374 3040 Goodrich Corporation FAX 330 374 2290 1555 Corporate Woods Parkway Uniontown Ohio 44685 8799 Technical Assistance PH 800 334 2377 330 374 3743 FAX 330 374 2290 Email dssd support goodrich com http www deicingsystems goodrich com Black Standard Pneumatic De Icer Installation Maintenance and Repair Manual ATA 30 10 31 SmartBoot System ATA 30 10 65 8 ELECTRONIC FLIGHT I...

Page 14: ...ntext See www avantext com or PH 800 998 8857 11 FIRE EXTINGUISHER PORTABLE Vendor Address H3R Inc PH 800 249 4289 43 Magnolia Ave 4 San Francisco California 94123 2911 http www h3r com index htm 12 FORCE APPLICATOR KIT Vendor Address Safe Flight Instrument Corp PH 914 946 9500 20 New King Street White Plains New York 10602 13 FUEL BOOST PUMP Vendor Address Parker Hannifin Corp PH 800 272 7537 Nic...

Page 15: ...ww unisonindustries com index4 html Installation Operation F1100 MASTER SERVICE MANUAL and Maintenance 4300 6300 SERIES MAGNETO MAINTENANCE AND Instructions OVERHAUL MANUAL L 1363 19 NAVIGATION COMMUNICATIONS AND GPS NAV COM GPS Vendor Address Garmin International PH 913 397 8200 1200 East 151ST Street Olathe KS 66062 http www garmin com 20 OXYGEN SYSTEM Vendor Address Scott Aviation PH 716 683 51...

Page 16: ...DAR WEATHER RDR 2000 Vendor Address Honeywell Bendix King See Autoflight above Maintenance Manual Bendix King ART 2000 P N 006 05332 0001 25 RADIO COOLING BLOWER Vendor Address Globe Motors PH 937 228 3171 2275 Stanley Ave FAX 937 229 8531 Dayton Ohio 45404 http www globe motors com home html 26 STARTER Vendor Address Kelly Aerospace See Alternator above or Sky Tec Partners Ltd PH 800 476 7896 350...

Page 17: ...MALIBU MIRAGE MAINTENANCE MANUAL 28 VACUUM PUMP Vendor Address Aero Accessories Inc PH 800 822 3200 1240 Springwood Avenue Gibsonville NC 27249 http www aeroaccessories com index html 29 VACUUM REGULATORS Vendor Address Parker Hannifin Corp see Fuel Boost Pump above ...

Page 18: ...PAGE 10 Feb 28 07 INTRODUCTION 1A18 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 19: ...chapter CHAPTER SECTION TITLE GRID NO 4 AIRWORTHINESS LIMITATIONS 1C1 00 Airworthiness Limitations 5 TIME LIMITS MAINTENANCE CHECKS 1C9 00 General 10 Time Limits 20 Scheduled Maintenance Checks 30 Special Inspections 50 Unscheduled Maintenance Checks 6 DIMENSIONS AND AREAS 1E13 00 General 7 LIFTING AND SHORING 1F1 10 Jacking 8 LEVELING AND WEIGHING 1F9 10 Weighing and Balancing 20 Leveling 9 TOWIN...

Page 20: ...emperature Control 22 AUTOFLIGHT 2F11 10 Autopilot 23 COMMUNICATIONS 2G19 00 General 50 Audio Integrating 60 Static Discharging 24 ELECTRICAL POWER 2H11 00 General 30 DC Generation 40 External Power 60 Electrical Load Distribution 25 EQUIPMENT FURNISHINGS 2J11 10 Flight Compartment 20 Passenger Compartment 50 Cargo Compartments 60 Emergency 26 FIRE PROTECTION 2K15 20 Extinguishing 27 FLIGHT CONTRO...

Page 21: ...rs 60 Propellers Rotors 31 INDICATING RECORDING SYSTEMS 4C1 50 Central Warning Systems 32 LANDING GEAR 4C13 00 General 10 Main Gear and Doors 20 Nose Gear and Doors 30 Extension and Retraction 40 Wheels and Brakes 50 Steering 60 Position and Warning 33 LIGHTS 4G5 10 Flight Compartment 20 Passenger Compartment 30 Cargo and Service Compartments 40 Exterior 34 NAVIGATION 5C1 00 General 10 Flight Envi...

Page 22: ...00 General 10 Investigation Cleanup and Aerodynamic Smoothness 70 Repairs 80 Electrical Bonding 52 DOORS 6G13 10 Passenger Crew 20 Emergency Exit 30 Cargo 70 Monitoring and Operation 55 STABILIZERS 6H13 00 General 10 Horizontal Stabilizers 20 Elevator 30 Vertical Stabilizer 40 Rudder 56 WINDOWS 6I19 00 General 10 Flight Compartment 20 Cabin 30 Door 57 WINGS 6K5 40 Attach Fittings 50 Flight Surface...

Page 23: ... Power Supply 20 Distribution 76 ENGINE CONTROLS 7G17 10 Power Control 77 ENGINE INDICATING 7H3 10 Power 20 Temperature 40 Integrated Engine Instrument Systems 79 OIL 7J3 20 Distribution 30 Indicating 80 STARTING 7J15 10 Cranking 81 TURBINES 7K9 20 Turbo Supercharger 91 CHARTS WIRING DIAGRAMS 8C1 10 Charts 21 and up Electrical Schematics 91 CONT CHARTS WIRING DIAGRAMS CONT 9C1 Electrical Schematic...

Page 24: ...PAGE 16 Feb 28 07 INTRODUCTION 1A24 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 25: ...sion Control Wing 6L3 Attitude Indicator 5D5 Autopilot 2F17 Component Locator 2G2 Installation 2F18 2F20 Maintenance 2F23 Operational Checkout 2F24 Pitch Servo 2G12 Pressure Transducer 2G6 Roll Servo 2G4 Servo Clutch Torque Adjustment 2G15 Trim Monitor 2G3 Trim Servo 2G6 Yaw Amplifier 2G14 Yaw Servo 2G10 Avionics Cooling 2C14 Avionics Master Switch 2H1 B Ball Diameters for Testing Hose Restriction...

Page 26: ...rrection 2I10 Troubleshooting 2I7 2I13 Valve Regulated Lead Acid 2I13 Bonding 6G9 Resistance Index 6G10 Buses Avionics 2H19 Main 2H19 Circuit Breaker Panel 6D22 Electrical Shelf 6E7 External Power 2I19 Load Distribution 2J1 Relay Installation Co Pilot s Side 6E10 K1 thru K8 6E10 Pilot s Side 6E9 Schematics Air Conditioning 8E7 Airspeed Standby 9E19 Altimeter Radar 9F14 Altimeter Standby 9E19 Annun...

Page 27: ...n Light 9E5 WX 500 9F11 XM Receiver 8E23 Switch Panels 6E1 Symbols 8D14 System 2H17 Troubleshooting 2H20 Tie Bus Panel Connections 6E3 Volt Ammeter 2J4 Voltage Regulation and Control 2H19 Wire Coding 8D13 Elevator Balancing 6I3 Control System Installation 3D23 Rigging and Adjustment 3D24 Troubleshooting 3D19 Torque Tube Bearing Changes 3D20 Trim Controls Actuator Assembly 3E3 Corrosion Control 3E4...

Page 28: ...Drain Valve 3G8 Draining 1I19 Draining Moisture 1I18 Fuel Filter 3G7 Fuel Pumps Specifications 3G5 Fuel Quantity Gauge Accuracy Test 3G14 Full Range Check 3G20 Senders 3G13 Leak Test Setup 3G1 Selector Switch and Valve 3G6 Cable Adjustment 3G7 Troubleshooting 3F16 Leak Evaluation 3F22 G GMA 340 Audio Panel Adjustments 2H6 Installation 2H3 System Functional Test 2H4 GNS 430 5F5 GNS 530 5F5 Ground C...

Page 29: ... 4D11 Position and Warning 4F19 Landing Gear Up Power Reduced Warning Switch Adjustment 4G2 Troubleshooting 4F20 Leading Particulars and Principal Dimensions 1E20 Leveling 1F17 Life Limited Parts 1C7 Lifting 1F7 See also 57 40 00 Lights Exterior 4H3 Landing 4H7 Position 4H4 Pulse 4H7 Strobe 4H3 Taxi 4H6 Wing Inspection Light 4H7 Interior 4G11 Annunciator Panel 4G12 Baggage Area 4G21 Forward 4H1 Re...

Page 30: ...g 3K6 Troubleshooting 3J20 Propeller Assembly 7C9 Publications Piper A12 Vendor A12 Q Quad Digital Indicator QDI See Engine Instruments Transicoil EMIS R Radar 5F1 Repairs Fiberglass 6F19 Metal Wire Stitching 6G5 Thermoplastic 6F21 List of Materials 6F24 Window Windshield Acrylic 6J10 Restraint System 2J23 Inertial Reel Adjustment 2J23 Inspection 2J23 Revised Material A11 Robinair 34700 Charging S...

Page 31: ... Bellcrank Centering 4C22 Horn Arm Gap 4C22 Nose Wheel Centering 3C15 4C22 Rudder Pedal Neutral Alignment 3C15 4C22 Rudder Travel Tool 3C15 Torque Conversion 8C20 Torque Wrench Formula 1K2 Towing 1G5 Transponder 5F9 GTX 327 5F9 GTX 330 5F9 Post Installation Setup Procedure 5F10 ARINC 429 Configuration Page 5F11 Display Mode and Key Lighting 5F11 Hexadecimal Conversion 5F13 Operation Configuration ...

Page 32: ...in 6I11 Vertical Speed Indicator 5C18 Volt Ammeter See Electrical W Warnings Cautions and Notes A11 Weather Radar 5F1 Weighing 1F15 Wheel Brake Assembly 4F4 Wheels Bearing Cup 4F4 Main Wheel Assembly 4F2 Nose Wheel Assembly 4F1 Repairs 4F3 Windows and Windshields Door Window 6K3 Heated Windshield Testing 3J15 Troubleshooting 3J15 Inspection and Repair Definitions 6J1 Limitations 6J1 Crack Limitati...

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Page 35: ...1C1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 4 AIRWORTHINESS LIMITATIONS ...

Page 36: ...1C2 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 37: ...T INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 4 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 4 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 4 Table of Contents 1 Feb 28 07 2 Feb 28 07 4 00 00 1 Feb 28 07 2 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 39: ...eb 28 07 1C5 4 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 4 AIRWORTHINESS LIMITATIONS TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO AIRWORTHINESS LIMITATIONS 4 00 00 1 1C7 ...

Page 40: ...PAGE 2 Feb 28 07 1C6 4 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 41: ... time and or cycles remaining on them as well as the disposition of life limited parts with no time and or cycles left Life limited parts defined by Type Certificate TC are listed in paragraph 1 above Other parts which are replaced or rebuilt at specific intervals are listed in Chapter 5 A Parts that are removed prior to accumulating their life limit are to be marked with indelible ink or marker w...

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Page 43: ...1C9 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 5 TIME LIMITS MAINTENANCE CHECKS ...

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Page 45: ... 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 19 Feb 28 07 20 Feb 28 07 21 Feb 28 07 22 Feb 28 07 5 30 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHAPT...

Page 46: ...PAGE 2 Feb 28 07 5 LIST OF EFFECTIVE PAGES 1C12 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 47: ...pit Group 10 1D4 Fuselage and Empennage Group 12 1D6 Landing Gear Group 14 1D8 Wing Group 15 1D9 Special Inspection 16 1D10 Operational Inspection 17 1D11 General 17 1D11 Notes 18 1D12 SPECIAL INSPECTIONS 5 30 00 1 1D17 Per Flight Hour 1 1D17 Per Calendar Year 4 1D20 Per Specific Operation Operating Environment 6 1D22 Operation in High Dust or Industrial Pollution Environment 6 1D22 Operation in H...

Page 48: ...PAGE 2 Feb 28 07 1C14 5 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 49: ...egistration then the registered owner s is responsible for forwarding these Bulletins and Letters to the operating location s or person s Changes in aircraft registration may take a substantial amount of time to be recorded by the Federal Aviation Administration and received by Piper to change the mailing address Owners and operators should make arrangements to keep abreast of service releases dur...

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Page 51: ...nd related structural inspection procedure required for type certification 2 Refer to 5 20 00 for Piper s recommended Inspection Program It includes the frequency and extent of the inspections required for the continued airworthiness of the airplane 3 Inspections required by Flight Hour or Calendar Year if due are included as part of the Annual 100 Hour Inspection and or the Progressive Inspection...

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Page 53: ...he time periods given for inspections of various components are based on average usage and environmental conditions NOTE The listed inspection overhaul and replacement schedules do not guarantee that a particular item or component will reach the listed time without malfunction Unique operating conditions encountered by individual airplanes cannot be controlled by the manufacturer 2 Definitions A I...

Page 54: ... an operational test of the component and its related system should be performed to ensure proper function Serviceable parts that were issued to the component will be filed in the aircraft permanent records The person performing the test must make appropriate entries in the aircraft s permanent maintenance record F Maintenance The word maintenance as defined by FAR Part 1 means inspection overhaul...

Page 55: ...chedule This schedule will be published in a separate manual form which when available may be ordered from Piper Distributors under P N 767 013 Refer to Piper Customer Service Info Aerofiche revision checklist for availability and to ensure obtaining latest issue NOTE The PA 46 350P Malibu Mirage 50 Hour Progressive Inspection Manual P N 767 013 referenced above will not be a stand alone document ...

Page 56: ...umns or listed as a special inspection in 5 30 00 or both 2 Refer to the applicable chapter of this manual for instructions on how to gain access to remove any item that must be removed and is not completely accessible 3 Inspection Report Forms To help in the performance of periodic inspections Inspection Report forms are available through Piper Dealers as P N 767 011 NOTE Service centers conducti...

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Page 58: ...PAGE 6 Feb 28 07 1C24 5 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 59: ...ess in hub pilot tube O 8 Check condition of propeller deicer system if installed O 9 If installed inspect propeller deice slip rings brush block and brush length replace as required O 10 Lubricate propeller See appropriate Hartzell Owner s Manual and Lubrication Chart 12 20 00 O 11 Install spinner O B ENGINE GROUP WARNING GROUND MAGNETO PRIMARY CIRCUIT BEFORE WORKING ON ENGINE NOTE Read Note 5 50...

Page 60: ...d cleanliness O 19 Check magneto main points for clearance See 74 10 00 Magnetos 100 Hour Inspection O 20 Inspect magnetos for oil leaks O 21 Check magneto to engine timing See Note 6 O O 22 Inspect security of injector nozzle and sense line See Note 9 O NOTE Clean injector nozzles as required Clean with acetone only 23 Remove air filter and clean per 12 10 00 replace as required See Note 28 O O 2...

Page 61: ...gine shock isolator mounts for deterioration Replace as required O 43 Inspect firewall for cracks condition and security O 44 Check condition of firewall sealing O 45 Inspect alternator s for cracks condition and security O 46 Inspect condition and tension of alternator drive belts Refer to 24 30 00 O 47 Inspect starter for cracks condition and security See Note 43 O 48 Check air conditioning syst...

Page 62: ...r worn or damaged areas loose clamps cracks and leaks See Note 45 O O 12 Inspect intercooler clips for condition and security See 81 20 00 Intercooler Attachment Clips Inspection Replacement O O 13 Inspect turbo and controller system oil lines for leaks and security O O 14 Inspect for oil leakage from controller and sense lines O O 15 Install engine cowling O O D CABIN AND COCKPIT GROUP 1 Remove i...

Page 63: ...ion of safety wire on screw attaching valve cam O 20 Check operation of cabin heat and defrost controls O 21 Inspect all knobs switches and levers for security of attachment and condition O 22 Check condition of environmental system ducts O WARNING BE SURE SKIN AND CLOTHING ARE FREE OF GREASE OIL OR OTHER PETROLEUM PRODUCTS BEFORE CHECKING OR PERFORMING MAINTENANCE ON ANY COMPONENT OF THE OXYGEN S...

Page 64: ... misrigging or structural imbalance and attachment points for missing or worn hardware O CAUTION PRESSURIZED FLIGHT IS PROHIBITED WITH DISCOLORATION CRACKS OR CRAZING 3 Inspect windshield and windows for nicks scratches cracks crazing and discoloration O 4 Inspect avionics compartment components and wiring for condition security and operation O 5 Inspect control cable boots for condition and secur...

Page 65: ...e Notes 13 and 21 O 25 Check fuel filter Clean or replace as required O O 26 Inspect deice system pneumatic valves and lines for condition and security if installed O 27 Check baggage compartment door latches and hinge for operation condition and security O 28 Check baggage compartment upholstery for condition O 29 Check baggage compartment light and switch for operation condition and security O 3...

Page 66: ...0 O O CAUTION WHEN AIRCRAFT HAS OPTIONAL RADAR POD INSTALLED ON RIGHT WING ENSURE THAT JACK DOES NOT COME INTO CONTACT WITH RADAR POD 2 Place airplane on jacks Refer to 7 10 00 O 3 Remove inspection covers and panels O 4 Inspect nose gear steering control and travel O 5 Inspect nose gear installation for condition and security See Notes 27 35 and 36 O 6 Inspect nose gear trunnion for cracks and co...

Page 67: ...s for leakage and security See Note 23 O 31 Perform gear retraction and extension operation check Per Landing Gear Retraction System Functional Test 32 30 00 O 32 Place weight of aircraft on landing gear DO NOT REMOVE JACKS O 33 Check anti retraction system on gear lever for proper operation O 34 Install inspection covers and panels O O WARNING DO NOT REMOVE JACKS UNTIL IT HAS BEEN DETERMINED THAT...

Page 68: ... ERRONEOUS STALL WARNINGS NECESSITATING CALIBRATION OF SYSTEM SEE CHAPTER 27 10 Inspect lift transducer for security of attachment spring centering of switch blade and corrosion Check heat element for operation O 11 Inspect wing inspection light for broken lens security wiring and attachment if installed O 12 Lubricate per Lubrication Chart 12 20 00 O 13 Check condition of hydraulic fuel and pneum...

Page 69: ... O 15 Check magneto switch operation O O 16 Check magneto RPM variation O O 17 Check throttle and mixture operation O O 18 Check propeller smoothness O O 19 Check constant speed propeller action O O 20 Check engine idle O O 21 Check alternate air O O 22 Check air conditioning compressor clutch operation O O 23 Check cabin pressure controller See Operational Inspection Cabin Pressure Controller 21 ...

Page 70: ...etion of any inspections 3 Piper Service Bulletins are of special importance and Piper considers compliance mandatory In all cases see Service Bulletin Service Letter Index P N 762 332 or Service Bulletin Service Letter Aerofiche Set P N 1762 331 to verify latest revision 4 Piper Service Letters are product improvements and service hints pertaining to servicing the airplane and should be given car...

Page 71: ...etin No 1017 19 In S N s 4636021 thru 4636190 only verify compliance with Piper Service Letter No 1023 20 In S N s 4636001 thru 4636198 only verify compliance with Piper Service Bulletin No 1029 and Lycoming Service Bulletin No 534 21 In S N s 4636001 thru 4636215 only verify compliance with Piper Service Bulletin No 1034 22 In S N s 4636001 thru 4636221 only in airplanes which have not installed ...

Page 72: ...perform V Band Coupling 100 Hour Inspection 81 20 00 46 In S N s 4636350 thru 4636351 only verify compliance with Piper Service Bulletin No 1151E 47 In S N s 4636362 and up for airplanes delivered from the factory in bare metal verify compliance with Piper Service Letter No 1089 48 In S N s 4636001 thru 4636368 only verify compliance with Piper Service Letter No 1097 49 In S N s 4636001 thru 46363...

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Page 75: ... Pilot s Copilot s Window in 56 10 00 Each 250 Hours Replace Turbine Inlet Temperature TIT probe See TIT Gauge Probe Replacement 77 20 00 and FAA Airworthiness Directive AD 99 15 04 Comply with the latest revisions of Textron Lycoming Service Bulletins No 521 and 531 Each 400 Hours Inspect Airborne pressure manifold every 400 hours See Pressure Manifold Check Valve Testing 30 10 00 For airplanes e...

Page 76: ...500 Hour Inspection and Cleaning Replace engine air filter Coin tap erosion shield on composite blades See latest revision Hartzell Composite Blade Manual No 135 Each 1000 Hours Replace engine compartment flexible hoses fuel oil etc as required but not to exceed 1000 hours time in service eight 8 years or engine overhaul whichever comes first Coin tap the entire blade on composite blades See lates...

Page 77: ...ervice Letter No 61 whichever comes first overhaul or replace the propeller governor Overhaul or replace Hartzell propellers each five or six years or each 2000 or 2400 hours Refer to latest revision of Hartzell Service Letter No 61 to determine specific requirements for individual airplanes At engine overhaul or each 2000 hours whichever comes first overhaul or replace alternators Each 2400 Hours...

Page 78: ...reafter the battery should be removed and capacity tested per Battery Capacity Test 24 30 00 Each Twelve 12 Months Lubricate Hartzell propeller every 100 Hours or annually whichever comes first If annual usage is significantly less than 100 Hours lubricate propeller each six 6 months See Hartzell Standard Practices Manual No 202A If installed each twelve 12 calendar months conduct SpeedBrake Annua...

Page 79: ...ividual airplanes Each Seven 7 Years Each 2000 hours or seven 7 years whichever occurs first remove interior panels and headliner and conduct detailed inspection of aircraft structure skin bulkheads stringers etc for condition and security Inspection of structure concealed by headliner may be accomplished by alternate means i e through the use of a borescope without removing the headliner providin...

Page 80: ...on Interval Engine Air Filter Clean and inspect Daily Cabin Environmental and Inspect and replace if necessary 100 Hours Instrument Air Filters Pitot Static system Check for obstruction Reverse 100 Hours or flow to lines as required Landing Gear Actuators Clean Before each flight and Oleos Inspect 100 Hours Landing Gear Wheel Clean inspect and repack 50 Hours Bearings Windows Inspect for cracks er...

Page 81: ...KICK BACK Engines with more than Each five days pull prop through five Each 5 days 50 hours total time complete revolutions and Each 30 days fly aircraft for 30 minutes each 30 days or ground run until oil temperature is in the green arc Avoid excessive ground run Engines with less than Each day pull prop through five Daily 50 hours total time complete revolutions and Each 30 days fly aircraft for...

Page 82: ...Terrain Item Inspection Inspection Interval Landing Gear Inspect for cracks attachment 100 Hours damage cleanliness and lubrication Wheels Inspect for cracks damage chipped 100 Hours rims bearings for damage corrosion and lubrication Tires Inspect for cuts wear inflation and Daily deterioration Wheel Wells Inspect for foreign material damage 100 Hours and corrosion Brakes Inspect for damage foreig...

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Page 85: ...e only before further flight Engine See latest revisions of appropriate Each occurrence Textron Lycoming Service Bulletins before further flight and Overhaul Manual Electrical and Avionics Inspect and check harness connections Each occurrence Systems and equipment for high voltage damage before further flight burns and insulation degradation Replace or overhaul as required Consult with appropriate...

Page 86: ...Manual procedures If there are any questions regarding repairs or procedures contact your Piper Distributor s Service Advisor DSA D Inspect the following items closely to determine the extent of damage Item Inspection Inspection Interval Landing Gear Struts Cracks signs of overstress Each occurrence Not required for deformation loose or damaged before further flight severe turbulence trunnion moun...

Page 87: ...struments and accessories installation for security and operation Perform ground pressurization check See 21 30 00 Pressurization System Test Empennage Skins for buckling wrinkles loose or Each occurrence missing rivets Elevator rudder vertical before further flight fins and horizontal stabilizer for security of attachment and overstress of bolts Ribs stringers for buckling cracks and damage Wheel...

Page 88: ...light Tubular Structures Check for internal corrosion If immersed each event i e Engine Mounts etc Clean and represerve as required before further flight See 71 20 00 Engine Mount Corrosion Inspection Immersion in Water Wings Inspect to ensure that contaminants If immersed each event are cleaned from fuel cell areas before further flight Landing Gear and associated Check all limit switches replace...

Page 89: ...nce with manufacturer s instructions to determine fitness for future use Reassemble engine using new seals gaskets stressed bolts nuts and crankshaft sludge tubes All reused parts must conform with Lycoming Table of Limits No SSP 2070 for fits and clearances See latest revision of Lycoming Service Bulletin No 357 Engine Accessories Inspect Aircraft systems that supply If immersed each event either...

Page 90: ...ropriate maintenance manual Replace de icer timers Clean and check prop de icer brush holders Clean and check voltage regulators and overvoltage relays Replace as necessary Clean and check aIl strobe light power supplies Refer to appropriate maintenance manual Replace all fuel senders trim tab sender pots flap position senders etc Clean inspect and check heated pitot systems Inspect and check harn...

Page 91: ...ssociated before further flight lines and pumps and header tanks Clean and inspect all fuel tank vents cap vents and vent lines Instruments Clean and inspect instruments Bench If immersed each event check per appropriate maintenance before further flight manual Heating and Ventilating Replace blowers If immersed each event Systems before further flight Clean and inspect all distribution boxes duct...

Page 92: ...ect and check harness connections Each occurrence and equipment for high voltage damage before further flight burns and insulation degradation Replace or overhaul as required Consult with appropriate avionics vendor s for inspection and operational checks Bench check alternator and voltage regulator s See 24 30 00 Insulation and Upholstery Remove all wet insulation and upholstery If immersed each ...

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Page 95: ...1E13 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 6 DIMENSIONS AND AREAS ...

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Page 97: ... MIRAGE MAINTENANCE MANUAL CHAPTER 6 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 6 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 6 Table of Contents 1 Feb 28 07 2 Feb 28 07 6 00 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 99: ...6 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 6 DIMENSIONS AND AREAS TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO GENERAL 6 00 00 1 1E19 Leading Particulars and Principal Dimensions 2 1E20 Station References 4 1E22 Access and Inspection Provisions 5 1E23 ...

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Page 101: ... Association MAA plate which is located below the tailcone at approximately F S 311 50 The engine serial number plate is located on the right side of the engine between cylinders 1 and 3 Three View PA 46 350P Figure 1 14 5 4 42 m 7 43 2 28 m 11 59 3 53 m 43 0 13 11 m 4 58 1 38 m 80 0 DIA 2 03 m 4 42 1 35 m 12 3 3 7 m 6 17 1 88 m 4 5 Dihedral 28 9 8 81 m 11 3 3 4 m 5 17 1 57 m 2 25 68 m Static Grou...

Page 102: ...ty 12 0 quarts Fuel Specification 100 or 100LL Aviation Grade Fuel Injection System Textron Lycoming Motors Magnetos Pressurized Slick Left 6363 Right 6360 Magneto Timing 20 BTC Magneto Breaker Point Clearance 008 012 Using E gap method Spark Plugs Shielded Refer to latest revision of Textron Lycoming Service Bulletin No 1042 Spark Plug Gap Setting 019 Firing Order 1 4 5 2 3 6 Starter 24 volt Kell...

Page 103: ...Angle High Pitch Low RPM 40 0 to 41 0 38 7 0 5 Governor Model Hartzell V 5 2 FUEL SYSTEM Fuel Tank Capacity Gal 61 per wing Total Fuel Onboard Gal 122 Total Usable Fuel Gal 120 Fuel Minimum Grade 100 100LL Aviation Grade LANDING GEAR Type Retractable Hydraulic Shock Strut Design Combination Air and Oil Turning Radius 35 4 ft Nose Gear Travel 30 Left and Right Wheel Nose McCauley D 30500 Cleveland ...

Page 104: ... of airplane structural members Station References Figure 2 B L 00 00 B L 6 62 B L 37 50 B L 29 00 B L 86 00 B L 80 31 B L 37 36 W S 51 54 W S 93 00 W S 107 56 W S 115 25 W S 134 00 W S 156 00 W S 182 00 W S 209 00 W S 240 00 W S 257 50 W S 258 75 F S 32 990 F S 42 00 F S 79 00 F S 100 00 F S 117 00 F S 135 90 F S 158 30 F S 164 80 F S 171 40 F S 186 30 F S 198 00 F S 226 30 F S 214 90 F S 241 50 ...

Page 105: ...aft of station 265 00 3 12 BOTTOM VIEW 2 2 1 12 3 13 TOP VIEW SIDE VIEW 10 11 9 8 7 6 5 4 14 15 16 17 1 Elevator Trim Jackscrew Elevator Up Stop Elevator Sector Rudder Sector Rudder Stops Emergency Locator Transmitter Elevator Cable Turnbuckles Condenser and Condenser Fan 2 Collector Tank Main Landing Gear Actuator Flap Bellcranks Up Limit Switch Squat Switch L H side 3 Strobe Power Supply 4 Nose ...

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Page 107: ...1F1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 7 LIFTING AND SHORING ...

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Page 109: ... MAINTENANCE MANUAL 1F3 7 LIST OF EFFECTIVE PAGES CHAPTER 7 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 7 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 7 Table of Contents 1 Feb 28 07 2 Feb 28 07 7 10 00 1 Feb 28 07 2 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 111: ... 28 07 1F5 7 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 7 LIFTING AND SHORING TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO JACKING 7 10 00 1 1F7 General 1 1F7 Jacking 1 1F7 ...

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Page 113: ...upporting 2 Jacking CAUTION DISABLE LIFT DETECTOR WINDSHIELD HEAT AND PITOT HEAT PRIOR TO JACKING AIRCRAFT CAUTION WHEN THE AIRCRAFT HAS OPTIONAL RADAR POD ON RIGHT WING ENSURE JACK DOES NOT COME IN CONTACT WITH RADAR POD A Align jacks under wing with respective pads on the wing main spar CAUTION ENOUGH SUPPORT BALLAST MUST BE ADDED TO THE TAILSTAND TO PREVENT THE AIRPLANE FROM TIPPING FORWARD ON ...

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Page 115: ...1F9 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 8 LEVELING AND WEIGHING ...

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Page 117: ...AGE MAINTENANCE MANUAL CHAPTER 8 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 8 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 8 Table of Contents 1 Feb 28 07 2 Feb 28 07 8 10 00 1 Feb 28 07 2 Feb 28 07 8 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 119: ... 28 07 1F13 8 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 8 LEVELING AND WEIGHING TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO WEIGHING 8 10 00 1 1F15 LEVELING 8 20 00 1 1F17 ...

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Page 121: ...lance computations level the airplane per instructions given in the paragraph titled Leveling E Fill engine with oil to full capacity F Place pilot and copilot seats in fifth notch aft of forward position Put flaps in the fully retracted position and all control surfaces in the neutral position Tow bar should be in the proper location and all entrance and baggage doors should be closed G Weigh the...

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Page 123: ...rposes of weighing or rigging the following procedures may be used NOTE Always level the airplane laterally first then level the airplane longitudinally A To laterally level the airplane place a level across the forward edge of the rear baggage compartment If the airplane is resting on its gear raise or lower one wing tip by deflating the main gear tire on the high side of the airplane until the b...

Page 124: ...enterline of the bottom fuselage skin behind the forward pressure bulkhead and adjust the jacks until the level is centered Should the airplane be either on scales or on the floor first insert a 3 4 inch spacer on each of the main gear struts and a 3 0 inch spacer on the nose gear strut Level airplane by deflating or inflating as required the nose wheel tire to center the bubble in the level ...

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Page 127: ...1F21 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 9 TOWING AND TAXIING ...

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Page 129: ...MAINTENANCE MANUAL CHAPTER 9 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 9 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 9 Table of Contents 1 Feb 28 07 2 Feb 28 07 9 00 00 1 Feb 28 07 2 Feb 28 07 9 10 00 1 Feb 28 07 2 Feb 28 07 9 20 00 1 Feb 28 07 2 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 131: ...1G1 9 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 9 TOWING AND TAXIING TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO GENERAL 9 00 00 1 1G3 TOWING 9 10 00 1 1G5 TAXIING 9 20 00 1 1G7 ...

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Page 133: ...lot or other personnel about tow turning limits of nose gear engine starting and shutdown procedures and any other system functions required to properly and safely move the airplane Pivot Point 30 27 6 27 10 49 4 70 10 3 4 2 1 NOTES 1 Inner Main Gear 7 ft 8 inches 2 Nose Gear 16 ft 1 inch 3 Outer Main Gear 20 ft 1 inch 4 Outer Wing Tip 35 ft 5 inches Turning Radius and Limits Figure 1 ...

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Page 135: ...bar that is stowed in the forward baggage area or by using power equipment that will not damage or cause excess strain to the nose gear steering assembly The stem on the bar is inserted in the hollow of the nose wheel axle at its right side In the event towing lines are necessary lines rope should be attached to both main gear struts as high up on the tubes as possible Lines should be long enough ...

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Page 137: ...the following checks CAUTION DO NOT OPERATE THE ENGINE AT HIGH RPM WHEN RUNNING UP OR TAXIING OVER GROUND CONTAINING LOOSE STONES GRAVEL OR ANY LOOSE MATERIAL THAT MAY CAUSE DAMAGE TO THE PROPELLER BLADES CAUTION OBSERVE WING CLEARANCES WHEN TAXIING NEAR BUILDINGS OR OTHER STATIONARY OBJECTS IF POSSIBLE STATION A GUIDE OUTSIDE THE AIRPLANE TO OBSERVE CAUTION WHEN TAXIING ON UNEVEN GROUND AVOID HOL...

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Page 139: ...1G9 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 10 PARKING AND MOORING ...

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Page 141: ...MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 10 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 10 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 10 Table of Contents 1 Feb 28 07 2 Feb 28 07 10 10 00 1 Feb 28 07 2 Feb 28 07 10 20 00 1 Feb 28 07 2 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 143: ...NTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 10 PARKING AND MOORING TABLE OF CONTENTS SUBJECT SECTION PAGE grid no PARKING 10 10 00 1 1G15 Parking 1 1G15 Locking Airplane 1 1G15 MOORING 10 20 00 1 1G17 ...

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Page 145: ...rking the airplane for any length of time or overnight it must be moored according to sub system section on mooring below NOTE Care should be taken when setting brakes that are overheated or when setting brakes during cold weather when moisture can freeze the brakes 2 Locking Airplane The cabin and baggage compartment doors are provided with a key lock on the outside These locks use the same key A...

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Page 147: ...airplane into wind if possible B Block wheels C Lock aileron and elevator controls with front seat belts CAUTION WHEN USING ROPE OF NON SYNTHETIC MATERIAL LEAVE SUFFICIENT SLACK TO AVOID DAMAGE TO AIRPLANE D Secure wing tie down ropes to retractable tie down rings located on underside of wings outboard of the main gear and to tail tie down ring at approximately 45 degrees NOTE Additional preparati...

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Page 149: ...1G19 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 11 PLACARDS AND MARKINGS ...

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Page 151: ...b 28 07 11 Table of Contents 1 Feb 28 07 2 Feb 28 07 11 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 11 30 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 CHAPTER ...

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Page 153: ...AFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 11 PLACARDS AND MARKINGS TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO EXTERIOR PLACARDS AND MARKINGS 11 20 00 1 1H1 INTERIOR PLACARDS AND MARKINGS 11 30 00 1 1H9 Meyercord Decals 14 1G1 ...

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Page 155: ...ailcone at approximately F S 311 50 The placard identifies the airplane by its model number and serial number Should a question arise concerning the care of the airplane it is important to include the airplane serial number in any correspondence to Piper Aircraft Inc NOTE Any time an airplane is repainted or touched up inspect all placards to ensure that they are not covered with paint are legible...

Page 156: ...RAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Exterior Placards and Markings Figure 1 Sheet 2 of 6 9 11 10 12 13 BOTTOM VIEW FRONT VIEW 8 9 11 89502 AY NOTE Item numbers refer to Decal and Placard detail views shown in Sheets 3 thru 6 ...

Page 157: ...PIN LOCATED ON MAIN STRUT Decal 1 Decal 2 Decal 3 RECOMMENDED SAE GRADE OIL AVERAGE MIL L 22851 AIR TEMP ASHLESS DISPERSANT ALL TEMPS 15W 50W OR 20W 50W ABOVE 80 F 60 ABOVE 60 F 40 OR 50 30 F TO 90 F 40 0 F TO 70 F 30 40 OR 20W 40 BELOW 10 F 30 OR 20W 30 REFER TO LATEST REV OF LYCOMING S I 1014 Exterior Placards and Markings Figure 1 Sheet 3 of 6 Placard 4 GRADE 100LL GRADE 100 Placard 5 NO STEP ...

Page 158: ...05030 2 S N s 4636364 UP Placard 7 S N s 4636001 thru 4636374 S N s 4636375 UP TC PC MANUFACTURED BY THE NEW PIPER AIRCRAFT INC VERO BEACH FLORIDA MODEL SERIAL NO PLATE NO PIPER PART NO 100697 3 Exterior Placards and Markings Figure 1 Sheet 4 of 6 TC PC PIPER AIRCRAFT INC VERO BEACH FLORIDA MODEL SERIAL NO PLATE NO PIPER PART NO 100697 004 ...

Page 159: ...UGH THE FILLER OPENING UNTIL IT REACHES THE TOP OF THE FILLER PLUG HOLE MANUALLY COMPRESS AND EXTEND STRUT SEVERAL TIMES TO REMOVE TRAPPED AIR ADD FLUID EACH TIME IF REQUIRED REPLACE VALVE AND WITH NOSE GEAR STILL CLEAR OF GROUND INFLATE STRUT TO 110 PSI AIR PRESSURE INFLATE NOSE TIRE TO 50 PSI AIR PRESSURE REMOVE JACKS FROM AIRPLANE NORMAL NOSE GEAR STRUT EXTENSION IS 1 70 INCHES WITH APPROX 720 ...

Page 160: ...GE 6 Feb 28 07 1H6 11 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Decal 13 TURN LIMIT Exterior Placards and Markings Figure 1 Sheet 6 of 6 Decal 14 S N s 4636349 thru 4636363 only ...

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Page 162: ...PAGE 8 Feb 28 07 1H8 11 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 163: ...ard detail views shown in Sheets 2 thru 7 Interior Placards and Markings Figure 1 Sheet 1 of 7 1B TOP VIEW 12 7 11 SIDE VIEW 2 3 4 8 9 10 5 16 6 1A I N C R P R O P E L E R O P E N P O W E R L E V E R S I D L E R E V E R S E T H E R H I G H I D L E S T O P L O W I D L E FLIGHT DECK VIEW 7 17 18 19 15 14 OR 14A 13 FRONT VIEW RIGHT WING ONLY 14A 21 20 89502 AY 83985 R ...

Page 164: ...ROLEUM BASE RED HYDRAULIC OIL UNIVIS 40 OR MIL H 5606 OR EQUIVALENT TABLE MUST BE STOWED DURING TAKE OFF LANDING EMERGENCY OXYGEN IN DRAWER UNDER SEAT PULL MASK OUT OF DRAWER FULLY AT FULL EXTENSION GIVE CORD A TUG MAXIMUM DURATION 15 MINS SEE POH NO SMOKING WHILE IN USE EMERGENCY EXIT REMOVE GLASS EMERGENCY OXYGEN IN DRAWER UNDER SEAT AISLE ACCESS PULL MASK OUT OF DRAWER FULLY AT FULL EXTENSION G...

Page 165: ...AL POWER 28 VOLTS D C TURN MASTER SWITCH AND ALL EQUIP OFF BEFORE INSERTING OR REMOVING PLUG Decal 6 Decal 5 Decal 7 Decal 8 Decal 9 Decal 11 Decal 10 FIRE EXTINGUISHER MAXIMUM BAGGAGE THIS COMPARTMENT 100 LBS OPEN CLOSE INSURE PIN WINDOWS GREEN OPEN COURTESY LIGHT RESET OPEN CLOSE PULL LATCH ROTATE HANDLE UP ROTATE HANDLE DOWN INSURE PIN WINDOWS GREEN ...

Page 166: ...STALL PITOT SURFACE WNDSHLD HEAT DEFOG HEAT HEAT HEAT DE ICE CONTROL POWER ICE PROTECTION Decal 13 Typical TURN LANDING GEAR HYDRAULIC PUMP STALL FUEL COORD INDICATION WARNING CONTROL POWER WARN MGT FLIGHT SYSTEMS CABIN ENGINE CO PILOT CABIN CABIN AIR CONDITIONING PRESS START TURN LIGHTS FANS CONTROL POWER DUMP COORD EMERG L BOOST R BOOST FUEL FUEL ELEC ENGINE ENGINE FUEL PUMPS QTY FLOW TAC GAGES ...

Page 167: ... 1 ADF 1 ADF 2 XPDR 2 ENCODER 2 GPS AVIONICS LORAN BUS TIE FLITE INV COOLING PHONE DME 1 SPEAKER NAV 1 COMM 1 COMM 2 NAV 2 HEAD SET DME 2 AMP AMP PITCH AUTO COMPASS RADAR STORM RADAR TRIM PILOT ALT SCOPE PITOT DRAIN STATIC DRAIN STATIC DRAIN PITOT DRAIN STATIC DRAIN LEFTHAND SIDE RIGHTHAND SIDE Decal 14A S N s 4636375 and up TRANSFERS OR DECALS 104349 023 PITOT DRAIN STATIC DRAIN 104349 025 STATIC...

Page 168: ... MALIBU MIRAGE MAINTENANCE MANUAL Interior Placards and Markings Figure 1 Sheet 6 of 7 I N C R O P E N I N C R R I C H L E A N D E C R C L O S E D E C R F R I C T I O N T H R O T T L E P R O P R P M M I X T U R E D N N U P E L E V T R I M L NOSE R Silkscreen 17 ...

Page 169: ...R I F R DAY AND NIGHT ICING FLIGHT WHEN EQUIPPED IN ACCORDANCE WITH THE AIRPLANE FLIGHT MANUAL WARNING AIR CONDITIONER MUST BE OFF TO INSURE NORMAL TAKEOFF CLIMB PERFORMANCE WARNING TURN OFF STROBE LIGHTS WHEN IN CLOSE PROXIMITY TO GROUND OR DURING FLIGHT THROUGH CLOUD FOG OR HAZE PRESSURIZED LANDING NOT APPROVED Placard 19 CAUTION COMPASS CAL MAY BE IN ERROR WITH ELECT EQUIPMENT OTHER THAN AVIONI...

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Page 171: ...PAGE 9 Feb 28 07 1H17 11 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Effectivity 4636001 thru 4636131 Interior Placards and Markings Figure 2 Sheet 1 of 8 ...

Page 172: ...PAGE 10 Feb 28 07 1H18 11 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Interior Placards and Markings Figure 2 Sheet 2 of 8 Effectivity 4636132 thru 4636313 less 4636299 ...

Page 173: ...Interior Placards and Markings Figure 2 Sheet 3 of 8 Effectivity 4636299 4636314 thru 4636374 PAGE 11 Feb 28 07 1H19 11 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 174: ...36 S N s 4636375 and up VA 133 KIAS AT 4300 LBS VLO 165 DN 126 UP SEE AFM VLE 195 MAX NOTE Part numbers shown in Sheets 4 thru 8 are reference only See parts catalog to order Interior Placards and Markings Figure 2 Sheet 4 of 8 MFD PFD 1 PFD 2 OPT ATTITUDE AIRSPEED ALTITUDE GI 106 ADF REC OPT 330 XPONDER 1 ADF IND OPT GNS 430 GNS 430 S TEC A P GMA 340 KRA 10A OPT 330 XPNDR 2 OPT DME OPT COUPLED UN...

Page 175: ...LTR NO 1 ALTR NO 2 NON ESSEN BATTERY S N S 4636001 THRU 4636020 ONLY S N S 4636021 THRU 4636374 ONLY 84967 091 84967 186 S N s 4636021 thru 4636131 84967 228 S N s 4636132 thru 4636374 TIE BUSS MAIN MAIN AVIONICS AVIONICS 1 2 ALTR NO 1 ALTR NO 2 NON ESSEN BATTERY S N S 4636375 AND UP 84967 337 ALTERNATE STATIC SOURCE LOCATED BELOW PANEL UP ALTERNATE DOWN PRIMARY Decal 4 84967 022 S N s 4636001 thr...

Page 176: ...09 In S N s 4636132 up cut decal in half and install above and below indicator Decal 10 84967 110 CABIN PRESS PULL OFF N XXXXX 1 2 3 4 5 6 CYLINDER NUMBER C H T CYCLE DIMMING SWITCH PANEL AVIONICS Decal 11 84967 111 LANDING GEAR UP DOWN RIGHT LEFT FUEL SELECTOR OFF FUEL SELECTOR RIGHT LEFT OFF S N S 4636375 and up Service replacement for 4636001 thru 4636374 84967 024 S N S 4636001 thru 4636374 or...

Page 177: ...A F M BEFORE RE ENGAGEMENT Decal 13 84967 098 Decal 14 84967 099 Decal 15 84967 002 Decal 16 84967 097 Decal 17 84967 106 AMP ALTR 1 SYST VOLT AMP ALTR 2 0 10 20 36 FLAPS DEFROST CABIN TEMP PULL ON PULL HOT PRESS TO TEST DO NOT EXCEED 36 MP BELOW 2400 RPM 32 MP BELOW 2300 RPM S N s 4636001 thru 4636020 only 84967 195 Decal 18 DO NOT EXCEED 36 MP BELOW 2400 RPM 32 MP BELOW 2300 RPM S N s 4636021 an...

Page 178: ...7 268 Placard 30 84967 270 Placard 26 84967 241 Placard 27 84967 259 Placard 21 84967 256 S N s 4636299 and 4636314 thru 4636374 84967 317 S N s 4636375 and up Placard 22 35669 081 Placard 28 84967 049 PARK BRAKE PULL GROUND CLEAR A P NAV 2 Placard 32 84967 242 RMI NAV 2 Placard 33 84967 243 FD PLX ADJ Placard 34 84967 247 NAV 1 ARGUS ADF Placard 35 84967 238 RADIO MASTER Placard 36 84967 239 8496...

Page 179: ...TED SURFACE AND NOT REMOVED IMMEDIATELY If panel is painted with enamel or lacquer use a clean cloth dampened with Mark It J 70 solvent to remove placard to be replaced B Installation 1 If required clean surface to receive decal using alcohol Newly painted surfaces need no preparation 2 Mix a solution consisting of six 6 parts water and one 1 part J 70 solvent P N 179 497 3 Submerge decal in the m...

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Page 181: ...1I3 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 12 SERVICING ...

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Page 183: ... 12 00 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 12 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 12 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 2...

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Page 185: ...tenance of Relief Tube System 5 1I13 REPLENISHING 12 10 00 1 1I17 Service Points 1 1I17 Fuel System 2 1I18 Filling Fuel Cells 2 1I18 Draining Moisture From Fuel System 2 1I18 MIL I 27686 Fuel Anti icing Inhibitors 3 1I19 Draining Fuel System Complete 3 1I19 Brake System 3 1I19 Filling Brake System Reservoir 3 1I19 Draining Brake System 3 1I19 Landing Gear Oleo Struts 4 1I20 Filling Oleo Struts 4 1...

Page 186: ...ation 9 1J1 Cleaning and Inspection 9 1J1 Alternate Air Door 9 1J1 SCHEDULED SERVICING 12 20 00 1 1J5 Airframe Lubrication 1 1J5 Application of Grease 1 1J5 Application of Oil 1 1J5 Lubrication Charts 2 1J6 Chart 1 Special Instructions 2 1J6 Chart 2 Cabin Door Baggage Door and Seats 3 1J7 Chart 3 Main Landing Gear and Hydraulic System 4 1J8 Chart 4 Nose Gear 5 1J9 Chart 5 Control System 6 1J10 Cha...

Page 187: ...ystem The guidelines outlined below must be followed to prevent damage to the finish and ensure long paint life 1 For the first 30 days after painting a Hand wash the aircraft often Use fresh water only b Avoid parking under trees or places where birds roost If sap bird droppings or insect remains are discovered rinse them off immediately Sap bird droppings or insect remains will damage the paint ...

Page 188: ...ircraft Finish Care above and Windshields and Windows below B Engine Compartment Before cleaning the engine compartment 1 Place a pan under the engine to catch waste CAUTION DO NOT SPRAY SOLVENT IN TO THE ALTERNATOR S STARTER AIR INTAKE AND ALTERNATE AIR INLETS 2 With the engine cowling removed spray or brush the engine with solvent or a mixture of solvent and degreaser as desired It may be necess...

Page 189: ...llent coating 1 Flush with clean water to remove excessive amounts of dirt and other substances Adhered particles should be dislodged using fingers or fingernails 2 Use only clean materials such as a soft cloth or clean sponge or soft paper towel such as Kaydry Wipers Wash with a 50 50 solution of isopropanol and water Alternative cleaning solutions that can be used if isopropanol is not available...

Page 190: ...ion between ice and rubber surface of the deice boots G Interior NOTE It is best to test the cleaner on an inconspicuous portion of the fabric to test for discoloration Also avoid soaking or harsh rubbing 1 Vinyl interior surfaces may be cleaned with a damp cloth and mild soap and water solution 2 Leather may be cleaned with a mild hand soap and water solution or with a saddle soap Follow the prec...

Page 191: ...t if the system has been used Likewise attention to the exterior of the aircraft is equally important and exterior surfaces must be cleaned as described below 1 Interior CAUTION SHOULD SPILLAGE EXTENDING INTO THE FUSELAGE BE EVIDENT PROMPT MAINTENANCE ACTION IS REQUIRED TO ENSURE URINE SPILLAGE IN THE FUSELAGE STRUCTURE IS NEUTRALIZED REMOVE PANELS TO ACCESS THE FLOOR STRUCTURE AS REQUIRED a After...

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Page 195: ...PAGE 1 Feb 28 07 1I17 12 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL REPLENISHING 1 Service Points Service Points Figure 1 ...

Page 196: ...r a total capacity of 122 U S gallons Two U S gallons are considered unusable fuel B Draining Moisture From Fuel System CAUTION WHEN DRAINING ANY AMOUNT OF FUEL CARE SHOULD BE TAKEN TO ENSURE THAT NO FIRE HAZARD EXISTS BEFORE STARTING THE ENGINE The fuel tanks and fuel strainer should be drained daily prior to first flight and after refueling to avoid the accumulation of water or sediment Each fue...

Page 197: ...he drain cup pin to hold the valve open The remaining fuel in the system may be drained through the filter bowl 3 Brake System The brake system contains a hydraulic fluid reservoir through which the brake system is periodically serviced Fluid is drawn from the reservoir by the brake master cylinders to maintain the volume of fluid required for maximum braking efficiency Spongy brake pedal actions ...

Page 198: ...ing Oleo Struts For landing gear and or oleo strut repair procedures refer to 32 10 00 and 32 20 00 A Filling Oleo Struts To fill the nose or main gear oleo strut with fluid MIL H 5606 whether it be the addition of a small or large amount proceed as follows 1 Raise the airplane on jacks 2 Place a pan under the gear to catch spillage 3 At the filler plug relieve air pressure from the strut housing ...

Page 199: ... NOTE Moisture free compressed air may be used in lieu of nitrogen gas on a temporary basis however the strut should be deflated and serviced with nitrogen as soon as possible Lower the airplane and while rocking it let air from the valve to bring the strut down to the proper extension Before capping the valve check for valve core leakage If the airplane is on jacks ensure that the struts are full...

Page 200: ...re tight The cylinder rods are to be free of all dirt and grit To clean the rods use a rag soaked in hydraulic fluid and carefully wipe them All the hydraulic lines should also be checked for leaks kinks and corrosion Check the tightness of the attachment fittings Repair and inspection procedures for the hydraulic pump cylinders and various components may be found in 29 10 00 of this manual Servic...

Page 201: ...ere after every 50 hours of engine operation this is accomplished by removing the lockwire from the bolt head at the end of the filter loosening the bolt and removing the filter assembly from the adapter 2 Before discarding the filter element remove the outer perforated paper cover and using a sharp knife cut through the folds of the element at both ends close to the metal caps Then carefully unfo...

Page 202: ...2 amp rate Quick charges are not recommended B Battery Valve Regulated Lead Acid S N s 4636375 and up Access to the 24 volt battery is gained by opening the forward baggage door and removing the left floor of the forward baggage compartment Gill valve regulated non maintainable batteries are fully charged when they leave the factory Non maintainable means that this type of battery cannot be opened...

Page 203: ...ent filter refer to Parts Catalog 2 Remove the filter element and blow out with compressed air from gasket side or wash in warm water and mild detergent and allow to dry 3 The filter housing can be cleaned by wiping with a clean cloth soaked in suitable quick drying type solvent When the housing is dry reinstall in accordance with Installation of Air Filter 12 Alternate Air Door The alternate door...

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Page 207: ...ace as necessary C Removal all excess lubricants from components to prevent collecting dirt and sand in quantities capable of causing excessive wear or damage to bearing surfaces 2 Application of Grease When lubricating bearings and bearing surfaces with a grease gun ensure gun is filled with new clean grease specified for the particular application before applying lubricant to grease fittings A I...

Page 208: ...O NOT BLOW OUT WITH COMPRESSED AIR OR USE OIL REPLACE FILTER IF EXCESSIVELY CONTAMINATED DAMAGED OR PUNCTURED 2 LUBRICATION POINTS WIPE CLEAN OR GREASE OIL DIRT ETC BEFORE LUBRICATING 3 BEARING AND BUSHINGS CLEAN EXTERIOR WITH A DRYING TYPE SOLVENT PRIOR TO LUBRICATING 4 WHEEL BEARINGS CLEAN OLD GREASE FROM WHEEL HOUSING OUTER RACE AND BEARING ASSEMBLY USING DRYING TYPE SOLVENT PACK GREASE BETWEEN...

Page 209: ... PRF 7870C 100 HRS 2 BAGGAGE DOOR LATCH MECHANISM Special Instruction 2 DRY LUBRICANT 100 HRS 3 PILOT AND COPILOT SEAT ADJUSTMENTS MIL PRF 7870C 100 HRS 4 CABIN DOOR HINGES Special Instruction 2 MIL PRF 7870C 100 HRS 5 CABIN DOOR LATCH MECHANISM Special Instruction 2 DRY LUBRICANT 100 HRS 6 ACCESS DOOR HINGE Special Instruction 2 MIL PRF 7870C 100 HRS 7 ACCESS DOOR LATCH Special Instruction 2 DRY ...

Page 210: ...T LUBRICANT FREQUENCY 1 BRAKE RESERVOIR Special Instruction 5 MIL H 5606 50 HRS 2 HYDRAULIC PUMP RESERVOIR Special Instruction 5 MIL H 5606 50 HRS 3 RETRACTION CYLINDER ROD END BEARINGS Special Instruction 3 MIL PRF 7870C 100 HRS 4 MAIN GEAR TORQUE LINKS Special Instruction 2 MIL PRF 7870C 100 HRS 5 MAIN GEAR WHEEL BEARINGS Special Instruction 4 MIL G 81322 100 HRS ...

Page 211: ... HRS 2 RETRACTION CYLINDER AND ASSIST SPRING ROD END BEARINGS Special Instruction 3 MIL PRF 7870C 100 HRS 3 NOSE GEAR PIVOT POINT Special Instruction 2 MIL G 7711 100 HRS 4 TORQUE LINK ASSEMBLY Special Instruction 2 MIL PRF 7870C 100 HRS 5 NOSE WHEEL BEARINGS Special Instruction 4 MIL G 81322 100 HRS 6 STEERING BELLCRANK AND ROD ENDS Special Instruction 3 MIL PRF 7870C 100 HRS 7 NOSE GEAR DOOR HIN...

Page 212: ... Instruction 2 MIL G 23827 100 HRS 1 FLAP CONTROL ROD END BEARINGS Special Instruction 3 MIL PRF 7870C 100 HRS 2 RUDDER CONTROL SECTOR Special Instruction 3 MIL PRF 7870C 100 HRS 3 ELEVATOR TRIM ROD END BEARINGS Special Instruction 3 MIL PRF 7870C 100 HRS 4 ELEVATOR SECTOR AND CONTROL ROD END BEARINGS Special Instruction 3 MIL PRF 7870C 100 HRS 5 ELEVATOR TRIM SCREW Special Instruction 2 MIL G 238...

Page 213: ...0 HRS 2 CONTROL COLUMN ATTACHMENT ARM Special Instruction 3 MIL PRF 7870C 100 HRS 3 ELEVATOR TORQUE TUBE ASSEMBLY Special Instruction 3 MIL PRF 7870C 100 HRS 4 RUDDER TORQUE TUBE ASSEMBLY Special Instruction 2 MIL PRF 7870C 100 HRS 5 BRAKE ROD ENDS Special Instruction 2 MIL PRF 7870C 100 HRS 6 BUSHING RUDDER PEDAL MOUNT Special Instruction 3 MIL PRF 7870C 100 HRS AILERON ELEVATOR RUDDER AND TRIM C...

Page 214: ...CANT FREQUENCY 1 PULLEYS AND TRIM WHEELS Special Instruction 3 MIL PRF 7870C 100 HRS 2 AILERON HINGES Special Instruction 3 MIL PRF 7870C 100 HRS 3 AILERON SECTOR Special Instruction 2 DRY LUBRICANT 100 HRS AILERON ELEVATOR RUDDER AND TRIM CABLES Special Instruction 2 MIL G 23827 100 HRS Grease cables where they pass through a fair lead or over a pulley Not shown ...

Page 215: ...REQUENCY 1 COMPOSITE BLADE PROPELLERS Special Instruction 6 AEROSHELL 6 GREASE 100 HRS 12 MONTHS whichever comes first 1 ALUMINUM BLADE PROPELLERS Special Instruction 6 AERO SHELL 6 GREASE 100 HRS 12 MONTHS whichever comes first NOTE If annual operation is significantly less than 100 hours calendar lubrication intervals should be reduced to six months ...

Page 216: ... patch across the top center of the tire Rotate the tire 45 and release it again If the tire returns to the same position add a 1 ounce patch and again rotate the tire and release it Continue this procedure until the tire is balanced C When balance is attained put a chalk mark on the sidewall directly below the patch Use one mark for each half ounce of weight needed Mark the valve stem location on...

Page 217: ...hen tapping them with a 1 8 27 pipe tap C The 6 spacers were made from 1 2 inch aluminum tubing the two lengths of spacers are suitable for balancing most any aircraft wheel D The 7 bushings may be made from one inch phenolic or aluminum using a 1 1 2 inch hole saw to cut out the smaller bushing and a 1 3 4 hole saw to cut out the larger By inserting a 1 4 inch long threaded bolt through the pilot...

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Page 221: ...1J19 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 20 STANDARD PRACTICES AIRFRAME ...

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Page 223: ...GE DATE 20 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 20 Table of Contents 1 Feb 28 07 2 Feb 28 07 20 00 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 20 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 225: ... 1K4 Inspection of Flexible Hoses 4 1K4 Flared Tube Assemblies 6 1K6 Flareless Tube Assemblies 7 1K7 Support Clamps 9 1K9 Dye Penetrant Inspection 10 1K10 Threaded Fastener Installation 10 1K10 Lubrication of Threads 11 1K11 PAINTING 20 20 00 1 1K13 Painting Safety 1 1K13 Polyurethane Paint Safety 1 1K13 Paint Application 2 1K14 Painting Sequence 2 1K14 Color Matching 2 1K14 Trim and Registration ...

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Page 227: ...r is not sufficient and is not recommended Some wrenches are quite sensitive to the way they are supported during a tightening operation Any instructions furnished by the manufacturer must be followed explicitly When it is necessary to use a special extension or adapter wrench together with a torque wrench a simple mathematical equation must be worked out to arrive at the correct torque reading Fo...

Page 228: ...C PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 2 Feb 28 07 1K2 20 00 00 Torque Wrench Formula Figure 1 Installing Rod End Bearings Figure 2 3 Installing Rod End Bearings Install rod end bearings as shown in Figure 2 ...

Page 229: ...he rivet sleeve when removing rivets tends to enlarge hole B To remove from thin material drill away tapered portion of stem to destroy the lock Use a small center drill bit on top of the rivet stem to provide a guide for a larger bit See Figure 3 Views 2 and 3 C Pry remainder of locking collar out of rivet head with a drift pin See Figure 3 View 3 D Drill almost but not completely through head of...

Page 230: ...sionally occurs This condition is such that rubber material protrudes through the wire braid cover This condition has no effect on hose quality It is recommended that flexible hoses be inspected every 100 hours especially those in the engine compartments When inspecting hoses look for the following conditions A Check each installation to be sure the hose is not kinked twisted or distorted Check fo...

Page 231: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 5 Feb 28 07 1K5 20 00 00 Hose Tube and Line Markings Figure 4 ...

Page 232: ...ical seals are never to be reused If a connection is broken the seals must be replaced B Install new conical seals CAUTION ANGULAR MISALIGNMENT BETWEEN TUBE AND FITTING WILL OVER STRAIN SLEEVE AND NUT DURING TORQUE UP APPLY TORQUE ONLY AFTER TUBE CENTER LINE IS SQUARELY MATED TO THE FITTING CENTER LINE NOTE Apply torque on back portion of nut next to shoulder to minimize distortion of thread C Tig...

Page 233: ...ten nut until cutting edge of sleeve grips tube This point is determined by slowly turning tube back and forth while tightening nut When tube no longer turns nut is ready for final tightening D Final tightening depends upon type and size of tubing On aluminum alloy tubing up to and including half inch outside diameter tighten nut from 1 to 1 1 6 turns On aluminum alloy tubing over half inch outsid...

Page 234: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 8 Feb 28 07 1K8 20 00 00 Flareless Tube Fittings Figure 6 ...

Page 235: ...es in areas not subject to vibration A teflon cushioned clamp is used in areas where the deteriorating effects of hydraulic fluid or fuel is expected however because it is less resilient it does not provide as good a vibration damping effect as other cushion materials Use bonded clamps to secure metal hydraulic fuel and oil lines in place Unbonded clamps should be used only for securing wiring Rem...

Page 236: ...ler washers spacers under the nut to adjust for fastener length or alignment of cotter key hole Where nutplates are used adjust for protruding head fastener length by using up to a maximum of two standard filler washers under the fastener head B Washer Usaqe Add a maximum of two NAS1149 washers of the correct diameter material and finish that matches the fastener being installed under fastener hea...

Page 237: ...red fittings apply lubricant to next three threads only F Ensure lubricant does not enter fittings or flared areas G Lubricate any fittings going to engine with same fluid going through lines CHART 3 THREAD LUBRICANTS TYPE OF LINE TYPE OF LUBRICANT Brake MIL H 5606 Tite Seal 3 Y3 Deicer Air TT A 580 JAN A 669 Anti Seize Compound White Lead Base Freon TT A 580 or MIL T 5544 Anti Seize Compound Fuel...

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Page 239: ...HANE PAINT MAY BE DANGEROUS TO YOUR HEALTH SERIOUS INJURY WILL RESULT IF SAFETY PRECAUTIONS ARE NOT FOLLOWED WARNING DURING TRANSIT AND STORAGE CHECK FOR SIGNS OF A BULGING CAN OTHER THAN NORMAL ODOR OR A CHANGE IN RESIN FROM A CLEAR TO A CLOUDY STATE A SLOW CARBON DIOXIDE BUILDUP WILL CAUSE CAN TO BURST REMOVE AND PROPERLY DISPOSE ANY DEFECTIVE CANS WARNING ENSURE ADEQUATE VENTILATION AND WEAR AP...

Page 240: ...ailerons and flaps Paint flap and aileron wells wing tips and leading and trailing edges D Paint the bottom of the airplane first including bottom of horizontal tail surfaces Starting at the root and working outward spray chordwise Work up fuselage and allow spray to cover sides Work up to engine Spray wing bottom Start each painter at the root and work toward tip spraying chordwise E Lower airpla...

Page 241: ...nitrocellulose lacquers over old nitrocellulose finishes D Acrylic nitrocellulose lacquers will not adhere to nitrocellulose and epoxy finishes and to bare metal For best results apply lacquers over fresh successive coatings of wash primer and modified zinc chromate They also adhere to freshly applied epoxy coatings dried less than 6 hours E Epoxy topcoats adhere to all paint systems in good condi...

Page 242: ...Occupational Safety and Health Act OSHA requirements regarding air circulation lighting and fire protection Lock storage facilities to prevent children and unauthorized personnel entry C Invert pigmented materials every inventory so pigments will not pack to can bottom Properly dispose of empty containers D Use older materials first Useful life of some finishes is limited E Storage area temperatur...

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Page 245: ...PART NUMBER 761 876 February 28 2007 2A1 AIRPLANE MAINTENANCE MANUAL CARD 2 OF 9 PA 46 350P S N s 4636001 AND UP PIPER AIRCRAFT INC ...

Page 246: ...2A2 Published by Technical Publications Piper Aircraft Inc 2926 Piper Drive Vero Beach Florida 32960 U S A Member General Aviation Manufacturers Association ...

Page 247: ...2 3 4 5 and 6 CR981223 December 23 1998 1 2 3 4 5 and 6 PR000201 February 1 2000 1 2 3 4 5 and 6 PR010515 May 15 2001 1 CR050730 July 30 2005 1 2 3 4 5 6 7 and 8 PR060207 February 7 2006 1 2 3 4 5 6 7 and 8 CR070228 February 28 2007 1 2 3 4 5 6 7 8 and 9 COMPLETE REVISION OF MAINTENANCE MANUAL 761 876 Revisions appear in all Aerofiche Cards Accordingly discard your entire existing Aerofiche Card S...

Page 248: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 1 Feb 28 07 AEROFICHE EFFECTIVITY 2A4 THIS PAGE INTENTIONALLY BLANK ...

Page 249: ...Feb 28 07 Intro Table of Contents 1 Feb 28 07 2 Feb 28 07 Introduction 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 Index 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHA...

Page 250: ...PAGE 2 Feb 28 07 INTRO LIST OF EFFECTIVE PAGES 2A6 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 251: ...A9 Effectivity 2 2A10 Serial Number Explanation 2 2A10 Assignment of Subject Material 2 2A10 Pagination 3 2A11 Aerofiche Effectivity 3 2A11 Identifying Revised Material 3 2A11 Indexing 3 2A11 List of Effective Pages 3 2A11 Warnings Cautions and Notes 3 2A11 Accident Incident Reporting 4 2A12 Supplementary Publications 4 2A12 Piper Publications 4 2A12 Vendor Publications 4 2A12 Chapter Section Inde...

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Page 253: ...GENUINE PIPER AIRCRAFT PARTS OR PIPER AIRCRAFT APPROVED PARTS OBTAINED FROM PIPER APPROVED SOURCES IN CONNECTION WITH THE MAINTENANCE AND REPAIR OF PIPER AIRPLANES Genuine PIPER parts are produced and inspected under rigorous procedures to ensure airworthiness and suitability for use in PIPER airplane applications Parts purchased from sources other than PIPER even though identical in appearance ma...

Page 254: ...ane are broken down into subsystems These sub systems are identified by the second element of the standard numbering system The element 40 of the number 28 40 01 concerns itself with the indicating section of the fuel system C Unit Subject The individual units within a sub system section may be identified by the third element of the standard numbering system The element 01 of the number 28 40 01 i...

Page 255: ...his set 8 Identifying Revised Material A revision to a page is defined as any change to the printed matter that existed previously Revisions additions and deletions are identified by a vertical line i e change bar along the left hand margin of the page opposite only that portion of the printed matter that was changed A change bar in the left hand margin opposite the footer i e chapter section subj...

Page 256: ...s Catalog P N 761 878 2 Periodic Inspection Report Form P N 767 011 3 Progressive Inspection Manual 50 hour P N 767 013 B Vendor Publications WARNING FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION S WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT MAY RENDER THE AIRCRAFT UNAIRWORTHY 1 AIR CONDITIONING COMPRESSOR Vendor Address Sanden International USA Inc PH 972 442 8400...

Page 257: ...cialty Systems PH 330 374 3040 Goodrich Corporation FAX 330 374 2290 1555 Corporate Woods Parkway Uniontown Ohio 44685 8799 Technical Assistance PH 800 334 2377 330 374 3743 FAX 330 374 2290 Email dssd support goodrich com http www deicingsystems goodrich com Black Standard Pneumatic De Icer Installation Maintenance and Repair Manual ATA 30 10 31 SmartBoot System ATA 30 10 65 8 ELECTRONIC FLIGHT I...

Page 258: ...ntext See www avantext com or PH 800 998 8857 11 FIRE EXTINGUISHER PORTABLE Vendor Address H3R Inc PH 800 249 4289 43 Magnolia Ave 4 San Francisco California 94123 2911 http www h3r com index htm 12 FORCE APPLICATOR KIT Vendor Address Safe Flight Instrument Corp PH 914 946 9500 20 New King Street White Plains New York 10602 13 FUEL BOOST PUMP Vendor Address Parker Hannifin Corp PH 800 272 7537 Nic...

Page 259: ...ww unisonindustries com index4 html Installation Operation F1100 MASTER SERVICE MANUAL and Maintenance 4300 6300 SERIES MAGNETO MAINTENANCE AND Instructions OVERHAUL MANUAL L 1363 19 NAVIGATION COMMUNICATIONS AND GPS NAV COM GPS Vendor Address Garmin International PH 913 397 8200 1200 East 151ST Street Olathe KS 66062 http www garmin com 20 OXYGEN SYSTEM Vendor Address Scott Aviation PH 716 683 51...

Page 260: ...DAR WEATHER RDR 2000 Vendor Address Honeywell Bendix King See Autoflight above Maintenance Manual Bendix King ART 2000 P N 006 05332 0001 25 RADIO COOLING BLOWER Vendor Address Globe Motors PH 937 228 3171 2275 Stanley Ave FAX 937 229 8531 Dayton Ohio 45404 http www globe motors com home html 26 STARTER Vendor Address Kelly Aerospace See Alternator above or Sky Tec Partners Ltd PH 800 476 7896 350...

Page 261: ...MALIBU MIRAGE MAINTENANCE MANUAL 28 VACUUM PUMP Vendor Address Aero Accessories Inc PH 800 822 3200 1240 Springwood Avenue Gibsonville NC 27249 http www aeroaccessories com index html 29 VACUUM REGULATORS Vendor Address Parker Hannifin Corp see Fuel Boost Pump above ...

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Page 263: ...chapter CHAPTER SECTION TITLE GRID NO 4 AIRWORTHINESS LIMITATIONS 1C1 00 Airworthiness Limitations 5 TIME LIMITS MAINTENANCE CHECKS 1C9 00 General 10 Time Limits 20 Scheduled Maintenance Checks 30 Special Inspections 50 Unscheduled Maintenance Checks 6 DIMENSIONS AND AREAS 1E13 00 General 7 LIFTING AND SHORING 1F1 10 Jacking 8 LEVELING AND WEIGHING 1F9 10 Weighing and Balancing 20 Leveling 9 TOWIN...

Page 264: ...emperature Control 22 AUTOFLIGHT 2F11 10 Autopilot 23 COMMUNICATIONS 2G19 00 General 50 Audio Integrating 60 Static Discharging 24 ELECTRICAL POWER 2H11 00 General 30 DC Generation 40 External Power 60 Electrical Load Distribution 25 EQUIPMENT FURNISHINGS 2J11 10 Flight Compartment 20 Passenger Compartment 50 Cargo Compartments 60 Emergency 26 FIRE PROTECTION 2K15 20 Extinguishing 27 FLIGHT CONTRO...

Page 265: ...rs 60 Propellers Rotors 31 INDICATING RECORDING SYSTEMS 4C1 50 Central Warning Systems 32 LANDING GEAR 4C13 00 General 10 Main Gear and Doors 20 Nose Gear and Doors 30 Extension and Retraction 40 Wheels and Brakes 50 Steering 60 Position and Warning 33 LIGHTS 4G5 10 Flight Compartment 20 Passenger Compartment 30 Cargo and Service Compartments 40 Exterior 34 NAVIGATION 5C1 00 General 10 Flight Envi...

Page 266: ...00 General 10 Investigation Cleanup and Aerodynamic Smoothness 70 Repairs 80 Electrical Bonding 52 DOORS 6G13 10 Passenger Crew 20 Emergency Exit 30 Cargo 70 Monitoring and Operation 55 STABILIZERS 6H13 00 General 10 Horizontal Stabilizers 20 Elevator 30 Vertical Stabilizer 40 Rudder 56 WINDOWS 6I19 00 General 10 Flight Compartment 20 Cabin 30 Door 57 WINGS 6K5 40 Attach Fittings 50 Flight Surface...

Page 267: ... Power Supply 20 Distribution 76 ENGINE CONTROLS 7G17 10 Power Control 77 ENGINE INDICATING 7H3 10 Power 20 Temperature 40 Integrated Engine Instrument Systems 79 OIL 7J3 20 Distribution 30 Indicating 80 STARTING 7J15 10 Cranking 81 TURBINES 7K9 20 Turbo Supercharger 91 CHARTS WIRING DIAGRAMS 8C1 10 Charts 21 and up Electrical Schematics 91 CONT CHARTS WIRING DIAGRAMS CONT 9C1 Electrical Schematic...

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Page 269: ...sion Control Wing 6L3 Attitude Indicator 5D5 Autopilot 2F17 Component Locator 2G2 Installation 2F18 2F20 Maintenance 2F23 Operational Checkout 2F24 Pitch Servo 2G12 Pressure Transducer 2G6 Roll Servo 2G4 Servo Clutch Torque Adjustment 2G15 Trim Monitor 2G3 Trim Servo 2G6 Yaw Amplifier 2G14 Yaw Servo 2G10 Avionics Cooling 2C14 Avionics Master Switch 2H1 B Ball Diameters for Testing Hose Restriction...

Page 270: ...rrection 2I10 Troubleshooting 2I7 2I13 Valve Regulated Lead Acid 2I13 Bonding 6G9 Resistance Index 6G10 Buses Avionics 2H19 Main 2H19 Circuit Breaker Panel 6D22 Electrical Shelf 6E7 External Power 2I19 Load Distribution 2J1 Relay Installation Co Pilot s Side 6E10 K1 thru K8 6E10 Pilot s Side 6E9 Schematics Air Conditioning 8E7 Airspeed Standby 9E19 Altimeter Radar 9F14 Altimeter Standby 9E19 Annun...

Page 271: ...n Light 9E5 WX 500 9F11 XM Receiver 8E23 Switch Panels 6E1 Symbols 8D14 System 2H17 Troubleshooting 2H20 Tie Bus Panel Connections 6E3 Volt Ammeter 2J4 Voltage Regulation and Control 2H19 Wire Coding 8D13 Elevator Balancing 6I3 Control System Installation 3D23 Rigging and Adjustment 3D24 Troubleshooting 3D19 Torque Tube Bearing Changes 3D20 Trim Controls Actuator Assembly 3E3 Corrosion Control 3E4...

Page 272: ...Drain Valve 3G8 Draining 1I19 Draining Moisture 1I18 Fuel Filter 3G7 Fuel Pumps Specifications 3G5 Fuel Quantity Gauge Accuracy Test 3G14 Full Range Check 3G20 Senders 3G13 Leak Test Setup 3G1 Selector Switch and Valve 3G6 Cable Adjustment 3G7 Troubleshooting 3F16 Leak Evaluation 3F22 G GMA 340 Audio Panel Adjustments 2H6 Installation 2H3 System Functional Test 2H4 GNS 430 5F5 GNS 530 5F5 Ground C...

Page 273: ... 4D11 Position and Warning 4F19 Landing Gear Up Power Reduced Warning Switch Adjustment 4G2 Troubleshooting 4F20 Leading Particulars and Principal Dimensions 1E20 Leveling 1F17 Life Limited Parts 1C7 Lifting 1F7 See also 57 40 00 Lights Exterior 4H3 Landing 4H7 Position 4H4 Pulse 4H7 Strobe 4H3 Taxi 4H6 Wing Inspection Light 4H7 Interior 4G11 Annunciator Panel 4G12 Baggage Area 4G21 Forward 4H1 Re...

Page 274: ...g 3K6 Troubleshooting 3J20 Propeller Assembly 7C9 Publications Piper A12 Vendor A12 Q Quad Digital Indicator QDI See Engine Instruments Transicoil EMIS R Radar 5F1 Repairs Fiberglass 6F19 Metal Wire Stitching 6G5 Thermoplastic 6F21 List of Materials 6F24 Window Windshield Acrylic 6J10 Restraint System 2J23 Inertial Reel Adjustment 2J23 Inspection 2J23 Revised Material A11 Robinair 34700 Charging S...

Page 275: ... Bellcrank Centering 4C22 Horn Arm Gap 4C22 Nose Wheel Centering 3C15 4C22 Rudder Pedal Neutral Alignment 3C15 4C22 Rudder Travel Tool 3C15 Torque Conversion 8C20 Torque Wrench Formula 1K2 Towing 1G5 Transponder 5F9 GTX 327 5F9 GTX 330 5F9 Post Installation Setup Procedure 5F10 ARINC 429 Configuration Page 5F11 Display Mode and Key Lighting 5F11 Hexadecimal Conversion 5F13 Operation Configuration ...

Page 276: ...in 6I11 Vertical Speed Indicator 5C18 Volt Ammeter See Electrical W Warnings Cautions and Notes A11 Weather Radar 5F1 Weighing 1F15 Wheel Brake Assembly 4F4 Wheels Bearing Cup 4F4 Main Wheel Assembly 4F2 Nose Wheel Assembly 4F1 Repairs 4F3 Windows and Windshields Door Window 6K3 Heated Windshield Testing 3J15 Troubleshooting 3J15 Inspection and Repair Definitions 6J1 Limitations 6J1 Crack Limitati...

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Page 279: ...2C1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 21 ENVIRONMENTAL SYSTEMS ...

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Page 281: ...07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 21 40 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 CHAPTER SECTION PAGE DATE 21 50 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 19 F...

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Page 283: ...oling Blower 3 2C13 Removal 3 2C13 Installation 3 2C13 Muffin Fan 3 2C13 PRESSURIZATION CONTROL 21 30 00 1 2C19 General 1 2C19 Troubleshooting 1 2C19 Components 7 2D1 Cabin Outflow Valve Cabin Safety Valve 7 2D1 Removal 7 2D1 Installation 7 2D1 Servicing 7 2D1 Auxiliary Volume Tank 7 2D1 Vacuum Regulator 7 2D1 Cabin Pressure Controller 10 2D4 Description 10 2D4 Operational Check 10 2D4 Vacuum Reli...

Page 284: ...D13 Removal 3 2D13 Installation 3 2D13 Rigging 4 2D14 Bleed Air Shutoff Valve 4 2D14 Removal 4 2D14 Installation 4 2D14 Auxiliary Cabin Heater 4 2D14 Removal 4 2D14 Installation 4 2D14 COOLING 21 50 00 1 2D17 General 1 2D17 Troubleshooting 1 2D17 Servicing Cooling System 7 2D23 Definitions 7 2D23 Service Valves 7 2D23 Description 7 2D23 Replacement 7 2D23 Malfunction Detection 9 2E1 Special Servic...

Page 285: ...2 Installation 31 2E23 Checking Compressor Oil Level 31 2E23 Adjustment of Drive Belt Tension 32 2E24 Refrigerant Lines and Routing 33 2F1 Evaporator Blower Assembly 34 2F2 Removal 34 2F2 Installation 34 2F2 Expansion Valve 34 2F2 Removal 34 2F2 Installation 34 2F2 Condenser 35 2F3 Removal 35 2F3 Installation 35 2F3 Condenser Blower Motor Assembly 35 2F3 Removal 35 2F3 Installation 35 2F3 Receiver...

Page 286: ...PAGE 4 Feb 28 07 2C8 21 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 287: ...h utilizes ambient air to cool the bleed air hot air from an exhaust shroud to heat the bleed air or a mixture of ambient and hot air to obtain the bleed air temperature necessary to maintain the desired cabin comfort level The cabin pressurization and control system consist of an outflow valve isobaric safety valve cabin altitude and rate selector electrically operated vacuum solenoid valve surge...

Page 288: ...PAGE 2 Feb 28 07 2C10 21 00 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 289: ...ration Flapper type check valves are located at the forward pressure bulkhead A Removal 1 Loosen the two clamps that secure the flexible adapter ducts to the blower 2 Loosen the two clamps that secure the flexible adapter ducts to the inlet and outlet ducts 3 Slide the aft flexible adapter duct rearward over the outlet duct 4 Disconnect the electrical leads from the blower 5 Slide the blower aft a...

Page 290: ...porators Defroster Safety Valve DEFROST PULL ON CABIN PRESS PULL OFF CABIN TEMP PULL HOT Conditioned Air Check Valve Check Valve Electric Duct Heater Ground Blower Pressure Bulkhead Defrost Control Cabin Press Control Temperature Control Dump Valve Sonic Nozzle Bleed Air Temperature Control Valve Air Selector Box NACA Flush Inlet Heat Muff Bleed Air Sonic Nozzle Firewall Bleed Air Shutoff Valve Ch...

Page 291: ...e and gaskets with flapper on aft side between bleed air supply tube and forward pressure bulkhead 5 Secure valve bleed air supply tube and cabin air supply tube to pressure bulkhead with six bolts 4 Avionics Cooling Blower See Figure 2 The avionics cooling blower is installed on the right side of the fuselage behind the instrument panel at FS 108 00 The cooling air is directed through ducts to in...

Page 292: ...PAGE 4 Feb 28 07 2C14 21 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL J308 P308 BLOWER DUCT TUBING A A Avionics Cooling Figure 2 Sheet 1 of 3 ...

Page 293: ...ANUAL FWD FWD UP MUFFIN FAN SCREW 2 WASHER 2 AV5 TO AUTOPILOT COMPUTER TO GNS 530 NO 2 TO GNS 530 NO 1 DUCT TUBING BLOWER VIEW A A ACFT SKIN F S 108 00 ROTATED 180 TO XPNDR 2 TO XPNDR 1 TO FLIGHT MAX DISPLAY S N S 4636299 4636314 THRU 4636374 104468 F Avionics Cooling Figure 2 Sheet 2 of 3 ...

Page 294: ...RAGE MAINTENANCE MANUAL FWD FWD UP MUFFIN FAN SCREW 2 WASHER 2 AV5 TO AUTOPILOT COMPUTER TO GNS 430 NO 2 TO GNS 430 NO 1 DUCT TUBING BLOWER VIEW A A ACFT SKIN F S 108 00 ROTATED 180 TO XPNDR 2 TO XPNDR 1 PLACE CAP ON OUTLET 105121 M Avionics Cooling Figure 2 Sheet 3 of 3 ...

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Page 297: ...ciator panel is provided to indicate a cabin altitude above 10 000 feet The cabin safety valve is held open on the ground with the engine operating by a vacuum applied to the control chamber of the safety valve The vacuum regulator of the vacuum system provides a vacuum of 4 8 5 2 in mercury referenced to cabin pressure This vacuum holds the safety valve open while on the ground through the action...

Page 298: ...PAGE 2 Feb 28 07 2C20 21 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Cabin Pressure Control System Figure 1 ...

Page 299: ...oller controller Defective landing gear Remove and replace safety switch switch Dump switch incorrectly Replace switch positioned or defective No pressure to door seal Check and repair door seal or door seal valve Excessive leakage in Locate leak and tighten pressurization ducts connections Excessive cabin leakage Locate and repair leak Solenoid valve malfunctions Replace valve in the open positio...

Page 300: ...replace controller Pressurized operation Solenoid valve malfunction Replace valve before takeoff and in the closed position after landing Landing gear safety switch Remove and replace dump switch malfunction in the switch open position Broken wiring to the Repair wiring solenoid valve Loose or damaged pneumatic Check tube connections or tube between solenoid valve replace damaged tube and safety v...

Page 301: ...ty valve Internal malfunction in Remove and replace controller controller Excessive cabin leak rate Seal leaks Cabin pressure will not Defective outflow valve Remove and replace valve maintain control setting Defective safety valve Remove and replace valve Defective cabin altitude Remove and replace cabin controller altitude controller Pressurization duct leakage Locate leak and tighten connection...

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Page 303: ...on shown in Detail A of Figure 2 must be met to ensure proper sealing To provide proper clearance between nuts and gasket face adjust for clearance as follows 1 Remove nuts using a deep socket and remove enough shims to meet dimensional requirements A minimum of one shim is required each place for installation of nut 2 Install nuts and tighten 3 Apply a drop of locking compound MIL S 22473 EV to t...

Page 304: ...PAGE 8 Feb 28 07 2D2 21 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Safety and Outflow Valves Figure 2 ...

Page 305: ...PAGE 9 Feb 28 07 2D3 21 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Cabin Pressure Controller Figure 3 ...

Page 306: ...in rate control selector knob to the 9 o clock position c Rotate cabin altitude selector knob until CABIN ALT indicates approximately 500 feet above field altitude d Set brakes start engine and establish a steady cabin air inflow e Pull landing gear warning circuit breaker and note that safety valve closes and outflow valve remains open f Rotate cabin altitude selector knob counterclockwise until ...

Page 307: ...alve to the bulkhead Remove the valve 3 Installation a Secure the valve to the bulkhead with the screws and washers b Reconnect the lines to the valve c Tighten the nuts finger tight plus one and one half turns F Bleed Air Dump Valve The bleed air dump valve is just forward of the firewall F S 79 00 and above the bleed air crossover duct assembly It is actuated by the cabin pressure control knob o...

Page 308: ...ULLY EXTENDED A Equipment Required Pressurization Test Cart commercially available B Procedure NOTE Remove cowling before beginning 1 Plug cabin altimeter indicator 3 in 1 indicator sensing port marked C P 2 Disconnect vacuum line at the tee on the rear of the cabin pressurization controller Cap tee and plug vacuum line CAUTION IMPROPER SETTING WILL CAUSE DAMAGE TO CABIN PRESSURIZATION CONTROLLER ...

Page 309: ...imum cabin differential of 5 25 psid occurs Determine airflow required to maintain 5 25 psid and record If airflow exceeds 40 SCFM or a major leak is occurring in one or more places or if excessive noise is found identify for corrective sealing NOTE If cabin will not pressurize above 1 psid due to excessive leakage a Disconnect cabin controller line at outflow valve b Pressurize to not more than 5...

Page 310: ...E IN NEXT STEP EXCESSIVE PRESSURE CAN CAUSE STRUCTURAL DAMAGE OR PERSONAL INJURY 17 Repeat step 11 Verify that the same valve operates first and that it operates within the correct pressure range i e 5 50 0 1 0 15 psid 18 Depressurize cabin at a rate not exceeding 1 500 fpm 19 Remove instrument line connector and pressurization outlet connections installed in steps 5 thru 7 Plug 1 4 inch fitting i...

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Page 313: ...PAGE 1 Feb 28 07 2D11 21 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Cabin Heat Defroster and Fresh Air System Figure 1 HEATING ...

Page 314: ...e two inch diameter bleed air tube at the firewall 4 Secure heat exchanger selector valve assembly brackets to mounting brackets on baggage compartment skin with four bolts and washers 5 Connect cabin pressure control cable and bleed air dump cable to air selector valve heat exchanger assembly 6 Attach flexible hose to bleed air supply manifold part of heat exchanger selector valve assembly and ti...

Page 315: ...changer 2 Remove plenum B Installation 1 Seal plenum to heat exchanger with RTV 106 sealant 2 Install plenum to heat exchanger with twelve screws 5 Defroster A Removal 1 Remove closeout panel covering magnetic float compass and windshield defroster by removing compass deviation and removing screw securing deviation card holder and close out panel 2 Remove the four screws and nylon spacers securing...

Page 316: ...lts and hardware 3 Tighten bleed air flexible hose band clamps 4 Connect control linkage to shutoff valve 5 Check rigging of shutoff valve 7 Auxiliary Cabin Heater A Removal 1 Loosen clamps attaching flex adapter to aft side of blower 2 Slide adapter forward over blower 3 Remove the six bolts attaching cabin air supply tube and auxiliary heater to forward pressure bulkhead 4 Disconnect electrical ...

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Page 319: ...The condenser is located in the aft fuselage Air is drawn through the condenser and vented overboard by means of a blower and duct The manifold assembly incorporates high and low service ports a high pressure switch and a low pressure switch that control the condenser head pressure by engaging or disengaging the compressor via a magnetic clutch The air conditioning system uses refrigerant HFC 134a...

Page 320: ...ubbles bubbles disappear Check or foam system for leaks Damaged compressor valves Replace compressor or dirt under valves Damaged compressor Worn Replace compressor or broken piston or piston rings Low suction pressure Low air supply through Repair blower or blower Accompanied by icing evaporator motor Clean stoppage in evaporator air ducts Very dirty evaporator fins Clean and flush with water and...

Page 321: ...ad Replace fuse Open circuit breaker Reset circuit breaker Broken or disconnected Check all terminals for electrical wire loose connections check wiring for hidden breaks Broken or disconnected Check ground wire to see if ground wire loose broken or disconnected Clutch coil burned out or Check current flow to disconnected clutch replace if inoperative Thermostat sensing element Check thermostat an...

Page 322: ...cessary receiver dehydrator or expansion valve plugged hose or coil System will not produce sufficient cooling Electrical Blower motor sluggish in Remove blower motor for operation service or replacement Mechanical Compressor clutch slipping Remove clutch assembly for service or replacement Obstructed blower passage Examine entire passage for obstruction Correct as necessary Insufficient air circu...

Page 323: ...Replace receiver dehydrator Excessively noisy system Mechanical Loose or excessively worn Tighten or replace as drive belt required Noisy clutch Remove clutch for service or replacement as necessary Compressor noisy Check mountings and repair remove compressor for service or replacement Compressor oil level low Fill with correct amount of specified oil Electrical Defective winding or Replace or re...

Page 324: ...PAGE 6 Feb 28 07 2D22 21 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Air Conditioning System Figure 1 ...

Page 325: ...old assembly All normal air conditioning service should be performed at the manifold assembly mounted valves NOTE Service valves are also located on the compressor in S N s 4636001 thru 4636186 only However use of these valves in servicing is not recommended NOTE In S N s 4636001 thru 4636186 only the service valves are screw on type Schrader valves In S N s 4636187 and up the service valves are q...

Page 326: ...PAGE 8 Feb 28 07 2D24 21 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Service Valves Figure 2 ...

Page 327: ...E For each 1 000 feet of elevation above sea level the gauge readings will be about one inch of mercury or 1 2 psi higher than the chart indicates It must be pointed out that the actual temperature of the air passing over the coils of the evaporator will be several degrees warmer than the fins allowing for a temperature rise caused by the loss in the fins and tubing of the evaporator The importanc...

Page 328: ...ading psi F 0 21 5 27 2 4 15 0 15 4 5 10 2 9 10 1 2 4 4 11 2 4 6 0 12 3 6 8 4 13 4 8 10 7 14 6 10 12 11 15 8 12 14 14 17 1 14 16 17 18 3 16 18 20 19 7 18 20 22 21 20 22 25 22 4 22 24 28 23 1 23 26 30 23 8 24 28 33 24 6 25 30 35 25 3 26 32 37 26 1 27 34 39 26 8 28 36 41 27 6 29 38 43 28 4 30 40 45 29 2 31 42 47 30 32 44 49 30 9 33 46 51 31 7 34 48 53 32 5 35 50 54 33 4 36 55 58 34 3 37 60 62 35 1 3...

Page 329: ... WITH THE PRESSURE AND THE REFRIGERATION EFFECTS OF THE RELEASE AND SUBSEQUENT EVAPORATION OF THIS PRESSURIZED LIQUID WARNING WEAR SUITABLE EYE PROTECTION WHEN HANDLING REFRIGERANT DUE TO THE POSSIBILITY OF FREEZING OF THE EYE IF CONTACTED BY ESCAPING LIQUID REFRIGERANT IF LIQUID REFRIGERANT DOES STRIKE THE EYE THE FOLLOWING ACTIONS SHOULD BE TAKEN 1 DO NOT RUB THE EYE 2 Splash large quantities of...

Page 330: ...HE APPROPRIATE REFRIGERANT OIL INTO A SYSTEM WARNING KEEP REFRIGERANT OIL CONTAINERS TIGHTLY SEALED AND CLEAN TO PREVENT ABSORPTION OF MOISTURE OR OTHER CONTAMINATION WARNING NEVER REUSE OIL REMOVED FROM THE SYSTEM DISCARD IT CAUTION WHEN LOCTITE REFRIGERANT SEALANT HAS BEEN USED ON A JOINT IT MUST BE HEATED TO 400 F PRIOR TO DISASSEMBLY LOCTITE MUST BE USED TO SEAL ANY PIPE THREADS IN THE SYSTEM ...

Page 331: ...imilar charging stand recovery station see Figure 3 Required only if the system contains refrigerant NOTE The term Discharge as used throughout this section in no sense implies or suggests discharging refrigerant to atmosphere In all cases when discharging an environmentally approved refrigerant recovery station is to be used a Gain access to service valves by removing rear access panel b Remove p...

Page 332: ...om of the rear side of the charging station until separator is empty j Close the oil drain valve Dispose of collected oil in an environmentally accepted manner Return collection bottle to its place on the charging stand k Plug unit into a proper voltage outlet Turn MAIN POWER switch ON l Press the RECOVER key on charging station keypad m To assure complete recovery of refrigerant a Wait 5 minutes ...

Page 333: ...the system p To enter diagnostic mode simultaneously press the SHIFT RESET and ENTER keys To display amount of refrigerant recovered by the unit press the 3 key The panel display will read the amount of recovered refrigerant in pounds or kilograms q Simultaneously press the SHIFT RESET and ENTER keys to clear internal counter Press SHIFT RESET to return to the main menu Kent Moore J23500 Charging ...

Page 334: ...move the protective caps from the high and low side service ports on the manifold assembly 3 Close all valves on the charging stand 4 Remove the protective cap from the vacuum pump outlet 5 Connect the blue and red hoses to the service ports see Figures 1 and 2 6 Start the vacuum pump 7 Open the valve on the vacuum pump Open the low pressure control valve and the vacuum control valve on the chargi...

Page 335: ...th quick disconnect connections open coupler valves 5 Open blue low side valve 1 on unit s control panel 6 Open both the red GAS vapor valve and the blue LIQUID valve on the tank 7 Program the length of evacuation time a Press the VACUUM key on control panel key pad b Display will show unit is in VACUUM mode c Refer to operator s manual for further detail 8 Enter the required time in minutes and s...

Page 336: ...PAGE 18 Feb 28 07 2E10 21 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Charging Hookup Figure 5 ...

Page 337: ... procedure is completed 9 If there is a pressure drop find leak s by applying a soap solution to all connections 10 Rework system as required to stop leaks and repeat Leak Check Procedure b Using HFC 134a PIR PPS50003 4 Rev A A leak may be located while a charging stand is hooked up to the system as follows 1 Ensure that there is at least one pound of refrigerant in the charging cylinder 2 Open th...

Page 338: ... valve 11 and the high pressure control valve 10 6 Allow the correct amount of refrigerant to enter the high side of the system 7 Close the high pressure control valve 10 and the refrigerant control valve 11 8 Perform Post Charging Operational Check below b Using a Robinair 34700 charging station or equivalent See Figures 3 and 6 CAUTION THE FOLLOWING PROCEDURE APPLIES TO ROBINAIR 34700 OR SIMILAR...

Page 339: ...OW PRESSURE CHARGING LINE BLUE ROBINAIR MODEL 34700 STATION LOW SIDE VALVE 1 HIGH SIDE VALVE 2 CHARGING VALVE VACUUM PUMP PROTECTION SWITCH RECOVERY PRESSURE SWITCH AUTOMATIC EXPANSION VALVE RECYCLING VALVE RECOVERY VALVE VACUUM SOLENOID VACUUM PUMP OIL SEPARATOR HEAT EXCHANGER MOISTURE INDICATOR AIR PURGE SERVICE PORT OIL DRAIN VALVE HIGH PRESSURE SWITCH FILTER DRIER FAN OIL DRAIN BOTTLE RECOVERY...

Page 340: ...T A QUALIFIED PERSON IS AT THE CONTROLS OF THE AIRPLANE ENSURE AIRPLANE IS HEADED INTO WIND 2 Activate the system and operate the engine at 1 000 rpm for 2 minutes Then operate the engine at 2 000 rpm for 2 minutes 3 Check the sight gauge on the receiver dehydrator during the engine operation at 1 000 and 2 000 rpm Any indication of bubbles passing the sight gauge indicates that additional refrige...

Page 341: ...he system and operate the engine at 1 000 rpm for 2 minutes Then operate the engine at 2 000 rpm for 2 minutes 4 Check the sight gauge on the receiver dehydrator during the engine operation at 1 000 and 2 000 rpm Any indication of bubbles passing the sight gauge indicates that additional refrigerant is required 5 If additional refrigerant is required add it slowly through the low pressure control ...

Page 342: ...PAGE 24 Feb 28 07 2E16 21 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Test Gauge and Manifold Set Figure 7 ...

Page 343: ...Start the vacuum pump e Open the low side manifold set hand valve The low side gauge should show a vacuum f After five minutes of pump operation the high side gauge should indicate slightly below zero If it does not stop the pump and eliminate the blockage in the system by replacing the faulty component then repeat the previous evacuation steps g Operate the vacuum pump for fifteen minutes or unti...

Page 344: ...PAGE 26 Feb 28 07 2E18 21 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Manifold Set Operation Figure 8 ...

Page 345: ...PAGE 27 Feb 28 07 2E19 21 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Leak Test Hookup Figure 10 Evacuation Hookup Figure 9 ...

Page 346: ...harging the System This method is the least desirable due to the requirement of operating the airplane s engine to run the compressor CAUTION ASCERTAIN THAT THE AREA AROUND THE AIRPLANE IS CLEAR AND THAT A QUALIFIED PERSON IS AT THE CONTROLS OF THE AIRPLANE a Keep the system under the vacuum established during the evacuating procedure with both hand valves in the closed position Disconnect evacuat...

Page 347: ...ring operation at 1 000 and 2 000 rpm Any indication of bubbles passing the sight gauge indicates that additional refrigerant is required c Add additional refrigerant slowly through the low side manifold set hand valve until the sight glass remains free of bubbles d Close the low side hand valve and refrigerant container valve e With the engine operating at 1 000 to 1 500 rpm the gauges should ind...

Page 348: ...ntact Sanden International for special tools and instructions for detailed compressor maintenance Refer to the Vendor List in the Introduction Section for the address and phone number CAUTION AN IMPORTANT FACTOR IN AIR CONDITIONING SERVICING IS CLEANLINESS TAKE CARE TO PREVENT DIRT OR FOREIGN MATERIAL FROM ENTERING THE SYSTEM ALL HOSE AND TUBING ENDS SHOULD BE CAPPED IMMEDIATELY ANY LUBRICATION RE...

Page 349: ...heir respective fittings e Install engine baffles f Evacuate and charge the system per instructions given above 4 Checking Compressor Oil Level Whenever a system component has been replaced or there is an obvious leak use the following procedure to check the compressor oil level after making necessary repairs a Run compressor for 10 minutes at engine idle rpm b Recover all refrigerant from the sys...

Page 350: ...l the oil filler plug first checking that the sealing O ring is not twisted Ensure that the seat and O ring are clean l Torque the plug from 6 to 9 foot pounds 0 8 to 1 2 kg m Do not over tighten the plug to stop a leak If plug leaks remove it and install a new O ring m Recharge the system per Servicing the System Charging above 5 Adjustment of Drive Belt Tension NOTE An alternate method of checki...

Page 351: ...ewall the hoses are routed underneath the battery underneath the left cabin floor back to the manifold assembly receiver dehydrator and evaporators From these components the lines continue back to the condenser NOTE Before any of the hose couplings are uncoupled the system must be completely discharged CHART 7 SANDEN SD 505 COMPRESSOR MOUNTING ANGLE OIL LEVEL Mounting Angle Degree Acceptable Oil L...

Page 352: ...uct to the lower outboard side of the blower d Connect the refrigerant lines to the inboard side of the evaporator e Charge the system J Expansion Valve NOTE If this part is not serviceable it must be replaced with a new part 1 Removal The expansion valves are located on the upper inboard corners of the evaporator assemblies between the receiver dehydrator and the evaporator inlet a Remove the nec...

Page 353: ...tall the bolts washers screws and nuts c Secure the lower end of the duct to the fuselage skin with the screws d Reconnect the lines to the condenser NOTE Whenever the air conditioning system has been open to the atmosphere it is recommended that the receiver dehydrator be replaced e Evacuate and recharge the system per instructions in this section f When the system is completely charged check it ...

Page 354: ...ct the two refrigerant lines to the top of the receiver dehydrator c Secure the receiver dehydrator to its mount by tightening the two clamps around the receiver hydrator body d In S N s 4636187 and up connect wiring to receiver dehydrator mounted pressure switches e Service the air conditioning system N Manifold Assembly The manifold assembly is located behind the receiver dehydrator and is mount...

Page 355: ...orporated into a single housing and are located on the receiver dehydrator In either case they control the system pressure by energizing or de energizing the compressor clutch 1 Removal a Discharge the air conditioning system into an appropriate environmentally approved refrigerant recovery station b Gain access to the manifold assembly or receiver dehydrator c Remove the electrical connections fr...

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Page 359: ...ve the four bolts that attach the cabin air temperature valve to the air selector valve through the firewall 5 Remove the valve from the airplane B Installation 1 Position the cabin temperature control valve in place 2 Attach the cabin temperature control valve to the air selector valve through the firewall with four bolts Ensure that the gasket is installed between the valves and firewall 3 Attac...

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Page 361: ...2F11 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 22 AUTOFLIGHT ...

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Page 363: ...eb 28 07 22 Table of Contents 1 Feb 28 07 2 Feb 28 07 22 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 19 Feb 28 07 20 Feb 28 07 21 Feb 28 07 22 Feb 28 07 23 Feb 28 07 24 Feb 28 07 25 Feb 28 07 26 Feb 28 07 CHAPTER ...

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Page 365: ...3 Post Maintenance Operational Checkout 8 2F24 Components 11 2G3 Panel Mounted Components 11 2G3 Component Locator 11 2G3 Trim Monitor 11 2G3 Removal 11 2G3 Installation 11 2G3 Roll Servo 12 2G4 Removal 12 2G4 Installation 12 2G4 Pressure Transducer 14 2G6 Removal 14 2G6 Installation 14 2G6 Trim Servo 14 2G6 Removal 14 2G6 Installation 16 2G8 Yaw Servo 18 2G10 Removal 18 2G10 Installation 18 2G10 ...

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Page 367: ...on for this system only is provided herein 2 S TEC System 55 55X A S TEC System 55 2000 This system was adopted in 2000 and is installed as standard equipment in S N s 4636160 4636248 thru 4636313 only B S TEC System 55X 2002 and up This system was adopted in 2001 and is installed as standard equipment in S N s 4636314 and up NOTE No model year 2001 PA 46 350P airplanes were built NOTE In S N s 46...

Page 368: ...K TRIM MASTER SW RED BLK RED TRIM CB PILOT S CONTROL WHEEL WHT P1 37 P1 36 TO A C GND P1 32 P1 33 P1 35 P1 34 OPTIONAL WHT Y AW MASTER Y AW MASTER Y1 Y1 101349 H 101486 E 104585 NEW E A B A P RAD STEERING HORIZON ANNUNCIATOR ANNUNCIATOR STR HRZ 12 PIN MOLEX PROG COMP A P RAD F D 2 BLK TO A C GND YAW MASTER SWITCH YAW POTENTIOMETER PROGRAMMER COMPUTER TRIM MONITOR 39237 4 OR 39328 4 39236 4 IN S N ...

Page 369: ...VO CO PILOT CONTROL WHEEL 30D05 DIODE BLK BLK WHT WHT BLK WHT ROLL SERVO TRIM SERVO UP 0121 CO PILOT CONTROL WHEEL PILOT CONTROL WHEEL PB1 Y AW SERVO Y AW AMP A B TRIM RELAY T4 PITCH SERVO YAW SERVO YAW AMP ROLL SERVO TRIM SERVO PRESSURE TRANSDUCER INSTALLED WITH SINGLE SIDE EFIS OPTION ONLY NOT INSTALLED WITH SINGLE SIDE EFIS OPTION S TEC System 55 55X Autopilot Flight Director Installation Figur...

Page 370: ... SWITCH YAW POTENTIOMETER PROGRAMMER COMPUTER P551 A C BUS AP C B 5 AMP Y1 J553 P553 BLK E BLU D GB3A LB2 WHT P555 BLK GB3A B TRIM MONITOR HORN TRIM MONITOR TRIM MASTER SWITCH J JB1 N WHT BLU C LB2 BLK GB3A A JB1 PROG COMP PILOT S CONTROL WHEEL RED J564 P564 TRIM MONITOR J565 J565 RED BLK GB3A D 3 3 P1E J1E A C BUS PRESSURE TRANSDUCER P557 TRANSDUCER CONTROL WHEEL TRIM 2 AMP C B A C BUS A B 105129...

Page 371: ...VO ROLL SERVO ROLL SERVO P562 P318 P418 YAW SERVO 0121 YAW AMP P460 YAW AMP UP PITCH SERVO GB3A P554 P BLK P567 RELAY PILOT CONTROL WHEEL H GB4A STALL WARN TRIGGER P561 P566 CO PILOT CONTROL WHEEL G JB14 P461 PILOT CONTROL WHEEL CO PILOT CONTROL WHEEL PITCH SERVO A B S TEC System 55 55X Autopilot Flight Director Installation Figure 1 Sheet 4 of 5 Effectivity 4636375 and up ...

Page 372: ... 6 Feb 28 07 2F22 22 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL S TEC System 55 55X Autopilot Flight Director Installation Figure 1 Sheet 5 of 5 Effectivity 4636160 4636248 and up ...

Page 373: ...te FAA certification with required test equipment and service data E GPSS System 55X only The Global Positioning System Steering GPSS is a function of the 55X autopilot only In the GPSS mode the converter receives ground speed and bank angle digital signals that are calculated and converted to a commanded turn rate The turn rate is then scaled and converted to a DC heading error signal that is com...

Page 374: ...ter ON OFF Switch ON 5 HDG and VS switches PRESS RELEASE Ensure that HDG and VS illuminate on the Fifty Five X annunciator 6 VS Knob ROTATE CW Pitch control i e the control yoke should move slowly out pilot may have to assist a heavy yoke 7 VS Knob ROTATE CCW Pitch control should move slowly in 8 A P DISC Trim Interrupt Switch on control yoke PRESS Verify the autopilot disconnects 9 HDG Mode ENGAG...

Page 375: ...uld run nose down 3 Move both segments of the Trim Command switch AFT Trim should run nose up b Re trim aircraft for takeoff and check controls for freedom of movement Be sure the autopilot and trim servos are dis engaged 15 Flight Director Test a Autopilot Master Switch SELECT FD Note the roll pitch and trim servos are disengaged The steering bar should be in view on the attitude indicator b HDG ...

Page 376: ... TURN COORDINATOR FD PARALLEX POTENTIOMETER ROLL SERVO TRIM SERVO YAW AMPLIFIER TRANSDUCER PITCH SERVO YAW SERVO FD PARALLEX POTENTIOMETER ROLL SERVO TRIM SERVO YAW AMPLIFIER ALTITUDE SELECTOR ANNUNCIATOR TRIM MASTER ANNUNCIATOR SWITCH HORN STEERING HORIZON TRIM MONITOR TURN COORDINATOR AFT PRESSURE BULKHEAD COMPONENTS NOT INSTALLED IN S N S 4636375 AND UP S N S 4636160 AND 4636248 THRU 4636374 TU...

Page 377: ... of the fwd most access panel in the cockpit floor at the co pilot s feet 1 Removal a Remove carpet to expose access panel b Remove screws holding access panel to floor and open access panel to expose trim monitor and autopilot harness c Disconnect autopilot harness d Remove screws 4 holding trim monitor to access panel and remove trim monitor 2 Installation a Place trim monitor in position on und...

Page 378: ...capstan and and tighten center ball setscrew as shown in Figure 3 g Replace cable guards and capstan cover secure with screws 4 h Position servo as shown in Figure 3 and install and secure nuts washers and bolts 4 ea holding servo to mounting brackets i Position cable clamps 2 as shown in Figure 3 and tighten nuts and bolts 2 ea Adjust cable clamps in or out along the aileron balance cable to obta...

Page 379: ...BELOW FOR BRIDLE CABLE WRAP INFORMATION LEFT FWD BULKHEAD F S 171 40 CHAFE BLOCK AILERON CABLE AILERON BALANCE CABLE PULLEY CABLE CLAMP L OF A C C AILERON BALANCE CABLE ADJUST AUTOPILOT BRIDLE CABLE TENSION TO 15 2 LBS BRIDLE CABLE WRAPPING DETAIL VIEW LOOKING UP CAPSTAN COVER AND CABLE GUARDS REMOVED FOR CLARITY LOCATION OF CENTER BALL WITH AILERONS IN NEUTRAL POSITION DEPRESS CENTER BALL TO BOTT...

Page 380: ...m both ends of the plastic tube d Slide the tube forward e Rotate the elevator trim control wheel until the right trim cable turnbuckle clears the aft end of the tube f Tie a pull rope to the right trim cable forward of the exposed turnbuckle g Tie a pull rope to the right trim cable aft of the idler pulley h Tie off both pull ropes to maintain tension on the left trim cable and the extreme forwar...

Page 381: ...LEY DETAIL MOUNTING PLATE IDLER PULLEY BULKHEAD F S 241 50 STAR WASHER MS35333 36 6 REQ D BOLT WASHER NAS1149C0632P CABLE GUARDS 3 REQ D BULKHEAD F S 249 60 VIEW LOOKING DOWN AT TRIM SERVO INSTALLATION BULKHEAD F S 241 50 TRIM SERVO C L OF A C WASHER NAS1149C0632P SCREW 3 REQ D BRACKET WASHER NAS1149F0363P TRIM SERVO BASEPLATE NUT NAS679A3W CAPSTAN COVER CABLE GUARDS 4 REQ D WASHER NAS1149F0363P 1...

Page 382: ...ble forward of the trim servo and capture the trim cable in the left cable groove on the bottom of the idler pulley h Slide the idler pulley along the trim cable underneath the servo capstan and bring it approximately to its installed position see Figure 4 At this point the forward portion of the trim cable should be routed under around the rear and over the top of the idler pulley and under aroun...

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Page 384: ...e capstan cover and cable guards from servo d Adjust yaw servo clutch torque per Servo Clutch Torque Adjustment below e Wrap autopilot bridle cable align capstan and and tighten center ball setscrew as shown in Figure 5 f Replace cable guards and capstan cover secure with screws 4 g Position yaw servo as shown in Figure 5 and secure with bolts nuts and washers 4 ea h Remove tape or clip holding br...

Page 385: ...EQ D CABLE CLAMP 2 REQ D BULKHEAD F S 282 00 RUDDER PULLEYS OMITTED FOR CLARITY VIEW DOWN AND AFT EA YAW SERVO VIEW EA EA LOOKING LEFT SEE DETAIL BELOW FOR BRIDLE CABLE WRAP INFORMATION EA L OF AIRCRAFT C FWD UP ADJUST BRIDLE CABLE TENSION PER NOTE 1 RIGHT RUDDER CABLE LEFT OMITTED FOR CLARITY CABLE GUARDS CAPSTAN COVER RIGHT RUDDER CABLE LEFT RUDDER CABLE NOTE 1 SYSTEM 55 S N S 4636160 AND 463624...

Page 386: ...with attached bridle cable 2 Installation a Rig elevator controls per Elevator Controls Rigging 27 30 00 b Remove screws 4 and remove capstan cover and cable guards from servo c Adjust pitch servo clutch torque per Servo Clutch Torque Adjustment below d Wrap autopilot bridle cable align capstan and and tighten center ball setscrew as shown in Figure 6 e Replace cable guards and capstan cover secur...

Page 387: ...636248 THRU 4636313 ONLY 15 2 LBS SYSTEM 55X S N S 4636314 AND UP 30 2 LBS EXISTING ELEVATOR CABLE 311 00 F S TURNBUCKLE LOCKING CLIP MS21256 1 2 REQ D FWD UP EXISTING PITCH CABLE COTTER PINS INSTALLED AS CABLE GUARDS 2 PLCS CLEVIS PIN 2 REQ D WASHER NAS1149F0363P 4 REQ D COTTER PIN MS24665 134 2 REQ D CUT TO LENGTH BRIDLE CABLE WRAPPING DETAIL CAPSTAN COVER AND CABLE GUARDS OMITTED FOR CLARITY WR...

Page 388: ... for correct operation d Replace and secure the aft fuselage access panel 3 Post Installation Ground Checks a Level aircraft laterally per 8 20 00 b Center trim pot on instrument panel c Align the cap on the yaw trim pot knob on instrument panel so that the white line is centered vertically d Adjust the pot in the yaw amplifier located under plug in top of amplifier to provide a null i e no servo ...

Page 389: ...able D Check capstan torque by attaching the capstan adjusting tool special tool see parts catalog to the capstan and using a currently calibrated torque wrench as shown in Figure 8 1 Acceptable torque is specified in Chart 1 2 If adjustment is required proceed as follows E Remove cotter pin from end of servo shaft and remove castle nut shim washers and tension washers F Replace tension washers as...

Page 390: ...6 101349 S TEC TOOL SEE PARTS CATALOG SCREW 4 REQ D CABLE GUARD 4 REQ D SHIM WASHER MIN 1 REQ D USE AS REQUIRED TO ALIGN COTTER PIN WITH SHAFT HOLE SERVO CAPSTAN COVER TORQUE WRENCH CASTLE NUT AN320 5 COTTER PIN MS24665 134 WASHER 4 REQ D AN936 A4 TENSION WASHERS SEE CHART 1 Servo Clutch Torque Adjustment Figure 8 ...

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Page 393: ...2G19 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 23 COMMUNICATIONS ...

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Page 395: ...23 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 23 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 23 Table of Contents 1 Feb 28 07 2 Feb 28 07 23 00 00 1 Feb 28 07 2 Feb 28 07 23 50 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 23 60 00 1 Feb 28 07 2 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 397: ... TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO GENERAL 23 00 00 1 2H1 Avionics Master Switch 1 2H1 Ground Clearance Switch 1 2H1 AUDIO INTEGRATING 23 50 00 1 2H3 Removal and Installation 1 2H3 System Functional Test 2 2H4 On Ground 2 2H4 In Flight 2 2H4 Adjustment 3 2H5 STATIC DISCHARGING 23 60 00 1 2H9 Static Wicks 1 2H9 ...

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Page 399: ...s via the avionics master solenoids which in turn are energized by the avionics master switch Refer to Chapter 24 and to schematics in 91 24 30 2 Ground Clearance Switch Optional The ground clearance switch furnishes power to the Comm 1 and speaker panel direct from the battery bus through the ground clearance relay Refer to 91 23 00 for schematic interface and troubleshooting ...

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Page 401: ...PECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT MAY RENDER THE AIRCRAFT UNAIRWORTHY SEE INTRODUCTION SUPPLEMENTARY PUBLICATIONS The Garmin GMA 340 Audio Panel is installed as standard equipment in S N s 4636248 and up It integrates the audio switching amplifier and intercom system with a marker beacon receiver Maintenance of the GMA 340 is on condition only and with the exception of swapping ...

Page 402: ... are loud and clear and push to talk PTT operation is correct 4 Intercom System ICS Check a Set the intercom to the ALL mode Crew and Pilot LED s off b Plug in headsets at each ICS position c Adjust squelch and volume for each position and verify that the ICS is working properly d Check Pilot and Copilot ICS positions for isolation and proper operation of volume and squelch controls e Press the PA...

Page 403: ...h access holes in the top cover of the GMA 340 A Marker beacon audio level Counter clockwise adjustment increases the marker audio level B Marker beacon sensitivity Clockwise CW adjustment increases the sensitivity LOW sensitivity can be adjusted without affecting HIGH sensitivity setting Adjusting HIGH sensitivity will however affect the LOW sensitivity If the HIGH sensitivity setting is adjusted...

Page 404: ...A MIC SPKR LEVEL CO PILOT PA MIC SPKR LEVEL AIRCRAFT RADIO SPKR LEVEL MUSIC 1 MUTE TRIP LEVEL NOT USED IN THIS INSTALLATION MARKER BEACON AUDIO LEVEL MARKER BEACON LOW SENSITIVITY MARKER BEACON HIGH SENSITIVITY FRONT VIEW LOOKING DOWN Effectivity GMA 340 Audio Panel Adjustments 4636248 and up Figure 3 ...

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Page 407: ... the rudder and one in the center of the elevator trim tab To aid in dissipating static electricity buildup the ailerons elevator and rudder are bonded to either the control s hinge or spar When replacing the jumper assemblies bonding straps secure the end of the jumper that mounts to the control s hinge or spar as follows see also 51 80 00 A Clean an area of 1 1 2 times the diameter of the jumper...

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Page 409: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL 2H11 CHAPTER 24 ELECTRICAL POWER ...

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Page 411: ...00 1 Feb 28 07 2 Feb 28 07 24 30 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 19 Feb 28 07 20 Feb 28 07 21 Feb 28 07 22 Feb 28 07 24 40 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 24 60 00 1 Feb 28 07 2 Feb 28 ...

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Page 413: ...12 2I6 Troubleshooting 12 2I6 Removal 12 2I6 Installation 15 2I9 Cleaning 15 2I9 Battery 15 2I9 Acid Recovery Jar and Vent Lines 15 2I9 Charging Gill Model G 243 16 2I10 Hydrometer Reading and Battery Charge 17 2I11 Discharge 18 2I12 Temperature Considerations 18 2I12 Repairs Storage and Service Tips 19 2I13 Preparing New Dry Charged Battery for Installation 19 2I13 Battery Valve Regulated Lead Ac...

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Page 415: ...rd E Dual main power distribution bus tie bus standard F One 10 amp hour lead acid battery manifold type Gill S N s 4636001 thru 4636374 standard One 10 amp hour lead acid battery recombinant gas type Gill S N s 4636375 and up standard G One acid recovery jar with venting overboard S N s 4636001 thru 4636374 standard H External power provisions standard I Visual annunciation with alternator OUT se...

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Page 417: ...TO MAKE THIS ADJUSTMENT Voltage regulation and control is provided for both alternators by Lamar solid state alternator control units that regulate voltage through control of field voltage and automatic overvoltage protection The only adjustment is the voltage adjust potentiometer located under the removable cover plug System voltage should be set at 28 5 Vdc maximum Should an overvoltage conditio...

Page 418: ...ster switch voltage regulator and alternator field terminal Interruption of voltage through any of these points isolates the faulty component or wire which must be replaced See wiring schematic Chapter 91 Open output circuit With the battery switch turned on check for battery voltage from the airplane s main bus through the entire output circuit to the alternator battery post Measure voltage from ...

Page 419: ... slowly by hand turning alternator rotor through 360 of travel If resistance is high check brushes for spring tension and excessive wear and replace if necessary If brushes are okay and field reads open replace alternator Shunt load resistor 5 amp Replace fuse after fuse open continuity check to ground Output indicated on Faulty voltage Start engine turn on load ammeter does not meet regulator ref...

Page 420: ...of deterioration at crimp or strands of broken wire at crimp Tighten any loose binding posts or replace bad wire terminals Open rectifier If any of the rectifiers of the alternator open up internally it will result in a definite limitation on the current that can be drawn from the alternator After having checked the previous causes of low output it can be assumed that a faulty rectifier exists Fie...

Page 421: ...o obvious signs of a physical short circuit at field terminal or brush holder replace alternator NOTE Intermittent short circuit Internal short circuiting of the field can occur at various positions of the rotor therefore reconnect field reset breaker CAUTION TURN MAGNETO SWITCH TO OFF BEFORE TURNING PROP Pull propeller slowly by hand turning alternator rotor through 360 of travel Observe circuit ...

Page 422: ...meter fluctuation High field circuit If problem persists jump continued resistance across the terminals of the following components one at a time until the faulty unit is isolated a Field 5 amp alternator circuit protector b Alternator switch c Overvoltage relay Defective voltage Replace voltage regulator regulator Faulty grounds Completely clean all corrosion from grounding points ...

Page 423: ...onditioner Power Alternator 1 Master Switch Alternator 2 Master Switch 3 A 15 A 3 A 60 A 60 A 70 A 70 A 80 A 1 A 70 A 5 A 1 A 5 A 40 A Voltage Regulator 1 Low Voltage Monitor LO BUS VOLTS Annunciator Panel ALT 1 INOP Annunciator Panel M M Voltage Regulator 2 ALT 2 INOP Annunciator Panel Alternator 1 F2 F1 AUX Shunt 5 A 5 A F2 F1 AUX Shunt 5 A 5 A A339A Ammeter BRT DIM Bright Dim Relay Volt Meter A...

Page 424: ...vidual electrical load of each alternator Should an overvoltage condition occur in either alternator its voltage regulator will shut off the field winding voltage of that alternator thus overvoltage relays are not required When either alternator fails or is selected OFF the appropriate ALTERNATOR INOP annunciator light will illuminate A Alternator Belt Tension 1 If properly installed tensioned and...

Page 425: ...ower Pure dc regulated power supply A 28 8V 5A Adjustable 6 12V power supply B 0 05A Resistors R1 1 R2 650 fine adjustment R3 7 2 dummy load 4A Ammeter 0 5A dc Voltmeters Precision meter between pins 1 and 8 between pin 3 and power B ground 50 MV precision meter between shunts at pins 6 and 7 Switch Between R1 and R2 Indicator 28V light Mazda 1829 or equivalent 3 Set up load resistance as follows ...

Page 426: ...Figure 2 c Equalizer Test 1 Apply voltmeter at pins 5 and 8 equalizer and ground Equalizer voltage should read 5 75 V 0 1 V NOTE Equalizer voltage outside 5 65 5 85 V limits may still be acceptable because of meter calibration differences and temperature If error is several times the stated 0 1 V tolerance have the unit rechecked by a fully equipped test facility 2 Set R2 for maximum resistance 65...

Page 427: ... R3 and switch 2 2 Open switches 1 and 2 Set power supply B at 11 V 3 Set power supply A at 31 8 V Depress PTT and hold for 5 seconds No activation should occur 4 Increase power A to 32 2 V Depress PTT Relay should activate almost instantly 5 Close switch 2 Increase power to 33 8 V Depress PTT for 5 seconds No activation should occur 6 Increase power to 34 5 V Depress PTT Relay should activate alm...

Page 428: ...y 100 hour inspection A Troubleshooting See Chart 2 B Removal 1 Remove battery access plate from floor of forward baggage compartment CAUTION REMOVE NEGATIVE CABLE FIRST BEFORE EXPOSING AND LOOSENING POSITIVE TERMINAL WING NUT TO AVOID SHORT CIRCUITS AND ELECTRICAL BURNS 2 Pull back rubber battery terminal boots loosen wing nuts and disconnect battery cables 3 Remove vent hose at battery manifold ...

Page 429: ...not hold charge Battery worn out Replace battery Standing too long Remove and recharge battery if left in unused airplane one week or more Equipment left ON Remove and recharge accidentally Impurities in electrolyte Replace battery clean and recharge acid recovery jar Short circuit ground Check wiring in wiring Broken cell partitions Replace battery clean and recharge acid recovery jar Battery lif...

Page 430: ...er added and battery Always recharge battery not charged immediately at least 1 2 hour when adding water in freezing weather Leaking cell Replace battery Clean and recharge acid recovery jar Battery polarity reversed Connected backwards on Battery should be slowly airplane or charger discharged completely and then charged correctly and tested Battery consumes Cracked jar one cell only Replace batt...

Page 431: ... solution to enter any cells b Wash entire battery with clear water and dry thoroughly c Wash down the battery support and floor area hold down supports connectors and cable ends with a soda solution followed by clear water Dry entire area and component parts thoroughly Apply fresh acid resistant paint if required 2 Acid Recovery Jar and Vent Lines a Visually inspect all vent lines for kinks crack...

Page 432: ... 2 Check that the electrolyte level in each cell is at the bottom of the split ring 3 A hydrometer check of each cell should be accomplished See Hydrometer Reading and Battery Charge below 4 It is recommended that vent caps be left on the battery while charging In addition a wet cloth should be placed over the vent caps within the manifold 5 The battery may be charged at any rate in amperes not to...

Page 433: ...nd electrolyte will not be mixed giving a false reading Temperatures different from the established norm will effect the hydrometer readings Refer to Chart 3 for the temperature corrections Specific gravity values for a fully charged battery are shown in Chart 4 To adjust low specific gravity charge the battery see Charging above until it is gassing and until the specific gravity rises no higher o...

Page 434: ...emselves Recommended discharge rates are listed in Chart 5 H Temperature Considerations Operation of storage batteries beyond their ambient temperature or charging voltage limits will result in excessive cell temperatures leading to electrolyte boiling rapid deterioration of the cell and finally battery failure The relationship between the maximum charging voltage and the number of cells in the ba...

Page 435: ... FOLLOW THE PREPARATION INSTALLATION INSTRUCTIONS FURNISHED WITH THE BATTERY BY TELEDYNE The Teledyne dry charged Model GILL G 243 Battery shall be stored as received from Teledyne Do not remove vent seals add acid nor attempt to charge a dry charged battery until the time arrives to install the battery into an airplane 9 Battery Valve Regulated Lead Acid Gill Model G 250S S N s 4636375 and up Gil...

Page 436: ...HARGING AREA SHOULD BE VENTED TO THE OUTSIDE AIR TO PREVENT HYDROGEN GASSES FROM BEING CIRCULATED THROUGHOUT THE BUILDING The National Electric Code forbids charging batteries installed in aircraft or within 10 feet of fuel tank areas The battery must be removed from the aircraft for charging Further an aircraft battery should not be allowed to deteriorate to the point where safety of flight is je...

Page 437: ...oltage The battery is considered airworthy if it meets 80 of the 1 hour capacity rating minimum of 48 minutes to the cut off voltage If the battery fails to meet the minimum run time recharge using the constant potential method until charge current stabilizes this could take 10 to 24 hours Allow the battery to stand on open circuit for one 1 hour after recharging Repeat the above capacity test If ...

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Page 439: ...SCONNECT THE PLUG ONLY FROM THE PILOT S SIDE OF THE AIRPLANE C Start engine and move ground power unit well away from aircraft D Turn ON Battery Master Switch E Observe Ammeter indicates Alternator electrical power is available F With the alternator on line observe charging current on ammeters G Do not take off until charging current falls below 20 AMPS NOTE The aircraft battery must be removed fr...

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Page 443: ...N essential electrical equipment one unit at a time Essential electrical equipment may consist of C Turn Alternator No 2 ON turn Alternator No 1 OFF Check to be sure that all equipment that was supported by the No 1 Alternator is supported by the No 2 Alternator D If necessary the non essential bus and it s related equipment can be eliminated by pulling the non essential 70 amp circuit breaker on ...

Page 444: ...Cont 3 0 1 50 M Starter Contactor 1 Int 5 0 1 47 Motor 1 Int 185 0 M Annunciator Panel Lamps 1 Int 3 46 M Fuel Pump Motor 2 Int 5 4 0 M Hydraulic Pump Motor 1 Int 25 26 0 M Relay 1 35 35 Control 1 3 M Strobe Light Light 2 3 Int 5 4 0 M Landing Light Lamp 250W 1 Int 10 9 0 Relay 29 29 M Taxi Lights Lamps 50W 2 Int 5 1 75 Relay 1 M Position Lights Lamps 2 Cont 5 1 5 M Wing Inspect Ice Light Lamp 1 I...

Page 445: ...nverter Int 2 70 AVI Transicoil EMIS Quad Digital Indicator 2 1 Cont 3 14 Digital Indicators Enhanced Digital Indicator 3 1 Cont 3 14 AVI Transicoil EMIS Oil Pressure Oil Temperature 1 Cont 5 50 Analog Indicators 4 MAP 1 Cont 3 25 RPM 1 Cont 3 25 TIT 1 Cont 3 25 Fuel Flow 1 Cont 3 25 CHT 1 Cont 3 25 Fuel Quantity 1 Cont 5 50 AVI 1 KX 155A COMM NAV Cont 0 06 6 0 AVI 2 KX 155A COMM NAV Cont 0 06 6 0...

Page 446: ...r 50 when in cruise and 0 68 during takeoff and landing 3 Volt Ammeter The volt ammeter combination indicator consists of two ammeters and a volt meter mounted in one case The ammeters indicate amperage load on each alternator The voltmeter indicates total system voltage The best troubleshooting approach to determine this instruments condition is to compare the readings with a known good meter Sho...

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Page 449: ...2J11 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 25 EQUIPMENT FURNISHINGS ...

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Page 451: ...ffective Pages 2 Feb 28 07 25 Table of Contents 1 Feb 28 07 2 Feb 28 07 25 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 25 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 25 50 00 1 Feb 28 07 2 Feb 28 07 25 60 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 453: ...traint System 7 2J23 Inspection 7 2J23 Inertial Reel Adjustment 7 2J23 PASSENGER COMPARTMENT 25 20 00 1 2K3 Aft Facing Passenger Seats 1 2K3 Removal 1 2K3 Installation 1 2K3 Gas Spring Support 1 2K3 Removal 1 2K3 Installation 1 2K3 Forward Facing Passenger Seats 1 2K3 Removal 1 2K3 Installation 2 2K4 Cabinets 2 2K4 Conference Table 2 2K4 CARGO COMPARTMENTS 25 50 00 1 2K7 Aft Baggage Net 1 2K7 EMER...

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Page 455: ...back support b Remove seat back 3 To remove seat track plunger cable a Remove cotter pin washer and pin that secures cable yoke to track plunger actuating lever b Remove the clamps which secure the upper portion of the cable sheath to the bottom of the seat frame c Remove the cotter pin washer and pin that secure the remaining end of the cable to the plunger actuating arm d Remove the two clamps w...

Page 456: ...IRAGE MAINTENANCE MANUAL 50 00 05 Track Plunger Actuating Lever Cable Yoke Cotter Pin Washer and Pin Yoke VIEW A 89976 AD Bend end of spring as shown Put free end inside coils of spring Plunger Actuating Arm Pilot s Copilot s Vertically Adjustable Seats Typical Figure 1 ...

Page 457: ...nds Off position the seat plunger should be full down and locked into the seat track When the handle assembly is operated the seat plungers must retract sufficiently into the seat assembly to allow fore and aft movement of the seat along the seat tracks 2 Lumbar Support Refer to Figure 2 A Description The pilot and co pilot seats incorporate a Lumbar support feature The installation consists of an...

Page 458: ...ra Safe 279 112 Safe Care 193 051 Dupont 2319S Plastic Prep 279 081 Isopropyl Alcohol 179 918 2 Apply a layer of 3M Scotch Grip 2210 or Delta Laboratories Contact Adhesive B 10161 P N 179 853 cement to smooth side of bladder pad 3 Apply a layer of 3M Scotch Grip 2210 or Delta Laboratories Contact Adhesive B 10161 P N 179 853 cement to back side of bladder side away from inflation tube nipple 4 All...

Page 459: ...PAGE 5 Feb 28 07 2J21 25 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Lumbar Seat Bladder Installation Figure 2 ...

Page 460: ...e Care 193 051 Dupont 2319S Plastic Prep 279 081 Isopropyl Alcohol 179 918 2 Apply a layer of 3M Scotch Grip 2210 or Delta Laboratories contact adhesive B 10161 P N 179 853 cement to rough side of bladder pad 3 Apply a layer of 3M Scotch Grip 2210 or Delta Laboratories contact adhesive B 10161 P N 179 853 cement to seat back filler where bladder is to be located 4 Allow the adhesive to dry for 15 ...

Page 461: ...eel and in and out of the adjusting buckle If excessively worn replace c Check inertia reel mechanism by pulling sharply on strap Verify reel will lock in place under sudden stress B Inertial Reel Adjustment The inertial reel locking feature prevents the shoulder strap from extending and holds occupant in place For normal movement strap will extend and retract as required If required adust inertia...

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Page 463: ...PAGE 9 Feb 28 07 2K1 25 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 464: ...PAGE 10 Feb 28 07 2K2 25 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 465: ...e gas spring support 2 Installation a Place the gas spring support in position b Connect the lower end of the gas spring to its lower bracket with the washers if any pins and cotter pins c Connect the upper end of the gas spring to its upper support on the outboard side of the seat back with the bolt washer nut and cotter pin 2 Forward Facing Passenger Seats Not Shown A Removal 1 Remove the seat b...

Page 466: ...the channel b Slide the bolt into the aft holes in the channel placing on the bolt in order washer if required bushing aft fitting of seat back actuator roller washer if required and nut c Insert a pin in each side of the stop assembly and secure them with cotter pins d Secure the seat back release cover to the forward portion of the channel with the nut and bolt e Attach the cable assembly to the...

Page 467: ...PAGE 3 Feb 28 07 2K5 25 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Passenger Seats Aft Facing Figure 1 ...

Page 468: ...PAGE 4 Feb 28 07 2K6 25 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 469: ...gage net is secured to the F S 233 87 frame by four screws The upper edge of the baggage net is secured to two stud assemblies one on either side of the interior The studs are located slightly aft of the shoulder harness inertia reel for the aft seat In the stowed position the net may be rolled and left on the baggage floor at the base of the aft seat backs ...

Page 470: ...PAGE 2 Feb 28 07 2K8 25 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 471: ...ink to alert the pilot or maintenance personnel Should the ELT be activated accidentally it must be reset To reset 1 Position the remote cockpit switch to ON then immediately reposition it to ARM or 2 Position the switch on the ELT to ON then immediately reposition it to OFF B Battery Removal and Installation Refer to Figure 1 1 Disconnect and remove positive cable from battery 2 Remove ELT from t...

Page 472: ...PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL BOTTOM VIEW END CAP MOUNTING HOLES BATTERY COVER SCREWS FRONT VIEW ON OFF SIDE VIEW MOLEX CONNECTOR 3 6 9 12 2 5 8 11 1 4 7 10 Artex 110 ELT Figure 1 AFT PRESSURE BULKHEAD ELT ANTENNA ACCESS ELT ACCESS COVER ...

Page 473: ...X ELT 110 4 LIGHT RESET 1 RESET 2 EXTERNAL ON G SWITCH LOOP G SWITCH LOOP 1A 2 3 5 6 7 8 P203 COCKPIT PANEL SWITCH P401 P301 AFT PRESSURE BULKHEAD WH WH BLU 1 1 WH ORG WH GRN WH RED 2 6 3 7 2 6 3 7 20B 22 TO ELT SW PWR 20R 9 28 VDC GROUND WH WH BLU WH ORG WH GRN WH RED GROUND 20B Artex 110 ELT Wiring Schematic Figure 2 ...

Page 474: ...ithin the time period made up of the first five minutes after any hour 3 If the operational tests must be made at a time not included within the first five minutes after the hour the test should be coordinated with the closest FAA Tower or Flight Service Station CAUTION CONSULT FAA ADVISORY CIRCULAR AC 20 81 FOR DETAILED INFORMATION CONCERNING UNSHIELDED TESTING 4 Turn the airplane master switch O...

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Page 476: ...PAGE 6 Feb 28 07 2K14 25 60 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 477: ...2K15 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 26 FIRE PROTECTION ...

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Page 479: ...50P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 26 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 26 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 26 Table of Contents 1 Feb 28 07 2 Feb 28 07 26 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 CHAPTER SECTION PAGE DATE ...

Page 480: ...PAGE 2 Feb 28 07 26 LIST OF EFFECTIVE PAGES 2K18 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 481: ... 2K19 26 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 26 FIRE PROTECTION TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO EXTINGUISHING 26 20 00 1 2K21 Portable Fire Extinguisher 1 2K21 ...

Page 482: ...PAGE 2 Feb 28 07 2K20 26 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 483: ...he lever Maximum extinguishing effect is obtained if the fire fighter uses side to side motion and keeps moving in towards the base of the fire source as it is extinguished Releasing the lever closes a secondary seal inside the operating head This interrupts the flow of extinguishant thus retaining part of the charge for dealing with a flash back or re ignition should they occur without waste or l...

Page 484: ...50P MALIBU MIRAGE MAINTENANCE MANUAL FIRE EXTINGUISHER LOCATED INSIDE REFRESHMENT CENTER FWD FWD FS 152 00 FOAM GROMMET CABINET CABINET DOOR FIRE EXTINGUISHER A600 A A B B CABINET GROMMET FOAM VIEW A A VIEW B B Fire Extinguisher Locator Figure 1 Sheet 1 of 2 ...

Page 485: ...eb 28 07 2K23 26 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL FS 151 00 BL 0 0 ACCESS PANEL FWD FIRE EXTINGUISHER BRACKET MOUNTED ON FLOOR Fire Extinguisher Locator Figure 1 Sheet 2 of 2 ...

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Page 487: ...PART NUMBER 761 876 February 28 2007 3A1 AIRPLANE MAINTENANCE MANUAL CARD 3 OF 9 PA 46 350P S N s 4636001 AND UP PIPER AIRCRAFT INC ...

Page 488: ...3A2 Published by Technical Publications Piper Aircraft Inc 2926 Piper Drive Vero Beach Florida 32960 U S A Member General Aviation Manufacturers Association ...

Page 489: ...2 3 4 5 and 6 CR981223 December 23 1998 1 2 3 4 5 and 6 PR000201 February 1 2000 1 2 3 4 5 and 6 PR010515 May 15 2001 1 CR050730 July 30 2005 1 2 3 4 5 6 7 and 8 PR060207 February 7 2006 1 2 3 4 5 6 7 and 8 CR070228 February 28 2007 1 2 3 4 5 6 7 8 and 9 COMPLETE REVISION OF MAINTENANCE MANUAL 761 876 Revisions appear in all Aerofiche Cards Accordingly discard your entire existing Aerofiche Card S...

Page 490: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 1 Feb 28 07 AEROFICHE EFFECTIVITY 3A4 THIS PAGE INTENTIONALLY BLANK ...

Page 491: ...Feb 28 07 Intro Table of Contents 1 Feb 28 07 2 Feb 28 07 Introduction 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 Index 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHA...

Page 492: ...PAGE 2 Feb 28 07 INTRO LIST OF EFFECTIVE PAGES 3A6 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 493: ...A9 Effectivity 2 3A10 Serial Number Explanation 2 3A10 Assignment of Subject Material 2 3A10 Pagination 3 3A11 Aerofiche Effectivity 3 3A11 Identifying Revised Material 3 3A11 Indexing 3 3A11 List of Effective Pages 3 3A11 Warnings Cautions and Notes 3 3A11 Accident Incident Reporting 4 3A12 Supplementary Publications 4 3A12 Piper Publications 4 3A12 Vendor Publications 4 3A12 Chapter Section Inde...

Page 494: ...PAGE 2 Feb 28 07 3A8 INTRO CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 495: ...GENUINE PIPER AIRCRAFT PARTS OR PIPER AIRCRAFT APPROVED PARTS OBTAINED FROM PIPER APPROVED SOURCES IN CONNECTION WITH THE MAINTENANCE AND REPAIR OF PIPER AIRPLANES Genuine PIPER parts are produced and inspected under rigorous procedures to ensure airworthiness and suitability for use in PIPER airplane applications Parts purchased from sources other than PIPER even though identical in appearance ma...

Page 496: ...ane are broken down into subsystems These sub systems are identified by the second element of the standard numbering system The element 40 of the number 28 40 01 concerns itself with the indicating section of the fuel system C Unit Subject The individual units within a sub system section may be identified by the third element of the standard numbering system The element 01 of the number 28 40 01 i...

Page 497: ...his set 8 Identifying Revised Material A revision to a page is defined as any change to the printed matter that existed previously Revisions additions and deletions are identified by a vertical line i e change bar along the left hand margin of the page opposite only that portion of the printed matter that was changed A change bar in the left hand margin opposite the footer i e chapter section subj...

Page 498: ...s Catalog P N 761 878 2 Periodic Inspection Report Form P N 767 011 3 Progressive Inspection Manual 50 hour P N 767 013 B Vendor Publications WARNING FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION S WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT MAY RENDER THE AIRCRAFT UNAIRWORTHY 1 AIR CONDITIONING COMPRESSOR Vendor Address Sanden International USA Inc PH 972 442 8400...

Page 499: ...cialty Systems PH 330 374 3040 Goodrich Corporation FAX 330 374 2290 1555 Corporate Woods Parkway Uniontown Ohio 44685 8799 Technical Assistance PH 800 334 2377 330 374 3743 FAX 330 374 2290 Email dssd support goodrich com http www deicingsystems goodrich com Black Standard Pneumatic De Icer Installation Maintenance and Repair Manual ATA 30 10 31 SmartBoot System ATA 30 10 65 8 ELECTRONIC FLIGHT I...

Page 500: ...ntext See www avantext com or PH 800 998 8857 11 FIRE EXTINGUISHER PORTABLE Vendor Address H3R Inc PH 800 249 4289 43 Magnolia Ave 4 San Francisco California 94123 2911 http www h3r com index htm 12 FORCE APPLICATOR KIT Vendor Address Safe Flight Instrument Corp PH 914 946 9500 20 New King Street White Plains New York 10602 13 FUEL BOOST PUMP Vendor Address Parker Hannifin Corp PH 800 272 7537 Nic...

Page 501: ...ww unisonindustries com index4 html Installation Operation F1100 MASTER SERVICE MANUAL and Maintenance 4300 6300 SERIES MAGNETO MAINTENANCE AND Instructions OVERHAUL MANUAL L 1363 19 NAVIGATION COMMUNICATIONS AND GPS NAV COM GPS Vendor Address Garmin International PH 913 397 8200 1200 East 151ST Street Olathe KS 66062 http www garmin com 20 OXYGEN SYSTEM Vendor Address Scott Aviation PH 716 683 51...

Page 502: ...DAR WEATHER RDR 2000 Vendor Address Honeywell Bendix King See Autoflight above Maintenance Manual Bendix King ART 2000 P N 006 05332 0001 25 RADIO COOLING BLOWER Vendor Address Globe Motors PH 937 228 3171 2275 Stanley Ave FAX 937 229 8531 Dayton Ohio 45404 http www globe motors com home html 26 STARTER Vendor Address Kelly Aerospace See Alternator above or Sky Tec Partners Ltd PH 800 476 7896 350...

Page 503: ...MALIBU MIRAGE MAINTENANCE MANUAL 28 VACUUM PUMP Vendor Address Aero Accessories Inc PH 800 822 3200 1240 Springwood Avenue Gibsonville NC 27249 http www aeroaccessories com index html 29 VACUUM REGULATORS Vendor Address Parker Hannifin Corp see Fuel Boost Pump above ...

Page 504: ...PAGE 10 Feb 28 07 INTRODUCTION 3A18 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 505: ...chapter CHAPTER SECTION TITLE GRID NO 4 AIRWORTHINESS LIMITATIONS 1C1 00 Airworthiness Limitations 5 TIME LIMITS MAINTENANCE CHECKS 1C9 00 General 10 Time Limits 20 Scheduled Maintenance Checks 30 Special Inspections 50 Unscheduled Maintenance Checks 6 DIMENSIONS AND AREAS 1E13 00 General 7 LIFTING AND SHORING 1F1 10 Jacking 8 LEVELING AND WEIGHING 1F9 10 Weighing and Balancing 20 Leveling 9 TOWIN...

Page 506: ...emperature Control 22 AUTOFLIGHT 2F11 10 Autopilot 23 COMMUNICATIONS 2G19 00 General 50 Audio Integrating 60 Static Discharging 24 ELECTRICAL POWER 2H11 00 General 30 DC Generation 40 External Power 60 Electrical Load Distribution 25 EQUIPMENT FURNISHINGS 2J11 10 Flight Compartment 20 Passenger Compartment 50 Cargo Compartments 60 Emergency 26 FIRE PROTECTION 2K15 20 Extinguishing 27 FLIGHT CONTRO...

Page 507: ...rs 60 Propellers Rotors 31 INDICATING RECORDING SYSTEMS 4C1 50 Central Warning Systems 32 LANDING GEAR 4C13 00 General 10 Main Gear and Doors 20 Nose Gear and Doors 30 Extension and Retraction 40 Wheels and Brakes 50 Steering 60 Position and Warning 33 LIGHTS 4G5 10 Flight Compartment 20 Passenger Compartment 30 Cargo and Service Compartments 40 Exterior 34 NAVIGATION 5C1 00 General 10 Flight Envi...

Page 508: ...00 General 10 Investigation Cleanup and Aerodynamic Smoothness 70 Repairs 80 Electrical Bonding 52 DOORS 6G13 10 Passenger Crew 20 Emergency Exit 30 Cargo 70 Monitoring and Operation 55 STABILIZERS 6H13 00 General 10 Horizontal Stabilizers 20 Elevator 30 Vertical Stabilizer 40 Rudder 56 WINDOWS 6I19 00 General 10 Flight Compartment 20 Cabin 30 Door 57 WINGS 6K5 40 Attach Fittings 50 Flight Surface...

Page 509: ... Power Supply 20 Distribution 76 ENGINE CONTROLS 7G17 10 Power Control 77 ENGINE INDICATING 7H3 10 Power 20 Temperature 40 Integrated Engine Instrument Systems 79 OIL 7J3 20 Distribution 30 Indicating 80 STARTING 7J15 10 Cranking 81 TURBINES 7K9 20 Turbo Supercharger 91 CHARTS WIRING DIAGRAMS 8C1 10 Charts 21 and up Electrical Schematics 91 CONT CHARTS WIRING DIAGRAMS CONT 9C1 Electrical Schematic...

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Page 511: ...sion Control Wing 6L3 Attitude Indicator 5D5 Autopilot 2F17 Component Locator 2G2 Installation 2F18 2F20 Maintenance 2F23 Operational Checkout 2F24 Pitch Servo 2G12 Pressure Transducer 2G6 Roll Servo 2G4 Servo Clutch Torque Adjustment 2G15 Trim Monitor 2G3 Trim Servo 2G6 Yaw Amplifier 2G14 Yaw Servo 2G10 Avionics Cooling 2C14 Avionics Master Switch 2H1 B Ball Diameters for Testing Hose Restriction...

Page 512: ...rrection 2I10 Troubleshooting 2I7 2I13 Valve Regulated Lead Acid 2I13 Bonding 6G9 Resistance Index 6G10 Buses Avionics 2H19 Main 2H19 Circuit Breaker Panel 6D22 Electrical Shelf 6E7 External Power 2I19 Load Distribution 2J1 Relay Installation Co Pilot s Side 6E10 K1 thru K8 6E10 Pilot s Side 6E9 Schematics Air Conditioning 8E7 Airspeed Standby 9E19 Altimeter Radar 9F14 Altimeter Standby 9E19 Annun...

Page 513: ...n Light 9E5 WX 500 9F11 XM Receiver 8E23 Switch Panels 6E1 Symbols 8D14 System 2H17 Troubleshooting 2H20 Tie Bus Panel Connections 6E3 Volt Ammeter 2J4 Voltage Regulation and Control 2H19 Wire Coding 8D13 Elevator Balancing 6I3 Control System Installation 3D23 Rigging and Adjustment 3D24 Troubleshooting 3D19 Torque Tube Bearing Changes 3D20 Trim Controls Actuator Assembly 3E3 Corrosion Control 3E4...

Page 514: ...Drain Valve 3G8 Draining 1I19 Draining Moisture 1I18 Fuel Filter 3G7 Fuel Pumps Specifications 3G5 Fuel Quantity Gauge Accuracy Test 3G14 Full Range Check 3G20 Senders 3G13 Leak Test Setup 3G1 Selector Switch and Valve 3G6 Cable Adjustment 3G7 Troubleshooting 3F16 Leak Evaluation 3F22 G GMA 340 Audio Panel Adjustments 2H6 Installation 2H3 System Functional Test 2H4 GNS 430 5F5 GNS 530 5F5 Ground C...

Page 515: ... 4D11 Position and Warning 4F19 Landing Gear Up Power Reduced Warning Switch Adjustment 4G2 Troubleshooting 4F20 Leading Particulars and Principal Dimensions 1E20 Leveling 1F17 Life Limited Parts 1C7 Lifting 1F7 See also 57 40 00 Lights Exterior 4H3 Landing 4H7 Position 4H4 Pulse 4H7 Strobe 4H3 Taxi 4H6 Wing Inspection Light 4H7 Interior 4G11 Annunciator Panel 4G12 Baggage Area 4G21 Forward 4H1 Re...

Page 516: ...g 3K6 Troubleshooting 3J20 Propeller Assembly 7C9 Publications Piper A12 Vendor A12 Q Quad Digital Indicator QDI See Engine Instruments Transicoil EMIS R Radar 5F1 Repairs Fiberglass 6F19 Metal Wire Stitching 6G5 Thermoplastic 6F21 List of Materials 6F24 Window Windshield Acrylic 6J10 Restraint System 2J23 Inertial Reel Adjustment 2J23 Inspection 2J23 Revised Material A11 Robinair 34700 Charging S...

Page 517: ... Bellcrank Centering 4C22 Horn Arm Gap 4C22 Nose Wheel Centering 3C15 4C22 Rudder Pedal Neutral Alignment 3C15 4C22 Rudder Travel Tool 3C15 Torque Conversion 8C20 Torque Wrench Formula 1K2 Towing 1G5 Transponder 5F9 GTX 327 5F9 GTX 330 5F9 Post Installation Setup Procedure 5F10 ARINC 429 Configuration Page 5F11 Display Mode and Key Lighting 5F11 Hexadecimal Conversion 5F13 Operation Configuration ...

Page 518: ...in 6I11 Vertical Speed Indicator 5C18 Volt Ammeter See Electrical W Warnings Cautions and Notes A11 Weather Radar 5F1 Weighing 1F15 Wheel Brake Assembly 4F4 Wheels Bearing Cup 4F4 Main Wheel Assembly 4F2 Nose Wheel Assembly 4F1 Repairs 4F3 Windows and Windshields Door Window 6K3 Heated Windshield Testing 3J15 Troubleshooting 3J15 Inspection and Repair Definitions 6J1 Limitations 6J1 Crack Limitati...

Page 519: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 9 Feb 28 07 INDEX 3B9 THIS PAGE INTENTIONALLY BLANK ...

Page 520: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 10 Feb 28 07 INDEX 3B10 GRIDS 3B10 THRU 3B24 INTENTIONALLY BLANK ...

Page 521: ...3C1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 27 FLIGHT CONTROLS ...

Page 522: ...3C2 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 523: ... 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 27 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHAPTER SECTION PAGE DATE 27 30 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 ...

Page 524: ...PAGE 2 Feb 28 07 27 LIST OF EFFECTIVE PAGES 3C4 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 525: ... Cables 9 3D3 Removal 9 3D3 Installation 10 3D4 Rigging and Adjustment 11 3D5 Aileron Tab 11 3D5 Aileron Rudder Interconnect 12 3D6 RUDDER AND TAB 27 20 00 1 3D9 Troubleshooting 1 3D9 Rudder Pedal Assembly 2 3D10 Rudder Controls 2 3D10 Removal 2 3D10 Installation 2 3D10 Rigging and Adjustment 5 3D13 Rudder Trim Controls 6 3D14 Removal 6 3D14 Installation 6 3D14 Rigging and Adjustment 8 3D16 ELEVAT...

Page 526: ...ion and Operation 11 3E6 Lift Detector Assembly 11 3E6 Removal 11 3E6 Installation 11 3E6 Dual Warning Unit Horn 11 3E6 Removal 11 3E6 Installation 11 3E6 Stall Warning Functional Test 11 3E6 Force Applicator Kit Test 12 3E7 Flap Switch Input Test 13 3E8 Stall Warning Flight Test Procedure 14 3E9 FLAPS 27 50 00 1 3E11 Flap Drive System 1 3E11 Troubleshooting 1 3E11 Flap Controls 3 3E13 Removal 3 3...

Page 527: ...CONTENTS continued SUBJECT SECTION PAGE GRID NO SPEEDBRAKES 27 60 00 1 3F1 Description and Operation 1 3F1 Troubleshooting 2 3F2 Inspections 2 3F2 50 Hour 2 3F2 Annual 2 3F2 SpeedBrake Cartridges 2 3F2 Removal 2 3F2 Installation 2 3F2 Asymmetric Logic Switching 4 3F4 SpeedBrake Switch 4 3F4 SpeedBrake Annunciator 4 3F4 Testing 4 3F4 ...

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Page 529: ...tivated only when controls are out of harmony In normal coordinated flight it is inactive 2 Standard Practices and Procedures Tips for the removal installation and rigging of the various assemblies A It is recommended though not always necessary to level and place the airplane on jacks during rigging and adjustment B Remove turnbuckle barrels from cable ends before withdrawing the cables through t...

Page 530: ...ging tensions specified must be corrected to ambient temperature in the area where the tension is being checked using Chart 1 On new airplanes it is suggested that cables initially be tensioned 25 to 30 percent over nominal tension then loosened to the High Side of the tolerance This will aid in maintaining specified tension after flight testing K Torque all nuts in the flight control system inclu...

Page 531: ...s To inspect each section which passes over a pulley or through a fairlead remove cable from aircraft to the extent necessary to expose that particular section Examine cables for broken wires by passing a cloth along length of cable This will clean the cable for a visual inspection and detect broken wires if the cloth snags on cable When snags are found closely examine cable to determine full exte...

Page 532: ...ther outer wires worn 40 50 percent as depicted in Figure 2 C Internal Cable Wear As wear is taking place on the exterior surface of a cable the same condition is taking place internally particularly in the sections of the cable which pass over pulleys and quadrants This condition shown in Figure 3 is not easily detected unless the strands of the cable are separated Wear of this type is a result o...

Page 533: ...PAGE 5 Feb 28 07 3C13 27 00 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Internal Cable Patterns Figure 3 Pulley Wear Patterns Figure 4 ...

Page 534: ...andard Inspection Check swaged terminal reference marks for any indication of cable slippage within fitting Inspect fitting assembly for distortion and or broken strands at the terminal Check that all bearings and swivel fittings bolted or pinned pivot freely to prevent binding and subsequent failure Check turnbuckles for proper thread exposure and broken or missing safety wires clips Pay particul...

Page 535: ...ure 4 4 Special Tools These tools are used at the factory and are recommended where the following rigging and or alignment procedures specify use a suitable tool Order them through any Piper Dealer Tool Tool Number Piper P N Rudder Pedal Neutral Alignment Tool HF 622724 762 151 Elevator Elevator Trim Travel Tool HF 689259 762 144 Nose Wheel Centering i e Neutral Tool HF 622722 762 147 Aileron and ...

Page 536: ...e seal B Removal 1 Remove the three seal clips per seal 2 Compress the seal and pull it from the hole in the bulkhead 3 Remove the seal from the cable C Installation 1 Fill the cable air seal with MIL G 21164 grease 2 Apply MIL G 21164 grease to the full travel of the cable section that passes through the seal when the control is actuated 3 Apply a light coat of MIL G 21164 on the external small e...

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Page 538: ...PAGE 10 Feb 28 07 3C18 27 00 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 539: ...ches wiring harness 2 Installation a Connect control wheel switches wiring harness b Slide control wheel onto tube c Position and secure control wheel attachment bolt spacer washer and locknut d Position cover pad assembly and secure with two screws from bottom of control wheel B S N s 4636021 thru 4636131 only 1 Removal a Remove two screws from bottom of control wheel and remove cover pad assembl...

Page 540: ...bbing Replace binding pulleys and or provide clearance between pulleys and brackets Cables not in place on Install cables correctly pulleys Check cable guards Bent aileron and or hinge Repair or replace aileron and or hinge Cables crossed or routed Check routing of control incorrectly cables Control wheels not Incorrect control column Re rig control column synchronized rigging Control wheels not I...

Page 541: ...PAGE 3 Feb 28 07 3C21 27 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Control Wheel Installation Figure 1 ...

Page 542: ...ure time f Prime threads of control wheel attachment screw with Loctite 7649 Piper P N 279 073 Allow to dry g Install control wheel attachment screw with spacer into nutplate using Loctite 271 Piper P N 279 128 NOTE This step must be accomplished promptly due to short cure time h Position retainer clip to capture spacer and control wheel attachment screw Secure with screws 2 being careful not to o...

Page 543: ...TE The control column stop assy is fitted over the tube secured by the same bolt and will be removed with the tube 7 The control column can now be removed from under the instrument panel 2 Installation a Forward control column assembly NOTE First ensure that the nut attaching control column rod to mount on forward end of control column is tightened to a torque of 40 to 45 inch pounds 1 Position th...

Page 544: ...PAGE 6 Feb 28 07 3C24 27 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Control Column Installation Figure 3 ...

Page 545: ...ntrol wheel and tube 1 Connect the control wheel switches wiring harness 2 Slide the wheel and tube assembly into the instrument panel NOTE If bearing on instrument panel is loose when inserting wheel and tube assembly use LOC 498 50 or LOC 495 50 Super Bond adhesive to bond bearing onto instrument panel 3 Secure the tube and control wheel to the guide assembly with the four cap screws Safety the ...

Page 546: ...el switches electrical harness if installed 5 Attach the primary and control wheel balance cables to the aileron quadrant at the forward end of the control column assembly and secure each cable end retainer i e lockplate with a screw see note below Safety the cable end retainer screws with MS20995 C32 safety wire NOTE As of early 2006 the original MS35265 42 fillister head screw has been replaced ...

Page 547: ...ol column quadrant assemblies e Draw the cables back through the floor 3 To remove the primary control cable in either wing proceed as follows a Remove the access panel from the cabin floor at fuselage station 171 43 b Separate the primary cable at the turnbuckle within the fuselage and disconnect the opposite end at the sector out in the wing located aft of the rear spar at wing station 175 498 c...

Page 548: ...ust be replaced with the socket head screws upon reassembly Additionally when using the MS24674 8 P N 520 036 socket head screws torque to 12 to 15 in lbs c Ensure that the cable is properly placed around the pulley and install cable guards d Route cable around the pulley at fuselage station 171 43 and install cable guard e Connect cable turnbuckle to primary cable end from wing and ensure proper ...

Page 549: ...er in the aileron neutral position using a suitable tool 2 Lock the ailerons in neutral position using a suitable contour fixture at the inboard ends of the ailerons Neutral position is defined by wing loft contour at this location 3 Adjust the aileron control cables to a tension of 30 5 pounds 4 Remove the locking fixtures Aileron neutral position should be maintained at 0 1 0 degree with the con...

Page 550: ... that the aft cable clamp on the left aileron cable is positioned 2 00 inches from the aft face of the F S 139 80 fuselage frame E Ensure that the forward side of the forward arm of the aileron rudder interconnect is positioned 1 70 inches from the aft face of the F S 131 84 fuselage frame F Ensure that the forward side of the guide on the left rudder cable is positioned 3 50 inches from the aft s...

Page 551: ...low LEFT RUDDER CABLE GUIDE LEFT AILERON CABLE CONTROL CABLE SLEEVE CLAMPS 4 REQUIRED LBL 1 602 LBL 4 732 CABLE GUIDE AFT FACE OF FUSELAGE LOWER FRAME NOTE In early production airplanes these pins may interfere with the F S 139 80 frame If so reverse the pins and add two 2 NAS 1149FN416P washers between the cotter pin and the plate Aileron Rudder Interconnect Installation Figure 6 ...

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Page 553: ...vement properly Rudder pedal torque tube Lubricate torque tube bearing in need of lubrication bearings Cable tension too high Adjust cable tension Pulleys binding or rubbing Replace binding pulleys and or provide clearance between pulleys and brackets Cables not in place on Install cables correctly pulleys Check cable guards Cables crossed or routed Check routing of control incorrectly cables Inco...

Page 554: ...the screw which secures the rudder cable end retainer i e lockplate to the rudder bar sector Remove the cable from the sector b Remove the aft fuselage access panel c Disconnect the rudder turnbuckles by the rudder tube sector in the aft section of the fuselage d At the aft pressure bulkhead pull the control cable through the fin type air seal Refer to Figure 5 27 00 00 e Pull the cable aft and re...

Page 555: ...PAGE 3 Feb 28 07 3D11 27 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Rudder Controls Figure 1 ...

Page 556: ...0 00 Thread the cable forward through the airplane b Connect the forward and aft rudder cables at the turnbuckles in the aft end of the airplane c Attach the forward ends of the forward cables to the rudder bar sector and secure the cable end retainer i e lockplate with a screw see note below Safety the cable end retainer screw with MS20995 C32 safety wire NOTE As of early 2006 the original MS3526...

Page 557: ...gure 3 32 20 00 NOTE Measure the gap with the steering arm parallel to the steering horn rollers While measuring this clearance the gear should be down and locked and the airplane s weight should be on the gear 7 Torque the steering arm mounting nut and the adjuster jam nuts 8 Ensure that the two steering pushrods are holding the steering bellcrank perpendicular to B L 0 00 refer to 32 50 00 Steer...

Page 558: ...bly a Slide forward clip onto housing b Lubricate shaft at each end of spring with Aero Lubriplate white and insert shaft assembly into housing Install aft clip c Check for 0 020 inch max end play Add 62833 127 washers as required between forward clip and end of spring on the shaft assembly to bring the end play into tolerances d Ensure that length of trim bungee is correct as recorded in step 3 R...

Page 559: ...PAGE 7 Feb 28 07 3D15 27 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Rudder Trim Installation Figure 3 ...

Page 560: ... full travel stop to stop 5 Set trim wheel and trim indicator at midpoint of trim wheel travel with rudder set 3 degrees to the left of 0 6 Adjust length of bungee rod as required to reconnect it with no load on the bungee springs 7 Check full range travel to ensure that indicator guide pin does not reach either end of spiral groove in trim wheel before the stop is engaged at roll pin on worm CAUT...

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Page 563: ... tension too high Adjust cable tension Binding control column Adjust and lubricate Pulleys binding or rubbing Replace binding pulleys and or provide clearance between pulleys and brackets Cables not in place on Install cables correctly pulleys Cables crossed or routed Check routing of control incorrectly cables Incorrect elevator travel Elevator stops Adjust stop screws incorrectly adjusted Correc...

Page 564: ...etains the elevator cable lockplates e Remove the cable end retainer i e lockplate screws and remove the cables f Remove the bolts nuts and washers that secure the quadrant to the elevator torque tube g Remove the quadrant Trouble Cause Remedy Trim control wheel moves System not lubricated Lubricate system with excessive resistance properly Cable tension too high Adjust cable tension Pulleys bindi...

Page 565: ...ws with MS20995 C32 safety wire Ensure the safety wire is installed so that the wire is inside and clear of the elevator pushrod fork through the full travel of the quadrant NOTE As of early 2006 the original MS35265 42 fillister head screw has been replaced by a higher strength MS24674 8 P N 520 036 socket head screw In earlier airplanes anytime the cable end retainer screws are removed if the or...

Page 566: ... clearance from edge of the quadrant d Attach forward cable assemblies to aft cable assemblies at the turnbuckles located just forward of the aft quadrant e Ensure that all cable guards are in place f Refer to steps 5 and 6 g Attach the elevator downspring 4 To install the elevator aft cable assemblies a Attach cables to quadrant and secure the cable end retainers i e lockplate with screws see not...

Page 567: ...PAGE 5 Feb 28 07 3D23 27 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Elevator and Elevator Trim Installation Figure 1 ...

Page 568: ...secondary forward stops should be 0 30 0 10 inch There is no adjustment on the secondary stop NOTE If necessary use the cable rigging turnbuckles to bring the control wheels into their neutral position 7 With the elevator physically held against the trailing edge up primary aft stop adjust the secondary stop on the channel ahead of the instrument panel to provide a cushion gap of 0 06 0 09 inch Lo...

Page 569: ... clears the aft end of the plastic tube Keep tension on both ends of the disconnected cable while the assistant is rotating the trim wheel 8 Have the assistant tie another pull rope forward of the turnbuckle on the remaining cable 9 Have the assistant disconnect his cables keeping tension on both ends of the cable 10 Transfer the cable ends to one man Have him keep tension on all four cable ends 1...

Page 570: ...einstall the floor access panels that were previously removed f Ensure that the pulley cable guards are installed at all elevator trim cable pulleys g Replace the access panel on the console h Check operation of elevator trim controls See Caution under Rigging B Elevator Trim Actuator 1 Removal a Block the cables at the actuator drum b Disconnect the trim cable turnbuckles inside the plastic tube ...

Page 571: ...PAGE 9 Feb 28 07 3E3 27 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Elevator Trim Actuator Assembly Figure 2 ...

Page 572: ...sembly d Secure the aft retainer and guide to the aft side of the housing with the screws nuts and washers NOTE Refer to Figure 2 for information on setting trim drum end play e Place the housing drum assembly into the actuator frame f Insert the actuator screw through the frame and then into the housing drum assembly g Rotate the screw until the housing drum assembly is positioned as shown in Fig...

Page 573: ...TAB OPERATING GEOMETRY 4 Set the tab to the Elevator Tab Elevator Neutral Trailing Edge Down angle specified in Chart 2 by adjusting the two straight rods which penetrate the aft fuselage bulkhead The rods must be within 0 010 inch of the same length upon completion of adjustment Lock the jam nuts on the rods 5 Move the elevator trim wheel forward nose down until the elevator tab is at the Elevato...

Page 574: ...t detector to leading edge of wing b Pull lift detector partially out of opening in wing and disconnect wires at connector c Remove lift detector 2 Installation a Connect wires from detector to harness b Position lift detector in the opening in the wing and secure with the four screws c Check lift detector for operation per Stall Warning Functional Test C Dual Warning Unit Horn 1 Removal a Disconn...

Page 575: ...1952 1 to measure the tip grams of force settings required at the lift transducer vane to energize the signal 1 Attach the positioner to the lift transducer cavity as shown in Figure 2 1 in Safe Flight s Force Applicator Kit operation manual The squat switch shall be in the in flight condition a Position the cockpit pedestal power lever to the power off position and flaps to the full up position T...

Page 576: ...ove flap position switch to 36 Verify open circuit between pins 4 and 5 Verify continuity between pins 4 and 6 7 Move flap position switch back to 20 Verify open circuit between pins 4 and 6 Verify continuity between pins 4 and 5 8 Move flap switch to 0 Verify open circuit between pins 4 and 5 9 If all tests pass reinstall P376 on lift computer If all do not pass verify flap microswitch installati...

Page 577: ... to stall and continues until stall occurs b Desired stall warning begins at 6 to 9 KIAS prior to stall and continues until stall occurs 2 If the stall warning system fails to perform within the limits above adjust the system and refly the test 3 If not able to adjust the stall warning system sufficient to achieve the limits above recheck the replacement wing installation to ensure it is installed...

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Page 579: ...l pushrods extend out along the wing rear spar to an idler arm at W S 64 00 and on to another bellcrank at W S 93 00 Pushrods connected to the bellcranks at W S 64 00 and W S 93 00 connect the flaps to complete the drive system To ensure a good pressure seal at the fuselage exit points of the flap drive pushrods a bellows is connected to the pushrods and tube assemblies which are part of the fusel...

Page 580: ...PAGE 2 Feb 28 07 3E12 27 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Flap Motor Actuator and Drive System Figure 1 ...

Page 581: ...042 4 nut connecting the arm assembly to the pushrod assembly and link E b Remove the AN24 34A bolt MS21042 4 nut two 82695 97 bushings an NAS1149F0432P washer two NAS1149F0663P and two NAS1149F0632P washers that secure the arm assembly to the tube assembly and aft link assembly c Remove arm assembly 4 To remove the aft link assembly See Figure 2 a Disconnect the flap position indicator cable from...

Page 582: ...sher that secures the pushrod to the bellcrank b Remove the AN4 12A bolt MS21042 4 nut and two NAS1149F0463P washers that secures the pushrod to the support bracket on the flap c Remove the pushrod 8 To remove the flap interconnect pushrod assembly See Figure 3 a Remove the AN310 4 nut AN4 11 bolt NAS1149F0463P washer NAS1149F0432P washers and MS24665 134 pin that secures the interconnect pushrod ...

Page 583: ...PAGE 5 Feb 28 07 3E15 27 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Flap Motor Actuator and Drive System Fuselage Components Figure 2 ...

Page 584: ...PAGE 6 Feb 28 07 3E16 27 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Flap Motor Actuator and Drive System Wing Components Figure 3 ...

Page 585: ...utboard bellcrank arm with NAS464 P4A8 bolt MS21042 4 nut and NAS1149F0432P washer c Position pushrod s aft rod end bearing on flap support Install AN4 12A bolt with head pointing outboard two 82695 42 bushings two NAS1149F0463P washers under nut and MS21042 4 nut 2 To install the outboard bellcrank See Figure 3 a Position bellcrank in support b Install AN4 20 bolt head pointing down 82695 37 bush...

Page 586: ...d into flap 82977 2 pushrod assembly clevis Install the two 82695 39 bushings Position this assembly into the idler arms and secure with AN4 13 bolt head pointing down two NAS1149F0463P washers under nut and AN310 4 nut Tighten nut until idler arms seat on bushing then tighten one to two more castellations Ensure that idler operates freely then install MS24665 134 cotter pin c Place remaining rod ...

Page 587: ... 2 Secure other end of pushrod to the left inboard bellcrank assembly with a NAS464 P5A9 bolt and MS21042 5 nut d Attach right flap drive pushrod 1 Position flap drive pushrod in U shaped bracket on end of tube assembly Insert the two 82695 97 bushings Position the U shaped bracket on end of arm assembly over bushings with one each NAS1149F0663P and NAS1149F0632P washers between bushings and arm a...

Page 588: ... the link is free to pivot then install MS24665 132 cotter pin Safety with MS20995C32 wire c Secure link E to the pushrod and the motor actuator unit with two 82695 96 bushings NAS1149F0463P washer under nut NAS1149F0432P washer under bolt head AN4 16A bolt and MS21042 4 nut d Secure link E to connecting arm assembly and pushrod assembly with an AN4 13A bolt NAS1149F0463P washer and MS21042 4 nut ...

Page 589: ...ging Flaps 4 Flap System Rigging PIR PPS50056 2 Rev P WARNING PULL ELECTRIC FLAP CIRCUIT BREAKER BEFORE BEGINNING CAUTION DO NOT ADJUST PRESET LENGTH OF COMPONENTS UNLESS SPECIFIED BELOW A Before rigging flaps 1 If necessary disconnect flap pushrods from wing bellcranks 2 Rig flaps before lubricating flap tracks 3 Check that the length of the arm assembly Figure 2 is 14 92 inches If necessary to r...

Page 590: ... outboard rod end of the pushrod 85097 2 see Figure 2 bolts to a slot in the cam assembly To increase flap travel move that rod end forward in the slot To decrease flap travel move that rod end aft in the slot Adjust rod end as required to allow the cam assembly to activate the warning horn switch NOTE It is acceptable to have up to 3 16th inch vertical end play at flap trailing edge in the 0 flap...

Page 591: ...Remove the paint with a commercially available paint stripper such as Cee Bee E2012 or E2060 D Using a dye penetrant method of inspection per latest revision of AC 43 13 1 1 Inspect for cracks at either arm on the bellcrank shaft near the welds 2 Inspect for cracks on the shaft itself as shown in Figure 4 E If no cracks are found repaint the bellcrank s and reinstall F If cracks are found 1 Replac...

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Page 593: ...ce or repair and to operate Microswitch if Microswitch pulling circuit breaker returns is OK use schematic to brakes to stowed find break in wiring Switch inoperative Replace or repair switch if switch OK use schematic to find break in circuit Motor and Asymmetric Logic Replace Asymmetric Logic Control Unit failed Control Unit CAUTION DO NOT PUSH SPEEDBRAKE BLADES DOWN IF THEY FAIL TO RETRACT FORC...

Page 594: ...edBrake Cartridges which are in each wing between W S 93 00 and 107 50 consist of a gearmotor and clutch assembly driving the interconnected blades through a worm gear set The blades are loaded to the retracted position by a constant force spring The SpeedBrake cartridge also contains two microswitches one for the retracted position and one for the extended position The microswitches control gearm...

Page 595: ...PAGE 3 Feb 28 07 3F3 27 60 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL SpeedBrake 50 Hour Inspection Figure 1 Effectivity 4636187 and up If Installed ...

Page 596: ...rly operating SpeedBrake system should function as specified below 1 Turn on aircraft power 2 Switch SpeedBrakes ON Full deployment should occur in no more than 2 5 seconds WARNING DO NOT PUT FINGERS IN HOLES OF EXTENDED SPEEDBRAKE BLADES IF POWER TO THE SYSTEM IS INTERRUPTED THE SPEEDBRAKE BLADES WILL CLOSE WITH SUFFICIENT FORCE TO AMPUTATE FINGERS 3 Verify motor stop Verify full blade extension ...

Page 597: ...des remain extended turn aircraft power OFF remove the cartridge test connector from the left speedbrake wiring harness and reconnect the wiring harness to the left speedbrake cartridge 7 Turn aircraft power ON and operate speedbrake system WARNING DO NOT PUT FINGERS IN HOLES OF EXTENDED SPEEDBRAKE BLADES IF POWER TO THE SYSTEM IS INTERRUPTED THE SPEEDBRAKE BLADES WILL CLOSE WITH SUFFICIENT FORCE ...

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Page 601: ...3F9 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 28 FUEL ...

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Page 603: ...8 00 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 28 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 28 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 28 40 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb...

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Page 605: ... Pump 1 3G5 Removal 1 3G5 Installation 1 3G5 Fuel Selector Valve 2 3G6 Description 2 3G6 Removal 2 3G6 Installation 2 3G6 Switches Adjustment 3 3G7 Fuel Selector Cable Adjustment 3 3G7 Fuel Filter 3 3G7 Removal 3 3G7 Installation 3 3G7 Fuel Drain Valve 4 3G8 Description 4 3G8 O ring Replacement 4 3G8 Electric Boost Pump 4 3G8 Emergency Fuel Pump 5 3G9 Removal 5 3G9 Installation 5 3G9 INDICATING 28...

Page 606: ...only 4 3G16 Programmable Transicoil EMIS Gauge S N s 4636132 thru 4636374 6 3G18 Complete 8 3G20 Fuel Gauge Full Range Check S N s 4636021 thru 4636374 8 3G20 Set up 8 3G20 Non Programmable Transicoil EMIS Gauge S N s 4636021 thru 4636131 only 8 3G20 Programmable Transicoil EMIS Gauge S N s 4636132 thru 4636374 10 3G22 Complete 10 3G22 Fuel Quantity Indicator Calibration S N s 4636375 and up 11 3G...

Page 607: ...ind the copilot s seat in a non pressurized compartment All fuel lines passing through the pressurized cabin are metal tubes surrounded by plastic cushion and encased by a second metal tube This second tube is sealed from the cabin environment to preclude fuel from entering the cabin area or pressurized cabin air from entering fuel lines in the event of a leak The selector valve is cable controlle...

Page 608: ...valve valve Fuel quantity gauge Broken wire Check and repair fails to operate Gauge inoperative Replace gauge Fuel sender float Replace sender partially or completely filled with fuel Circuit breaker open Check and reset Float and arm assembly Check of fuel sender sticking Bad ground Check for good contact at ground lip or rear of gauge No fuel pressure Fuel selector valve Check fuel selector indi...

Page 609: ...oost Pump NACA Vent Nozzles vented to Deck Pressure Fuel Nozzle Flow Divider Deck Turbochargers Engine Driven Fuel Pump Seal Drain Firewall Electric Emergency Fuel Pump Supply Line Fuel Selector Handle Fuel Selector Valve Metering Unit Right Tank Vent Line Drain Fuel Quantity Gauge Finger Screens Fuel Lines Filler Cap Collector Tank To Intake Manifold Fuel Flow Transducer Filter and Drain ON Fuel ...

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Page 613: ...follows a In S N s 4636021 thru 4636379 remove the screws securing the access cover With a suitable tool pry the access cover away from the wing taking care not to damage the mating surfaces especially on the wing When the access cover becomes free carefully lower the cover and sender out of the wing until the electrical connection can be reached and disconnected b In S N s 4636380 and up remove t...

Page 614: ...mpartment The following provides criteria for evaluating various categories of leaks and the maintenance action required A Wing tanks WARNING CAREFULLY EXAMINE ANY LEAKAGE TO ENSURE THAT IT IS NOT PROGRESSING TO A CRITICAL AREA OF THE AIRPLANE AND THAT THERE IS NO POSSIBILITY OF FUEL BEING BLOWN INTO THE FUSELAGE AREAS 1 Upper wing surface The airplane may be released for flight with a fuel leak i...

Page 615: ...ne the leak area and apply the following criteria to identify the leak category and required maintenance action See Figure 2 and Chart 1 a A stain Detail A is evaluated as a leak where fuel wets an area around the apparent leak source such that the wetted area width is not over two 2 inches b A seep Detail B is defined as a leak where the fuel wets an area around the apparent leak source such that...

Page 616: ...PAGE 4 Feb 28 07 3F24 28 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Categorizing Fuel Leaks in the Wet Wing Figure 2 ...

Page 617: ...ER AND DRAIN FUEL PRESSURE SWITCH FUEL SUPPLY HOSE DISCONNECT AND CAP HERE CLEAR PLASTIC HOSE SMALL ORIFICE FITTING OPEN TO AMBIENT WATER MANOMETER 22 IN MANOMETER HOSE FUEL TANK VENT PLUG HERE ZERO MARK SCALE EACH MINOR TICK 0 2 IN H2O MAX HEIGHT 43 IN H2O 42 IN H2O TEST PRESSURE 1 FILL TO 22 IN MARK WITH COLORED WATER 2 ADJUST SCALE TO ZERO MARK FUEL SYSTEM LEAK TEST SETUP RIGHT SIDE SHOWN LEFT ...

Page 618: ...om the other fitting 4 Appropriate hoses to connect shop air and the manometer to the special fuel filler cap NOTE To minimize the chance of cross connecting shop air and the manometer to the wrong fitting these hoses should be semi permanently connected to the special fuel filler cap 5 The water manometer must be marked in inches at two tenths of an inch intervals have a height of no more than 43...

Page 619: ...ollows a Install special fuel filler cap on right wing fuel filler NOTE Verify that shop air hose is connected to the fitting with the small orifice and manometer hose is connected to the other fitting b Verify needle valve is fully closed and connect shop air to the quick disconnect fitting c Plug right wing fuel tank vent d Set fuel selector handle on RIGHT tank position WARNING IF MANOMETER FAI...

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Page 621: ... of the collector tank e Disconnect the electrical connection to the pump and the fuel line from the pump Cap the open line to prevent any possible contamination f Remove the four nuts securing the collector tank and remove the tank g Remove the two screws securing the pump to the tank and remove the pump 2 Installation a Position fuel pump with gasket into the tank and secure in place with the tw...

Page 622: ...e the fuel line pressure seal halves to the fuel line going to the left tank 4 Remove the screws and washers that secure the base of the pressure closeout plate to the frames Slide the pressure closeout plate inboard along the fuel line going to the left tank 5 Disconnect the fuel selector cable from the actuating arm on the bottom of the fuel selector valve 6 Disconnect the switches electrical co...

Page 623: ...e right tank position Visually check the fuel selector arm and cam to confirm proper adjustment Properly adjusted the selector knob will not reach the instrument panel slot travel limits when resting in the right tank and off positions Travel should be equal distance from center 10 4 Fuel Filter NOTE For routine filter servicing refer to 12 10 00 Fuel System A Removal Access to the fuel filter is ...

Page 624: ...ve snap ring to release inner assembly 4 Remove inner assembly by pushing up on drain screw with a screwdriver 5 Remove internal O ring 6 Soak replacement O rings in hydraulic fluid and coat with fluid compatible gel 7 Install O rings 8 Replace inner assembly Replace snap ring 9 Install drain valve in wing 6 Electric Boost Pump These pumps are located in each collector tank built into each wing wh...

Page 625: ...ve safety wire and three mounting bolts from emergency fuel pump 9 Remove emergency fuel pump and filter assembly from aircraft 10 Loosen jam nut at fuel pump inlet fitting 11 Remove emergency fuel pump B Installation NOTE Be sure to replace O rings at inlet and discharge pump fittings 1 Position emergency fuel pump onto filter and tighten jam nut at emergency fuel pump inlet fitting 2 Position em...

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Page 629: ...er access cover to indicate aircraft forward 4 Remove the sender access cover as follows a In S N s 4636021 thru 4636379 remove the screws securing the access cover With a suitable tool pry the access cover away from the wing taking care not to damage the mating surfaces especially on the wing When the access cover becomes free carefully lower the cover and sender out of the wing until the electri...

Page 630: ...lect position A on resistor decade Verify that instrument needle points to F If not adjust respective GAIN potentiometer to center needle on F radial 6 Full range check After low and high end adjustments have been made verify that for each resistive value the gauge indication is as specified in Chart 1 B Post installation functional check 1 Set up a Level the airplane 1 degree laterally and longit...

Page 631: ... G 6 8 E 0 1 2 F 16 1 5 1 2 E 29 5 10 1 2 D 38 8 15 1 2 C 58 7 30 1 2 B 75 2 45 1 2 A 102 3 F 1 2 SEE FIGURE 1 SEE FIGURE 2 1 2 NEEDLE WIDTH NEEDLE APPROPRIATE RADIAL MARK NEEDLE DEVIATION Needlewidth Figure 2 CHART 2 FULL RANGE CHECK TOTAL FUEL QUANTITY US GAL GAUGE TOLERANCE INCLUDES 1 GAL UNUSABLE INDICATION NEEDLEWIDTHS 1 E 0 1 6 5 3 4 11 10 3 4 16 15 1 31 30 1 1 2 46 45 1 1 2 60 F 1 1 2 SEE F...

Page 632: ...4636021 thru 4636374 PIR PPS60032 13 Rev O NOTE S N s 4636021 thru 4636374 Review Chapter Section 77 40 00 Transicoil Electronic Module Instrument System EMIS to ensure a basic understanding of the system components and their operation before proceeding NOTE S N s 4636021 thru 4636131 only If utilizing resistance measurements from Chart 4 it will be necessary to connect a digital ohmmeter per Char...

Page 633: ...tentiometers marked Z clockwise to lower reading until the analog pointers are at the center of the E empty graduations Allow indicators to stabilize for 30 40 seconds Readjust as required Check digital readout for a 0 gallon indication If digital does not indicate 0 readjust appropriate Z potentiometer until both analog and digital read zero NOTE The potentiometers are in cavities on the right an...

Page 634: ...de The left and right Fuel Quantity Module Analog Indicators are calibrated individually The following instructions specifically address the left indicator a If fuel quantity indicator is installed in instrument panel remove gauge from panel far enough to move calibration switch on left side of the module from RUN to CAL position move switch toward front of gauge This will place left fuel quantity...

Page 635: ...step being recorded the LED s will stop flashing and remain on the external alarm will sound and the EDI display and the fuel quantity module pointer will advance to the next step The external alarm will continue to sound as long as the SEL button is held NOTE If the sensor is out of range for the calibration step being programmed then pressing the left SEL button will not advance the module to th...

Page 636: ...ity Gauge Calibration Set up above B Non Programmable Transicoil EMIS Gauge S N s 4636021 thru 4636131 only NOTE The Programmable Transicoil EMIS Gauge P N 602 222 installed in S N s 4636132 thru 4636374 as original equipment is backwardly compatible and may be found installed in S N s 4636021 thru 4636131 as a service spare These modules can be identified by the absence of potentiometers and the ...

Page 637: ...ION WORKSHEET 3 When pointers are adjusted correctly fill each tank with 5 gals of fuel after 1 gal unusable has been added and record data in Chart 4 4 Fill tanks in 15 30 45 and 60 gal increments and record data in Chart 4 Vibrate the tanks by bumping their lower surfaces at each calibration point a While filling the tanks check operation of imbalance fuel annunciator light by adding 10 1 0 gals...

Page 638: ...icators must read E as described in Figure 3 Record data in Chart 4 4 Fill tanks in 5 15 30 45 and 60 gal increments and record data in Chart 4 Vibrate the tanks by bumping their lower surfaces at each calibration point a While filling the tanks check operation of imbalance fuel annunciator light by adding 10 1 0 gals more to right tank than left Light should illuminate b Reverse procedure and fil...

Page 639: ...t be accepted 6 Once all points have been calibrated the operator presses Calibration Complete to cause the calibration factors to be computed and applied to the DAU reported fuel quantity 7 Other options from the Calibration Underway state are to Restore Last Cal and Clear Cal a Pressing Restore Last Cal causes the calibration values from the last completed calibration to be restored and the stat...

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Page 641: ...3H1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 29 HYDRAULIC POWER ...

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Page 643: ...t of 1 Feb 28 06 Effective Pages 2 Feb 28 06 29 Table of Contents 1 Feb 28 06 2 Feb 28 06 29 00 00 1 Feb 28 06 2 Feb 28 06 3 Feb 28 06 4 Feb 28 06 29 10 00 1 Feb 28 06 2 Feb 28 06 3 Feb 28 06 4 Feb 28 06 5 Feb 28 06 6 Feb 28 06 7 Feb 28 06 8 Feb 28 06 9 Feb 28 06 10 Feb 28 06 11 Feb 28 06 12 Feb 28 06 13 Feb 28 06 14 Feb 28 06 15 Feb 28 06 16 Feb 28 06 CHAPTER SECTION PAGE DATE ...

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Page 645: ...ing 1 3H7 Hydraulic System Leading Particulars 1 3H7 MAIN 29 10 00 1 3H11 Description 1 3H11 Hydraulic Pump Parker Hannifin 1 3H11 Removal 1 3H11 Installation 3 3H13 Disassembly 3 3H13 Assembly 5 3H15 Hydraulic Pump Frisby 8 3H18 Removal 8 3H18 Installation 8 3H18 Testing 10 3H20 Bleeding Hydraulic System 11 3H21 Hydraulic Lines Removal and Installation 11 3H21 Hydraulic System Testing 13 3H23 Hyd...

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Page 647: ... pressure from exceeding 2600 psi when the landing gear is down and locked and airplane is on the ground The landing gear selector is an electrical switch that commands the pump to operate in either the up or down position The gear is held in the up position by hydraulic pressure Emergency gear extension is accomplished by a free fall function of the gear selector valve which releases gear up hydr...

Page 648: ...ting Current 1350 psig 55 Amps Max 27 Vdc Operating Time Gear Up 7 8 sec Gear Down 7 8 sec Overload Protection 25 Amp Circuit Breaker Hydraulic Pump Electrically Driven Reversible Flow Rate 1350 psi 1 gpm Hydraulic Fluid MIL H 5606 Reservoir Capacity 30 cu in 49 liters Normal Operating Pressure 1350 psi Relief Valve Thermal Opens at 2525 75 psig Relief Valve Pressure Opens at 1600 0 50 psig Pressu...

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Page 651: ...ace the fill plug 2 Hydraulic Pump Parker Hannifin S N s 4636001 thru 4636313 only See Figure 3 WARNING PLACE AIRPLANE ON JACKS PRIOR TO CHECKING OUT THE HYDRAULIC SYSTEM REFER TO 7 10 00 A Removal The hydraulic pump is located on a floor bracket just forward of the aft pressure bulkhead assembly 1 Place airplane on jacks refer to 7 10 00 Jacking 2 Reduce hydraulic pressure as follows a Place gear...

Page 652: ...PAGE 2 Feb 28 07 3H12 29 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Fluid Diagram of Hydraulic System Figure 2 ...

Page 653: ...y not require complete disassembly Follow steps 1 thru 8 as needed for access to air vent motor pump reservoir pressure relief valves and O rings Sight glass may be removed step 4 without removing other parts NOTE Follow steps 9 thru 13 as needed prior steps not necessary for removal of pressure switches elbow restrictor fittings upper manifold and lower manifold NOTE Drain pump prior to disassemb...

Page 654: ...ure switches Discard O rings 10 Remove elbow and restrictor fitting by loosening nut s unscrewing elbow s from lower manifold and discarding O ring s NOTE Upper and lower manifolds must be replaced as a set in pump serial numbers 156 and up These can be distinguished by gold color instead of gray in earlier models Refer to PA 46 350P Parts Catalog 11 Remove and discard large O ring from upper mani...

Page 655: ...If replacing sight glass install gasket glass and cover onto reservoir with four screws Torque 8 12 in lbs 7 Install O ring onto upper manifold 8 Install reservoir Align carefully on manifold See Figures 4 and 5 9 If cap plate and motor have been separated a Install new shaft seal onto cap plate b Assemble cap plate to motor with four screws washers and seals c Torque 25 35 in lbs CAUTION DO NOT A...

Page 656: ...PAGE 6 Feb 28 07 3H16 29 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Hydraulic Pump Parker Hannifin Disassembled Figure 4 Effectivity 4636001 thru 4636313 ...

Page 657: ...PAGE 7 Feb 28 07 3H17 29 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Hydraulic Pump Parker Hannifin Subassembly Alignment Figure 5 Effectivity 4636001 thru 4636313 ...

Page 658: ...and rapidly cap hydraulic lines and hoses 8 Install vent screw washer and warning tag 9 Remove four sets of mounting bolts washers rubber washers and nuts 10 Remove pump from airplane to a clean bench 11 Drain reservoir into a suitable container B Installation WARNING BE SURE AIRPLANE IS ON JACKS BEFORE BLEEDING AND TESTING HYDRAULIC SYSTEM 1 Place pump assembly in aircraft NOTE Align pump assembl...

Page 659: ... W D U R I N G F I L L I N G D O W N U P 102559 B PUMP MOTOR VENT SCREW REMOVE BEFORE FLIGHT REPLACE BEFORE REMOVING PUMP FROM AIRCRAFT FILL VENT REMOVE SCREW WHILE FILLING RESERVOIR FILL PLUG SEE THRU FLUID RESERVOIR DOWN PRESSURE SWITCH UP PRESSURE SWITCH Hydraulic Pump Frisby Figure 6 Effectivity 4636314 and up ...

Page 660: ...xcept if the pump operates once momentarily during this five minute period there shall be no repeated pump operation during the subsequent fifteen minutes c Repeat b above with the gear switch in the gear DOWN position d With the shut off valve open the gear selector switch in the gear DOWN position and the pressure switch disconnect switch in the DOWN position allow the pump to operate approximat...

Page 661: ...RAULIC PUMP IS OPERATING ALWAYS PULL THE HYDRAULIC PUMP CIRCUIT BREAKER BEFORE TESTING THE EMERGENCY GEAR RELEASE SYSTEM FAILURE TO COMPLY WILL DAMAGE THE EMERGENCY GEAR RELEASE VALVE CAUTION DO NOT OVERFILL AND DO NOT ALLOW HYDRAULIC FLUID LEVEL TO DROP BELOW THE L LOW MARK ON THE SIGHT GAUGE WITH THE GEAR IN THE DOWN POSITION NOTE Follow this sequence below to reduce foaming Add fluid to reservo...

Page 662: ...MIRAGE MAINTENANCE MANUAL UP DN WHT RED BLK HYDR PUMP P P UP DN PRESS SW PRESS SW PUMP UP PUMP DN PRESSURE SWITCH DISCONNECT GEAR SELECT SWITCH UP DN OFF UP DN 28 VDC 25A 3A GAUGE GAUGE SHUT OFF VALVE Effectivity Hydraulic Pump Frisby Test Set up 4636314 and up Figure 7 ...

Page 663: ...ulic lines by disconnecting the fittings at each end and where it is secured by brackets See Figure 1 as an aid in locating the attaching brackets and bends in the lines B Provide a small container for draining the line C Install new or repaired line in the reverse order of removal D Bleed system and lines E Check fluid level in reservoir 6 Hydraulic System Testing WARNING BE SURE AIRPLANE IS ON J...

Page 664: ...iewing fluid levels in the sight gauge If fluid is below the fill line remove filler plug and fill with MIL H 5606 hydraulic fluid Install filler plug and tighten B Frisby Check fluid level in reservoir every 50 hours by viewing fluid level directly If fluid is below the fill line i e the L mark remove fill plug and fill vent screw and add MIL H 5606 hydraulic fluid Ensure that the landing gear is...

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Page 667: ...3I3 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 30 ICE AND RAIN PROTECTION ...

Page 668: ...3I4 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 669: ... 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 19 Feb 28 07 20 Feb 28 07 21 Feb 28 07 22 Feb 28 07 23 Feb 28 07 24 Feb 28 07 25 Feb 28 07 26 Feb 28 07 30 30 00 1 Feb 28 07 2 Feb 28 07 30 40 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 CHAPTER SECTION PAGE DATE 30 60 00 1 Feb 28 07 2 Feb 28 07 3 Feb...

Page 670: ...PAGE 2 Feb 28 07 30 LIST OF EFFECTIVE PAGES 3I6 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 671: ...1 Removal 1 3I11 Installation 1 3I11 Vacuum Manifold Check Valve 3 3I13 Removal 3 3I13 Installation 3 3I13 Pressure Manifold Check Valve 6 3I16 Removal 6 3I16 Installation 6 3I16 Testing 6 3I16 Timer 6 3I16 Removal 6 3I16 Installation 6 3I16 Deicers Boots Pneumatic Deice System 7 3I17 Removal 7 3I17 Installation 10 3I20 Inspection 15 3J1 Maintenance 16 3J2 Repair Limits 18 3J4 Repair Procedures 19...

Page 672: ...ubleshooting 5 3J23 Components 8 3K2 Deicers i e Heater Boots 8 3K2 Inspection and Testing 8 3K2 Removal and Installation 8 3K2 Brush Modules 9 3K3 Replacement 9 3K3 Alignment 9 3K3 Metal Oxide Varistor MOV Module 10 3K4 Slip Ring Assembly 10 3K4 Replacement 10 3K4 Alignment 10 3K4 Deicer Heater Boot Wiring Harness 12 3K6 Testing 12 3K6 Resistance Test 12 3K6 Ammeter 12 3K6 Using the Ammeter 12 3K...

Page 673: ... is replaced by a Moritz unit The B F Goodrich propeller heat system installed on this airplane uses a single element type heater boots In this type system each heater has one electrothermal heating element When the PROP HEAT switch on the instrument panel is turned ON the timer directs power through the modular brush assembly and slip ring to all the heating elements for approximately 90 seconds ...

Page 674: ...132 thru 4636313 only incorporates the B F Goodrich SMARTbootTM Ice Detection System This system advises the pilot of icing conditions on the empennage of the airplane Electrical sensors integrated directly into the surface of the pneumatic de icers on the vertical fin and right horizontal stabilizer advise the presence of ice and appropriate time to de ice NOTE The system is installed as and perf...

Page 675: ...low B Deice Flow Valve Assembly The deice flow valve assembly is located behind the firewall on the right hand side of the airplane It is mounted to the lower fuselage 1 Removal a Disconnect the electrical leads to the individual deice valves at the three connectors b Disconnect the five hoses from the deice flow valve assembly c Remove the bolts which secure the deice flow valve assembly to the l...

Page 676: ...pect connections Make air leakage test Deicers do not inflate Pressure regulator valves Remove and clean or inflate slowly clogged Deicers inflate slowly Lines partially blocked Blow out lines and normal time 6 seconds or not connected securely inspect connections Make air leakage test Deflate solenoid valves not Ensure that both vent functioning properly ports on solenoid are open System pressure...

Page 677: ...alve Replace flight or vacuum to if necessary the system is inadequate Vacuum line restricted Disconnect line from instruments deflate valve and blow out line Broken line Inspect system and repair CHART 2 Sheet 1 of 2 TROUBLESHOOTING PNEUMATIC DEICE SYSTEM D Vacuum Manifold Check Valve The vacuum manifold check valve is located aft of the forward pressure bulkhead slightly to the right of the airp...

Page 678: ...PAGE 4 Feb 28 07 30 10 00 3I14 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Fluid Diagram of Pneumatic Deicer System Figure 1 Sheet 1 of 2 ...

Page 679: ...PAGE 5 Feb 28 07 30 10 00 3I15 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Fluid Diagram of Pneumatic Deicer System Figure 1 Sheet 2 of 2 ...

Page 680: ...trol valve connection c Slowly apply 20 psig of air pressure to the pressure manifold check valve d Close off regulated air e Check for leaks by noting the pressure drop in the pressure manifold check valve A pressure drop of not more than 5 psig in 10 seconds is permitted f If air flows through the pressure manifold check valve and out the vacuum pump discharge side of the manifold the diaphragm ...

Page 681: ...N AGENCY REGULATIONS CAUTION DO NOT USE MEK ON SMARTBOOTTM INSTALLATIONS VERTICAL FIN AND RIGHT STABILIZER AS MEK WILL ATTACK ESTANE MATERIAL USE TOLUENE INSTEAD NOTE Goodrich Black Standard Pneumatic De Icer Installation Maintenance Repair Manual ATA Report No 30 10 31 provides approved alternate procedures for removing and installing deice boots Reference to it is highly recommended It can be ob...

Page 682: ...ers only use Pure Bristle brush Piper P N 279 142 Neoprene deicers only Solvents CAUTION DO NOT USE MEK ON ESTANE I E SMARTBOOTSTM DEICERS INTENDED FOR REUSE OR CONTINUED USE Item Where Used Toluene Leading edge and deicer cleaning solvent Toluene or Leading edge stripping solvent Peerco 321 stripper or Methyl Ethyl Ketone MEK MEK or Toluene or Acetone Prop deicer removal and tackifying solvent To...

Page 683: ... Application Tool 74 451 209 24 Cement 74 451 210 24 Mixing Cup 74 451 211 24 Mixing Tool 74 451 212 50 Application Template 74 451 K 1 Edge Sealer Kit Black Estane Deicers only 74 451 117 1 1 qt Sealer Cement 74 451 120 4 oz Accelerator 74 451 L 1 Resurfacing Kit 74 451 120 4 oz Accelerator 74 451 122 1 qt Primer 74 451 123 1 qt Resurfacing Coat after P N 74 451 L is applied to a neoprene deicer ...

Page 684: ...llation NOTE Deicers can be installed on alodined or anodized surfaces and over zinc chromate primer that cannot be removed by scrubbing with solvent c Clean the metal surfaces thoroughly at least twice with MEK or Toluene For final cleaning wipe the solvent film off quickly with a clean dry cloth before it has time to dry d Fill gaps of skin splices that lead under deicers with any epoxy compound...

Page 685: ...r suitable non kink hose clamps should be used for this purpose Tighten each clamp with a pair of slip joint pliers but do not squeeze the clamp so tight that the hose is damaged NOTE If non kink hose clamps are not available wrap each hose connection with several turns of friction tape Over the tape wrap two separate bindings of safety wire about one half 1 2 inch apart Each of these bindings sho...

Page 686: ...s j Apply edge sealer using one of the following methods appropriate to the deicer installed 1 A 56 B Neoprene deicers only a Apply masking tape on deicer surface around deicer and cutouts at least 1 4 inch from edge If edge filler has been used make sure masking tape applied on deicer is at least 1 16 1 4 inch in from edge filler b Apply masking tape on leading edge one eighth 1 8 to one quarter ...

Page 687: ...ING TACKIFICATION FOR SAME REASON g Beginning on the upper spanwise edge of deicer tackify backside of strip side without peel ply with MEK in a fifteen 15 to twenty 20 inch length and press strip onto cemented area between tape lines Make sure strip contacts deicer surface and leading edge surface Remove peel ply on breeze side of strip and roll with rubber roller Continue until one side of deice...

Page 688: ...ot material cemented to the wing skin adjacent to installed boot following the identical procedure used for installation Leave one inch of the strip uncemented to attach a clamp Four 4 hours or more after the installation attach a spring scale to the un cemented end of each strip and measure the force required to remove strip at the rate of one inch per minute The pull should be applied 180 to the...

Page 689: ...IS PERMITTED b Repair surface damage detected per Repair Procedure below c Inflate deicer with regulated air source to correct operating pressure see Chart 3 Check inflation time Deicer should inflate to operating pressure within six 6 seconds d When deicer has reached operating pressure seal off deicer at air connection Check deicer pressure after 60 seconds Pressure drop should not exceed three ...

Page 690: ...SPRAYING USE WITH ADEQUATE VENTILATION AVOID PROLONGED BREATHING OF VAPOR IF DIZZINESS OR NAUSEA OCCURS OBTAIN FRESH AIR AVOID CONTACT WITH SKIN AND EYES IF EYE CONTACT OCCURS FLUSH EYES WITH WATER FOR 15 MINUTES THEN SEE PHYSICIAN IF SKIN CONTACT OCCURS WASH THOROUGHLY WITH SOAP AND WATER EMPTY CONTAINERS MAY CONTAIN FLAMMABLE OR EXPLOSIVE RESIDUAL VAPORS SEE MSDS FOR ADDITIONAL SAFETY INFORMATIO...

Page 691: ...st be removed before reapplication to avoid dulling or product build up 2 Apply light even coat of ShineMaster cosmetic treatment to deicer with clean lint free cloth wiping in one direction Let dry to touch about 5 15 minutes 3 Repeat Step 2 above once or twice to obtain desired shine c Icex II Application Icex II is an ice adhesion inhibitor that enhances deicer performance by lowering adhesion ...

Page 692: ...ERS MUST BE REPLACED IF 1 CUTS TEARS OR RUPTURES CUT THE INFLATABLE TUBE FABRIC AND OR EXCEED 4 X 9 INCHES OR 2 BROKEN STITCHES OR THREADS ARE APPARENT OR 3 DAMAGE LEAKS AIR AND EXCEEDS THE PATCH AND PINHOLE REPAIR LIMITS SPECIFIED BELOW NOTE In addition to meeting these repair limits the deicer must also pass the Inspection Pneumatic Deicers Boots Procedure below NOTE If patches and pinhole repai...

Page 693: ...EICER TUBES FAILURE TO DO SO MAY RESULT IN PATCH LIFTING WHEN DEICER INFLATES CAUTION PREPARATION OF DEICER SURFACE TO BE PATCHED IS CRUCIAL FOR GOOD PATCH ADHESION FAILURE TO REMOVE SHINEMASTER COSMETIC TREATMENT WAX GREASE OIL ICEX II AND OTHER CONTAMINANTS COMPLETELY CAN RESULT IN POOR PATCH ADHESION a Trim standard patch sizes to accommodate small areas of damage leaving at least 1 2 inch beyo...

Page 694: ...ation template with hole centered over pinhole e Open foil overpack of 74 451 209 cement Clip corner of Appli pak pouch and squeeze cement into mixing cup Make sure that all material from pouch is squeezed into mixing cup to assure proper mix ratio with accelerator CAUTION RECAP ACCELERATOR TIGHTLY AFTER USE AS ACCELERATOR WILL HARDEN IF NOT SEALED COMPLETELY f Add seven 7 drops of P N 74 451 201 ...

Page 695: ...e soap residue and loose particles raised from sanding CAUTION DO NOT USE MEK ON ESTANE SURFACE DEICERS AS MEK WILL ATTACK ESTANE 6 Wipe surface twice with cleaning solvent Use MEK or Toluene on neoprene deicers use only Toluene on Estane deicers 7 Apply masking tape to leading edge against edges of deicer 8 Apply primer a For Estane deicers skip to step 9 b For neoprene deicers only 1 Mix primer ...

Page 696: ... 20 inches Hg with engine operating at idle and 2 000 rpm In S N s 4636001 thru 4636131 check that vacuum gauge indication does not exceed 5 2 inches Hg with both pumps operating and both regulators connected If indication exceeds 5 2 inches readjust the left and right vacuum regulators per B and C above to provide an indication of no more than 5 2 inches Hg E Check all surface boots and ensure th...

Page 697: ...ice and appropriate time to deice are measured by the sensor installed within the vertical fin deicer only The sensor within the right horizontal stabilizer deicer advises the status of the detection system ice detect fail annunciator These annunciators located within the annunciator panel make up the visual cues of the deice detector deicer system The select de ice annunciator illuminates when ap...

Page 698: ...res of the 3E3302 1 test strip over the five sensors in the vertical fin boot and tape in place or thoroughly saturate two cloths small dish towel size with tap water and place over the vertical fin sensor 6 The amber SELECT DE ICE light should illuminate NOTE The amber SELECT DE ICE light may take approximately ten minutes to illuminate while the controller steps through the ice thickness measure...

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Page 701: ...standard pitot ice protection consists of a heated pitot head located on the lower side of both the left and right wing a switch on the De ice Switch Panel S N s 4636001 thru 4636131 only or Environmental Deice Switch Panel S N s 4636132 and up a 10 amp circuit breaker a relay and the circuit wiring B Removal Installation and Testing See 34 10 00 ...

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Page 703: ...NG HEATED WINDSHIELD SYSTEM WINDOWS AND WINDSHIELDS Heated Windshield See Figure 1 When installed the heated windshield consists of an electrically heated left windshield Circuit protection is provided by the windshield heat CONTROL and POWER breakers in the ICE PROTECTION section of the pilot s circuit breaker panel A Troubleshooting See Chart 1 B Testing CAUTION AMBIENT TEMPERATURE OF WINDSHIELD...

Page 704: ...PAGE 2 Feb 28 07 30 40 00 3J16 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Windshield Heat Figure 1 Effectivity 4636021 thru 46360131 shown ...

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Page 706: ...PAGE 4 Feb 28 07 30 40 00 3J18 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 707: ...e and the ship s ammeter will show an increase In flight the PROP HEAT switch flashes at a slow rate during the 90 second off cycle and is continuously illuminated during the 90 second ON cycle The propeller heat system consists of the following In S N s 4636001 thru 4636131 electrically heated deicers bonded to the propeller blades slip ring assemblies connected to the propeller hub to distribute...

Page 708: ...mmeter If low ammeter at zero replace output and input satis the ammeter factory replace ammeter If no voltage to ammeter locate and fix open between switch and ammeter Open ammeter to timer Disconnect harness at timer and check voltage at Pin B of harness to ground If none locate and correct open Ammeter shows normal Open in wiring between Use heat test to find current part of cycle timer and bru...

Page 709: ...o deicers for loose or corroded connections and partially broken wiring Correct as required Ammeter shows low current Aircraft voltage low Check voltage into switch over entire cycle Ammeter faulty Test for voltage up to and out of ammeter If low output and input satis factory replace ammeter If no voltage to ammeter locate and fix open between switch and ammeter High resistance up to Check for pa...

Page 710: ...st timer Ammeter does not flick Timer ground open timer Disconnect harness at approximately every 90 not cycling timer and check with seconds ohmmeter from Pin G of harness to ground If no circuit fix open per schematic diagram Timer contacts are Test timer If timer welded caused by short does not cycle with voltage circuit in system at Pin B replace timer but be sure short causing original failur...

Page 711: ...alignment Loose connection Refer to Ammeter flicks between 90 second phase period Switch or circuit breaker Place jumper wire across faulty switch or circuit breaker If radio noise disappears replace the switch or circuit breaker Wiring located too close to Relocate deicer wiring at radio equipment or associated least 8 inches away from wiring radio equipment and wiring Rapid brush wear or Brush b...

Page 712: ...PAGE 6 Feb 28 07 30 60 00 3J24 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Propeller Heat System Installation Figure 2 Effectivity 4636001 thru 4636131 shown ...

Page 713: ...t Figure 3 A A PROPELLER HUB ASSEMBLY VIEW B B VIEW A A B B COCKING OF BRUSHES TO SLIP RING SURFACE 2 0 0 30 ADD WASHERS AS REQUIRED TO ALIGN BRUSHES MOV MODULE NOT INSTALLED IN S N S 4636001 THRU 4636131 031 094 IN S L I P R I N G R O T A T I O N VIEW LOOKING LEFT MODULAR BRUSH ASSEMBLY SLIP RING TO PROP DEICE BOOTS 101124A ...

Page 714: ...OODRICH PROPELLER DE ICERS ARE NOT REPAIRABLE DEICER SURFACE DAMAGE SUCH AS PUNCTURES CUTS SCUFFS EROSION THAT EXPOSES THE WIRE OR ETCHED ELEMENT IS GROUNDS FOR REPLACEMENT AS ADDITION OF REPAIR MATERIAL COULD AFFECT DEICER PERFORMANCE CAUTION DISPOSE OF UNUSED MEK AND OTHER CHEMICALS AND SOLVENTS IN A MANNER CONSISTENT WITH LOCAL LAWS AND OR ENVIRONMENTAL PROTECTION AGENCY REGULATIONS 1 Inspectio...

Page 715: ...ttachment hardware and disconnecting the engine wire harness b Remove assembly screws and separate modules and spacers NOTE The part number of each module is etched into the surface of the plastic housing replace with the same part number module c Restack modules and spacer as shown in Figure 3 NOTE Ascertain flat washer is positioned between star washer and housing d Reconnect aircraft wire harne...

Page 716: ...out will result in severe arcing between the slip ring and brushes and will cause rapid brush wear If the run out is not corrected rapid deterioration of the slip ring and brush contact surfaces will result and lead to eventual failure of the heating system Check the slip ring run out with a dial indicator securely attached to the engine with the pointer resting on the slip ring See Figure 5 Rotat...

Page 717: ...PAGE 11 Feb 28 07 30 60 00 3K5 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Deicer Wiring Harness Installation Figure 6 ...

Page 718: ...ine incorrect resistance short or open at the brush to slip ring contact disconnect harness at the timer and use low range ohmmeter to read resistance from each deicer circuit lead Pins C D E and F of harness plug to ground it should read 58 to 67 If this reading is not obtained disconnect the deicer lead straps to measure deicer resistances individually Individual deicer should be 1 15 to 1 33 If...

Page 719: ...sts are satisfactory circuit breaker and switch are functioning correctly If testing is unsatisfactory and timer and ammeter check out satisfactorily repair or replace circuit breaker and or switch C Propeller Deicers i e Heater Boots 1 Final Electrical Check a Verify that deicers are installed so that blades can be moved throughout the entire blade pitch range without placing deicer leads or stra...

Page 720: ...e been checked connect a jumper wire from Pin B of harness to B contact of timer socket to power timer Connect a jumper wire from Pin G of harness to G contact of timer socket to complete the power circuit Now use voltmeter from ground to the timer socket and check that timer is cycling to deliver system voltage to the C contact Voltage must be delivered for approximately 90 seconds 3 If the timer...

Page 721: ...or interference occurs with PROP HEAT switch ON and disappears when switch is OFF refer to troubleshooting chart 3 Ascertain that all clamps clips mountings and electrical connections are tight Check for loose broken or missing safety wire 4 Deicers Closely check deicers for wrinkled loose or torn areas particularly around the outboard end Check that terminals and terminal studs are not shorting o...

Page 722: ...eck for proper clearance of brush block to slip rings see Figure 3 Loosen mounting screws and move in elongated holes to correct block position and tighten securely c Visually check brush block for 2 angle of attack see Figure 3 If not loosen mounting screws and twist block but be sure to hold clearance limits shown when tightening 1 Note direction of slip ring rotation 2 Place template against fa...

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Page 724: ...PAGE 18 Feb 28 07 30 60 00 3K12 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL GRIDS 3K12 THRU 3L24 INTENTIONALLY BLANK ...

Page 725: ...PART NUMBER 761 876 February 28 2007 4A1 AIRPLANE MAINTENANCE MANUAL CARD 4 OF 9 PA 46 350P S N s 4636001 AND UP PIPER AIRCRAFT INC ...

Page 726: ...4A2 Published by Technical Publications Piper Aircraft Inc 2926 Piper Drive Vero Beach Florida 32960 U S A Member General Aviation Manufacturers Association ...

Page 727: ...2 3 4 5 and 6 CR981223 December 23 1998 1 2 3 4 5 and 6 PR000201 February 1 2000 1 2 3 4 5 and 6 PR010515 May 15 2001 1 CR050730 July 30 2005 1 2 3 4 5 6 7 and 8 PR060207 February 7 2006 1 2 3 4 5 6 7 and 8 CR070228 February 28 2007 1 2 3 4 5 6 7 8 and 9 COMPLETE REVISION OF MAINTENANCE MANUAL 761 876 Revisions appear in all Aerofiche Cards Accordingly discard your entire existing Aerofiche Card S...

Page 728: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 1 Feb 28 07 AEROFICHE EFFECTIVITY 4A4 THIS PAGE INTENTIONALLY BLANK ...

Page 729: ...Feb 28 07 Intro Table of Contents 1 Feb 28 07 2 Feb 28 07 Introduction 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 Index 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHA...

Page 730: ...PAGE 2 Feb 28 07 INTRO LIST OF EFFECTIVE PAGES 4A6 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 731: ...A9 Effectivity 2 4A10 Serial Number Explanation 2 4A10 Assignment of Subject Material 2 4A10 Pagination 3 4A11 Aerofiche Effectivity 3 4A11 Identifying Revised Material 3 4A11 Indexing 3 4A11 List of Effective Pages 3 4A11 Warnings Cautions and Notes 3 4A11 Accident Incident Reporting 4 4A12 Supplementary Publications 4 4A12 Piper Publications 4 4A12 Vendor Publications 4 4A12 Chapter Section Inde...

Page 732: ...PAGE 2 Feb 28 07 4A8 INTRO CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 733: ...GENUINE PIPER AIRCRAFT PARTS OR PIPER AIRCRAFT APPROVED PARTS OBTAINED FROM PIPER APPROVED SOURCES IN CONNECTION WITH THE MAINTENANCE AND REPAIR OF PIPER AIRPLANES Genuine PIPER parts are produced and inspected under rigorous procedures to ensure airworthiness and suitability for use in PIPER airplane applications Parts purchased from sources other than PIPER even though identical in appearance ma...

Page 734: ...ane are broken down into subsystems These sub systems are identified by the second element of the standard numbering system The element 40 of the number 28 40 01 concerns itself with the indicating section of the fuel system C Unit Subject The individual units within a sub system section may be identified by the third element of the standard numbering system The element 01 of the number 28 40 01 i...

Page 735: ...his set 8 Identifying Revised Material A revision to a page is defined as any change to the printed matter that existed previously Revisions additions and deletions are identified by a vertical line i e change bar along the left hand margin of the page opposite only that portion of the printed matter that was changed A change bar in the left hand margin opposite the footer i e chapter section subj...

Page 736: ...s Catalog P N 761 878 2 Periodic Inspection Report Form P N 767 011 3 Progressive Inspection Manual 50 hour P N 767 013 B Vendor Publications WARNING FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION S WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT MAY RENDER THE AIRCRAFT UNAIRWORTHY 1 AIR CONDITIONING COMPRESSOR Vendor Address Sanden International USA Inc PH 972 442 8400...

Page 737: ...cialty Systems PH 330 374 3040 Goodrich Corporation FAX 330 374 2290 1555 Corporate Woods Parkway Uniontown Ohio 44685 8799 Technical Assistance PH 800 334 2377 330 374 3743 FAX 330 374 2290 Email dssd support goodrich com http www deicingsystems goodrich com Black Standard Pneumatic De Icer Installation Maintenance and Repair Manual ATA 30 10 31 SmartBoot System ATA 30 10 65 8 ELECTRONIC FLIGHT I...

Page 738: ...ntext See www avantext com or PH 800 998 8857 11 FIRE EXTINGUISHER PORTABLE Vendor Address H3R Inc PH 800 249 4289 43 Magnolia Ave 4 San Francisco California 94123 2911 http www h3r com index htm 12 FORCE APPLICATOR KIT Vendor Address Safe Flight Instrument Corp PH 914 946 9500 20 New King Street White Plains New York 10602 13 FUEL BOOST PUMP Vendor Address Parker Hannifin Corp PH 800 272 7537 Nic...

Page 739: ...ww unisonindustries com index4 html Installation Operation F1100 MASTER SERVICE MANUAL and Maintenance 4300 6300 SERIES MAGNETO MAINTENANCE AND Instructions OVERHAUL MANUAL L 1363 19 NAVIGATION COMMUNICATIONS AND GPS NAV COM GPS Vendor Address Garmin International PH 913 397 8200 1200 East 151ST Street Olathe KS 66062 http www garmin com 20 OXYGEN SYSTEM Vendor Address Scott Aviation PH 716 683 51...

Page 740: ...DAR WEATHER RDR 2000 Vendor Address Honeywell Bendix King See Autoflight above Maintenance Manual Bendix King ART 2000 P N 006 05332 0001 25 RADIO COOLING BLOWER Vendor Address Globe Motors PH 937 228 3171 2275 Stanley Ave FAX 937 229 8531 Dayton Ohio 45404 http www globe motors com home html 26 STARTER Vendor Address Kelly Aerospace See Alternator above or Sky Tec Partners Ltd PH 800 476 7896 350...

Page 741: ...MALIBU MIRAGE MAINTENANCE MANUAL 28 VACUUM PUMP Vendor Address Aero Accessories Inc PH 800 822 3200 1240 Springwood Avenue Gibsonville NC 27249 http www aeroaccessories com index html 29 VACUUM REGULATORS Vendor Address Parker Hannifin Corp see Fuel Boost Pump above ...

Page 742: ...PAGE 10 Feb 28 07 INTRODUCTION 4A18 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 743: ...chapter CHAPTER SECTION TITLE GRID NO 4 AIRWORTHINESS LIMITATIONS 1C1 00 Airworthiness Limitations 5 TIME LIMITS MAINTENANCE CHECKS 1C9 00 General 10 Time Limits 20 Scheduled Maintenance Checks 30 Special Inspections 50 Unscheduled Maintenance Checks 6 DIMENSIONS AND AREAS 1E13 00 General 7 LIFTING AND SHORING 1F1 10 Jacking 8 LEVELING AND WEIGHING 1F9 10 Weighing and Balancing 20 Leveling 9 TOWIN...

Page 744: ...emperature Control 22 AUTOFLIGHT 2F11 10 Autopilot 23 COMMUNICATIONS 2G19 00 General 50 Audio Integrating 60 Static Discharging 24 ELECTRICAL POWER 2H11 00 General 30 DC Generation 40 External Power 60 Electrical Load Distribution 25 EQUIPMENT FURNISHINGS 2J11 10 Flight Compartment 20 Passenger Compartment 50 Cargo Compartments 60 Emergency 26 FIRE PROTECTION 2K15 20 Extinguishing 27 FLIGHT CONTRO...

Page 745: ...rs 60 Propellers Rotors 31 INDICATING RECORDING SYSTEMS 4C1 50 Central Warning Systems 32 LANDING GEAR 4C13 00 General 10 Main Gear and Doors 20 Nose Gear and Doors 30 Extension and Retraction 40 Wheels and Brakes 50 Steering 60 Position and Warning 33 LIGHTS 4G5 10 Flight Compartment 20 Passenger Compartment 30 Cargo and Service Compartments 40 Exterior 34 NAVIGATION 5C1 00 General 10 Flight Envi...

Page 746: ...00 General 10 Investigation Cleanup and Aerodynamic Smoothness 70 Repairs 80 Electrical Bonding 52 DOORS 6G13 10 Passenger Crew 20 Emergency Exit 30 Cargo 70 Monitoring and Operation 55 STABILIZERS 6H13 00 General 10 Horizontal Stabilizers 20 Elevator 30 Vertical Stabilizer 40 Rudder 56 WINDOWS 6I19 00 General 10 Flight Compartment 20 Cabin 30 Door 57 WINGS 6K5 40 Attach Fittings 50 Flight Surface...

Page 747: ... Power Supply 20 Distribution 76 ENGINE CONTROLS 7G17 10 Power Control 77 ENGINE INDICATING 7H3 10 Power 20 Temperature 40 Integrated Engine Instrument Systems 79 OIL 7J3 20 Distribution 30 Indicating 80 STARTING 7J15 10 Cranking 81 TURBINES 7K9 20 Turbo Supercharger 91 CHARTS WIRING DIAGRAMS 8C1 10 Charts 21 and up Electrical Schematics 91 CONT CHARTS WIRING DIAGRAMS CONT 9C1 Electrical Schematic...

Page 748: ...PAGE 16 Feb 28 07 INTRODUCTION 4A24 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 749: ...sion Control Wing 6L3 Attitude Indicator 5D5 Autopilot 2F17 Component Locator 2G2 Installation 2F18 2F20 Maintenance 2F23 Operational Checkout 2F24 Pitch Servo 2G12 Pressure Transducer 2G6 Roll Servo 2G4 Servo Clutch Torque Adjustment 2G15 Trim Monitor 2G3 Trim Servo 2G6 Yaw Amplifier 2G14 Yaw Servo 2G10 Avionics Cooling 2C14 Avionics Master Switch 2H1 B Ball Diameters for Testing Hose Restriction...

Page 750: ...rrection 2I10 Troubleshooting 2I7 2I13 Valve Regulated Lead Acid 2I13 Bonding 6G9 Resistance Index 6G10 Buses Avionics 2H19 Main 2H19 Circuit Breaker Panel 6D22 Electrical Shelf 6E7 External Power 2I19 Load Distribution 2J1 Relay Installation Co Pilot s Side 6E10 K1 thru K8 6E10 Pilot s Side 6E9 Schematics Air Conditioning 8E7 Airspeed Standby 9E19 Altimeter Radar 9F14 Altimeter Standby 9E19 Annun...

Page 751: ...n Light 9E5 WX 500 9F11 XM Receiver 8E23 Switch Panels 6E1 Symbols 8D14 System 2H17 Troubleshooting 2H20 Tie Bus Panel Connections 6E3 Volt Ammeter 2J4 Voltage Regulation and Control 2H19 Wire Coding 8D13 Elevator Balancing 6I3 Control System Installation 3D23 Rigging and Adjustment 3D24 Troubleshooting 3D19 Torque Tube Bearing Changes 3D20 Trim Controls Actuator Assembly 3E3 Corrosion Control 3E4...

Page 752: ...Drain Valve 3G8 Draining 1I19 Draining Moisture 1I18 Fuel Filter 3G7 Fuel Pumps Specifications 3G5 Fuel Quantity Gauge Accuracy Test 3G14 Full Range Check 3G20 Senders 3G13 Leak Test Setup 3G1 Selector Switch and Valve 3G6 Cable Adjustment 3G7 Troubleshooting 3F16 Leak Evaluation 3F22 G GMA 340 Audio Panel Adjustments 2H6 Installation 2H3 System Functional Test 2H4 GNS 430 5F5 GNS 530 5F5 Ground C...

Page 753: ... 4D11 Position and Warning 4F19 Landing Gear Up Power Reduced Warning Switch Adjustment 4G2 Troubleshooting 4F20 Leading Particulars and Principal Dimensions 1E20 Leveling 1F17 Life Limited Parts 1C7 Lifting 1F7 See also 57 40 00 Lights Exterior 4H3 Landing 4H7 Position 4H4 Pulse 4H7 Strobe 4H3 Taxi 4H6 Wing Inspection Light 4H7 Interior 4G11 Annunciator Panel 4G12 Baggage Area 4G21 Forward 4H1 Re...

Page 754: ...g 3K6 Troubleshooting 3J20 Propeller Assembly 7C9 Publications Piper A12 Vendor A12 Q Quad Digital Indicator QDI See Engine Instruments Transicoil EMIS R Radar 5F1 Repairs Fiberglass 6F19 Metal Wire Stitching 6G5 Thermoplastic 6F21 List of Materials 6F24 Window Windshield Acrylic 6J10 Restraint System 2J23 Inertial Reel Adjustment 2J23 Inspection 2J23 Revised Material A11 Robinair 34700 Charging S...

Page 755: ... Bellcrank Centering 4C22 Horn Arm Gap 4C22 Nose Wheel Centering 3C15 4C22 Rudder Pedal Neutral Alignment 3C15 4C22 Rudder Travel Tool 3C15 Torque Conversion 8C20 Torque Wrench Formula 1K2 Towing 1G5 Transponder 5F9 GTX 327 5F9 GTX 330 5F9 Post Installation Setup Procedure 5F10 ARINC 429 Configuration Page 5F11 Display Mode and Key Lighting 5F11 Hexadecimal Conversion 5F13 Operation Configuration ...

Page 756: ...in 6I11 Vertical Speed Indicator 5C18 Volt Ammeter See Electrical W Warnings Cautions and Notes A11 Weather Radar 5F1 Weighing 1F15 Wheel Brake Assembly 4F4 Wheels Bearing Cup 4F4 Main Wheel Assembly 4F2 Nose Wheel Assembly 4F1 Repairs 4F3 Windows and Windshields Door Window 6K3 Heated Windshield Testing 3J15 Troubleshooting 3J15 Inspection and Repair Definitions 6J1 Limitations 6J1 Crack Limitati...

Page 757: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 9 Feb 28 07 INDEX 4B9 THIS PAGE INTENTIONALLY BLANK ...

Page 758: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 10 Feb 28 07 INDEX 4B10 GRIDS 4B10 THRU 4B24 INTENTIONALLY BLANK ...

Page 759: ...4C1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 31 INDICATING RECORDING SYSTEMS ...

Page 760: ...4C2 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 761: ...IRAGE MAINTENANCE MANUAL CHAPTER SECTION PAGE DATE 31 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 31 Table of Contents 1 Feb 28 07 2 Feb 28 07 31 50 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 CHAPTER SECTION PAGE DATE CHAPTER 31 LIST OF EFFECTIVE PAGES ...

Page 762: ...PAGE 2 Feb 28 07 31 LIST OF EFFECTIVE PAGES 4C4 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 763: ...350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 31 INDICATING RECORDING SYSTEMS TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO CENTRAL WARNING SYSTEMS 31 50 00 1 4C7 Annunciator 1 4C7 Annunciator Removal and Installation 3 4C9 Lamp Replacement 3 4C9 Wiring 3 4C9 ...

Page 764: ...PAGE 2 Feb 28 07 4C6 31 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 765: ...luminates if a fuel quantity difference of greater than 10 gallons is detected for more than 60 seconds between the left and right tanks Remains lighted until the imbalance is corrected GEAR WARN On the ground illuminates when the landing gear selector is placed in the UP position with the aircraft weight still on the gear In the air illuminates when the gear is in transit when all three gear are ...

Page 766: ...isory only STALL WARN FAIL Illuminates if the lift computer fails and or the STALL WARN circuit breaker trips STARTER ENGAGE Illumination during engine cranking is normal Illumination at any other time indicates a problem SURFACE DE ICE Illuminates when the de ice boots inflate i e when the SURFACE DE ICE switch is depressed and the pneumatic de ice system cycles in sequence tail lower wing upper ...

Page 767: ...131 Effectivity 4636132 thru 4636313 less 4636299 VACUUM NO 1 INOP ALTERNATOR NO 1 INOP ALTERNATOR NO 2 INOP PROP DE ICE FAIL VACUUM NO 2 INOP BOOST PUMP GEAR WARN OXYGEN OIL PRESS FUEL PRESS DOOR AJAR HYDRALIC PUMP LOW BUS VOLTAGE FLAPS ANNUNC INOP PITOT HEAT OFF INOP CABIN ALTITUDE STARTER ENGAGE FUEL IMABLANCE STALL WARN FAIL WINDSHIELD HEAT FAIL SURFACE DE ICE Annunciator Panel Figure 4 Effect...

Page 768: ...VAC 1 INOP FUEL IMBALANCE ANNUN INOP PITOT HTR OFF VAC 2 INOP SURF DE ICE BOOST PUMP WINDSHLD HTR FAIL R PITOT HEAT FLAPS ALT NO 2 INOP DOOR AJAR START ENGAGE RED AMBER GREEN TEST FUEL PRESS PRP DE ICE FAIL L PITOT HEAT GEAR WARN ALT NO 1 INOP LOW BUS VOLTS CABIN ALT STALL WRN FAIL OIL PRESS OXYGEN HYD PUMP VAC 1 INOP FUEL IMBALANCE ANNUN INOP PITOT HTR OFF VAC 2 INOP SURF DE ICE BOOST PUMP WINDSH...

Page 769: ...PAGE 5 Feb 28 07 4C11 31 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 770: ...PAGE 6 Feb 28 07 4C12 31 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 771: ...4C13 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 32 LANDING GEAR ...

Page 772: ...4C14 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 773: ... Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 CHAPTER SECTION PAGE DATE 32 30 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 19 F...

Page 774: ...PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 32 LIST OF EFFECTIVE PAGES continued 32 60 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHAPTER SECTION PAGE DATE CHAPTER SECTION PAGE DATE ...

Page 775: ...leaning Inspection and Repair 6 4D4 Adjustment 7 4D5 Alignment 7 4D5 Main Gear Tolerances 7 4D5 Main Gear Door Assembly 10 4D8 Removal 10 4D8 Installation 10 4D8 Cleaning Inspection and Repair 10 4D8 NOSE GEAR AND DOORS 32 20 00 1 4D11 Troubleshooting 1 4D11 Nose Gear Oleo 3 4D13 Disassembly 3 4D13 Assembly 3 4D13 Cleaning Inspection and Repair 5 4D15 Nose Gear Assembly 6 4D16 Removal 6 4D16 Insta...

Page 776: ...ment Parker Hannifin only 17 4E17 Emergency Gear Release Valve 18 4E18 Removal 18 4E18 Installation 18 4E18 Parker Hannifin Valves Only 19 4E19 Disassembly 19 4E19 Assembly 19 4E19 WHEELS AND BRAKES 32 40 00 1 4F1 Nose Wheel Assembly 1 4F1 Removal and Disassembly 1 4F1 Assembly and Installation 1 4F1 Inspection 2 4F2 Main Wheel Assembly 2 4F2 Removal and Disassembly 2 4F2 Assembly and Installation...

Page 777: ...G 32 50 00 1 4F15 Steering Pushrod 1 4F15 Removal 1 4F15 Installation 1 4F15 Steering Bellcrank 1 4F15 Removal 1 4F15 Installation 1 4F15 Bungee Assembly 1 4F15 Removal 1 4F15 Installation 2 4F16 Steering Pushrod Bellows 2 4F16 Removal 2 4F16 Installation 2 4F16 Steering Arm 2 4F16 Removal 2 4F16 Installation 2 4F16 POSITION AND WARNING 32 60 00 1 4F19 Troubleshooting 1 4F19 Nose Gear 4 4F22 Up Li...

Page 778: ...PAGE 4 Feb 28 07 4C20 32 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 779: ...also sound if the flaps are extended beyond approach position if the gears are not down and locked The red gear unsafe light also operates simultaneously with the warning horn Their primary purpose is to give warning when power is reduced below 15 1 In Hg manifold pressure and the landing gear has not reached the down and locked position This circuit is controlled by three 3 paralleling down limit...

Page 780: ...mber Piper P N Rudder Pedal Neutral Alignment Tool HF 622724 762 151 Nose Wheel Centering i e Neutral Tool HF 622722 762 147 Nose Gear Steering Bellcrank Centering i e Neutral Tool TL 622723 762 148 Nose Gear Steering Horn Arm Gap Tool TL 690672 N A Nose Gear Actuator Alignment Tool TL 690672 762 137 Nose Gear Downspring Disassembly Reassembly Tool SK VB1152 762 155 Nose Gear Downspring Remove Ins...

Page 781: ...t taxi tire if necessary takeoff or landing Worn or loose wheel Replace and or adjust bearings wheel bearings Worn torque link bolts Replace bolts and or and or bushings bushings Excessive or uneven Incorrect operating pressure Inflate tire to correct wear on main tires pressure Wheel out of alignment Check wheel alignment toe in or out Hydraulic actuator out of Check gear adjustment adjustment al...

Page 782: ...PAGE 2 Feb 28 07 4C24 32 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Main Gear Oleo Strut Assembly Figure 1 ...

Page 783: ...fluid and install it on the plug Lubricate the inside wall of the piston tube Insert the plug into the top of the piston tube and push it down the tube Align the bolt holes of the fork tube and plug Then install the bolt assembly 3 If desired cement a cork in the hole in the bottom of the fork body to prevent dirt from entering between the fork and tube 4 To assemble components of orifice tube ins...

Page 784: ...n e Fork tube for corrosion scratches nicks dents and misalignment f Air valve for general condition 3 Repair of the oleo is limited to smoothing out minor scratches nicks or dents and replacement of parts 3 Main Gear Assembly A Removal 1 Place the airplane on jacks 2 Disconnect locking actuator from strut housing 3 Disconnect brake line at its upper end in the wheel well 4 Disconnect gear door ac...

Page 785: ...PAGE 5 Feb 28 07 4D3 32 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Main Gear Installation Figure 2 ...

Page 786: ...ugh strut support and trunnion pin Secure bolt with nut and washers d Repeat steps b and c for remaining trunnion pin and strut support 2 Attach the gear door actuating rod to the gear housing 3 Connect brake line at its upper end in the wheel well 4 Connect locking actuator to gear housing 5 Ensure that the landing gear is lubricated per Lubrication Chart 3 12 20 00 6 Check the alignment of the w...

Page 787: ...of the center pivot bolt of the gear torque links Devise a support to hold the straightedge in this position 2 Set a square against the straightedge and check to see if its outstanding leg bears on the front and rear side of the brake disc It may be necessary to remove the brake assembly to have clear access to the disc If it touches both forward and rear flanges the landing gear is correctly alig...

Page 788: ... UNDER NUT BOLT 0 AN960 416 AN960 416 3 14 0 33 AN960 416 AN960 416 AN960 416 2 14 0 48 AN960 416L AN960 416 AN960 416 14 AN960 416 1 04 AN960 416 2 AN960 416 AN960 416 14 1 19 AN960 416L AN960 416L AN960 416 14 AN960 416 2 1 35 AN960 416 3 AN960 416 AN960 416 2 15 2 05 AN960 416 4 AN960 416 AN960 416 15 Max Allow AN960 416L Washers 031 Thick AN960 416 Washers 062 Thick Aligning Main Gear Figure 3...

Page 789: ... 1 Dimension 1 Tolerance Remarks 1 82695 59 Upper Actuator 439 Attachment Bushing 437 3 16DU24 Trunnion Pin Bushing 4 Lower Trunnion 314 NOTES 2 3 FF411 4 Bushing 315 5 31796 Torque Link 3760 NOTE 2 Bushing 3745 6 67026 7 Strut 313 NOTES 2 3 Bearing 314 NOTES 1 All dimensions are inside dimensions ID unless otherwise noted 2 Line ream to this dimension after installation of part 3 Press fit ...

Page 790: ... insert the hinge pins The pins should be installed with the safety wire holes towards the center line of the door 2 Ensure that the ends of the pins which have the safety wire holes protrude approximately 1 4 inch from the hinges Safety the pins to the wing with MS20995 C41 safety wire 3 Attach the door retraction rod to the door with the previously removed bolt washers and nut C Cleaning Inspect...

Page 791: ...PAGE 11 Feb 28 07 4D9 32 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 792: ...PAGE 12 Feb 28 07 4D10 32 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 793: ...ure Wear resulting from shimmy Refer to preceding trouble for correction Nose gear fails to Oleo cylinder binding Lubricate strut housing steer properly in strut housing refer to 12 10 00 Cylinder and or strut housing Determine cause and bushings damaged correct One brake dragging Determine cause and correct Rollers not engaged Metal Determine cause and to metal in Gear Down correct Position Steer...

Page 794: ...ten when sheared landing gear retracts Damaged guide Replace guide Strut bottoms on normal Insufficient air and or Service strut with air landing or taxiing on rough fluid in strut and or fluid ground Defective internal parts Replace defective parts in strut Landing gear doors fail Landing gear not retracting Check adjustment of to completely close completely gear Door retraction mechanism Check a...

Page 795: ...ach up along the tube and release the snap ring from the annular slot at the bottom of the strut c Pull the piston tube with its component parts from the strut d The piston tube components may be removed from the piston tube by removing the retainer from the annular slot at the top of the piston tube e Slide the bearing assembly with inner O ring and teflon retainer wiper ring washer and snap ring...

Page 796: ...PAGE 4 Feb 28 07 4D14 32 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Nose Gear Oleo Strut Assembly Figure 1 ...

Page 797: ...ks Lubricate the torque link bolts and tighten them only tight enough to allow no side play in the links yet still be free enough to rotate 10 Ensure that the two thrust washers with their coated surfaces together are installed in place on the lower portion of the strut immediately above the boss where the upper torque link attaches to the strut 11 Slide the strut assembly up into the trunnion Ens...

Page 798: ...free 2 Connect the actuator and emergency down mechanism to the right hand side of the trunnion with the previously removed bolt spacers and washers Safety the bolt to the trunnion with MS20995 C41 safety wire Remove the down spring retaining tool 3 Cycle the gear a minimum of three times to ensure proper operation 4 Ascertain that gear is lubricated per 12 20 00 Chart 4 5 Check the adjustment of ...

Page 799: ...PAGE 7 Feb 28 07 4D17 32 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Nose Gear Installation Figure 2 ...

Page 800: ... NO LOAD ON SPRINGS ADJUST LENGTH AS REQUIRED FOR STRAIGHT AHEAD NOSE WHEEL ALIGNMENT TIGHTEN JAM NUTS STA 0 0 TO 0 5 ENGINE MOUNT BUNGEE SEE NOTE WASHERS NAS1149F0863P AND NAS1149F0832P OR NAS1149F0863P AS REQUIRED LOCKING ASSY STEERING ARM STEERING ARM VlEW B B VlEW A A VIEW C NOSE GEAR ACTUATING CYLINDER BELLCRANK SEE VIEW C MOUNT PLATE DOWN SPRING STEERING HORN PADS MOUNT PLATE NOTE TORQUE BOL...

Page 801: ... accommodate the striking of a chalk line 2 Ascertain that the nose gear is properly adjusted as given in Nose Gear Assembly Adjustment above 3 With the landing gear in the down locked position weight proportionally on the nose gear and the nose wheel facing forward adjust the steering arm roller clearance as described in 27 20 00 Rudder Controls Rigging and Adjustment 4 Place the airplane on jack...

Page 802: ...r lay a straightedge along the side of the tire and parallel the straightedge with the chalk line 12 Adjust the steering bungee length and install with nose wheel straight forward Check that the rod ends have sufficient thread engagement by ascertaining that a wire will not go through the check hole in the rod Tighten the jam nuts 13 To check the nose gear steering for its 30 right and left maximu...

Page 803: ...PAGE 11 Feb 28 07 4D21 32 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Nose Gear Tolerances Figure 6 Sheet 1 of 2 ...

Page 804: ...ly removed bolt nut and washers Nose Gear Tolerances Figure 6 Sheet 2 of 2 Item Manufacturers Service Service No Part No Nomenclature Dimension 1 Dimension 1 Tolerance Remarks 1 452 857 Lower Strut 312 NOTES 2 4 FF411 2 Bearing 313 2 452 450 Link Assembly 2495 NOTES 2 FF310 5 Bearing 2505 3 4 3 452 857 Upper Strut 314 NOTES 2 5 FF411 2 Bearing 313 4 82695 18 R H Roller 660 O D Bushing 5 86700 47 L...

Page 805: ... tension Reject the spring if the tension does not maintain the doors in the full open position 5 Repairs to the door are limited to replacement of hinges and painting 6 Repairs to the retraction mechanism are limited to replacement of parts removal of light corrosion and painting 6 Nose Gear Door Adjustments A Place the airplane on jacks refer to 7 10 00 B Disconnect both gear door actuating rods...

Page 806: ...PAGE 14 Feb 28 07 4D24 32 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 807: ...draulic fluid in reservoir Fill reservoir with hydraulic below operating level fluid to full level and investigate cause Battery low or dead Check condition of battery Recharge or replace Hydraulic fluid leak in system Isolate leak and repair Hydraulic pump electric motor Repair replace motor top inoperative plate assembly Hydraulic lines obstructed or Check lines leaking Landing gear retraction H...

Page 808: ...re of adjustment relief valve Mechanical restriction or Place airplane on jacks and obstruction in hydraulic run extension check system to allow pressure Isolate and determine to build up and shut off cause pump before gear has extended retracted Pump fails to shut off Pressure switch inoperative Repair replace switch though gear has fully retracted extended Pressure switch out of Check bypass cir...

Page 809: ...uating cylinders for external leakage Check for broken or damaged hydraulic lines Pump running intermittently Hydraulic fluid low in Fill reservoir and check after gear has retracted reservoir for leaks Gear stops part way up but Hydraulic fluid in reservoir Fill reservoir with hydraulic pump continues to run below operating level fluid Internal leakage of system Check gear actuating cylinders for...

Page 810: ... actuators hoses etc NOTE Never operate the emergency gear release piston with the hydraulic pump circuit breaker IN 4 During all tests add clean filtered MIL H 5606 Revision F or higher hydraulic fluid to the reservoir as necessary to keep fluid level at the F full mark on the sight gauge with the gear down 5 Bleed the hydraulic system per 29 10 00 Bleeding Hydraulic System 6 Set the sequence val...

Page 811: ...nute period check for leaks or malfunctioning components in the system NOTE One momentary pump operation is allowable during this five 5 minute period provided that the gear warning light is out and no repeated pump operations for a subsequent fifteen 15 minute period occur 4 Place the gear selector switch in the UP position 5 Verify that a Three green safe lights are out b Red gear warning light ...

Page 812: ...ntinuing approximately two 2 minutes NOTE The main gear may not fall completely into the locked position during ground free fall tests Extend the main gear using a side force at the center line of axle that does not exceed nine 9 pounds The gear should move easily and then lock in place 12 Place the gear selector switch in the DOWN position 13 Push in the emergency gear release i e free fall knob ...

Page 813: ...uipped with Frisby hydraulic pumps only 1 Disconnect the gear down pressure switch circuit see Wire A Figure 1 and conduct the following sequence a Place the gear selector switch in the UP position The gear should function normally b Place the gear selector switch in the DOWN position The pump will shut OFF before the gears reach the full down position CAUTION DO NOT PULL THE EMERGENCY GEAR RELEAS...

Page 814: ...PAGE 8 Feb 28 07 4E8 32 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Down Pressure Switch Bypass Relay Figure 1 ...

Page 815: ...ped with Frisby hydraulic pumps only c Hydraulic pump motor stops operating after the gear is in down and locked position CAUTION ANY MOMENTARY BLINKING OF THE RED OR GREEN GEAR LIGHTS AFTER THE ACTUATOR IS DOWN AND LOCKED MAY INDICATE AN IMPROPERLY ADJUSTED SWITCH IN A LOCKING CYLINDER d Red gear warning light is illuminated while gear is in transit e Three green safe lights are illuminated as th...

Page 816: ...PAGE 10 Feb 28 07 4E10 32 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Nose Gear Actuator Installation Figure 2 ...

Page 817: ...THE DOWNSPRING ASSEMBLY 3 Position the special remove install tool P N 762 157 see Figure 3 so that the nose gear downspring is within the two end plates Secure the special tool to the downspring assembly with hose clamps Remove bolt holding actuator rod end bearing and downspring assembly to trunnion Remove washers spacers and bushing CAUTION IF COMPLETE DISASSEMBLY OF THE DOWNSPRING MECHANISM IS...

Page 818: ... to the nose gear actuator engine mount connecting hardware to ensure the correct locknut is used i e P N 404 891 MS 20365 720C Additionally check for proper thread engagement between the bolt and nut by ensuring at least one thread of the bolt protrudes through the nut per AC 43 13 1 latest revision If there are not sufficient threads exposed after the lock nut replace the bolt with a longer bolt...

Page 819: ... washer bushing and bolt 5 Disconnect upper end of actuator from its mounting bracket by removing bolt and washer 6 Remove actuator from airplane 7 Remove rod end bearing from actuator rod Check that rod end bearing lock nut is free of scoring and nicks Smooth out if necessary 8 Move landing gear selector to the DOWN position 9 Manually extend rod so that actuator assembly locks in down or fully e...

Page 820: ...PER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL WIDTH OF CHAMFER THE CHAMFER WIDTH IS TYPICALLY 25 INCHES EXCEPT FOR THE 12 INCH CHAMFER WIDTH SHOWN IN THE PHOTO 45 Chamfer Details Figure 4 Effectivity 4636001 thru 4636195 ...

Page 821: ...on of this modification 5 Nose Gear Door Actuator Assembly See Figure 5 NOTE No field repair of nose gear door actuators installed in PA 46 350P airplanes is authorized Actuator overhaul service is available through Piper distributors A Removal 1 Place airplane on jacks refer to 7 10 00 2 Reduce hydraulic pressure as follows a Place gear control in the UP position b Allow gear to retract approxima...

Page 822: ...PAGE 16 Feb 28 07 4E16 32 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Sequence Valve Parker Hannifin Figure 6 ...

Page 823: ...ove spring spring retainer and ball from plunger port H Remove and discard O ring from plunger port I Remove bolt and locknut to remove plunger seat and spring Use a No 1 Phillips screwdriver to aid in removal of plunger J Remove and discard O ring from seat K Remove and discard O ring from plunger port WARNING USE SOLVENT IN WELL VENTILATED AREA AVOID CONTACT WITH SKIN KEEP AWAY FROM HEAT OR FLAM...

Page 824: ...oor boards under copilot s seat A Removal 1 Remove copilot s seat carpet access panel and center floorboard 2 Remove and quickly cap hydraulic lines 3 Loosen nuts at bulkhead fittings 4 Disconnect cable 5 Remove valve from aircraft B Installation 1 Position valve in airplane Secure bulkhead fittings with nuts and tighten 2 Connect cable 3 Uncap and connect hydraulic lines 4 Install access panel an...

Page 825: ...valve body with hydraulic fluid c Install new O rings onto bulkhead fittings d Install bulkhead fittings into UP and DN ports Torque to 60 65 in lbs CAUTION CHECK VALVES ARE NOT INTERCHANGEABLE BEFORE INSERTING VALVES INTO UP AND DN PORTS CORRECTLY IDENTIFY VALVE BY PRINTED VENDOR NUMBER e Insert check valve with rubber seal 2203C 20 into DN port Arrow on check valve must point toward end gland Pu...

Page 826: ...PAGE 20 Feb 28 07 4E20 32 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL GRIDS 4E20 THRU 4E24 INTENTIONALLY BLANK ...

Page 827: ... then removing the other half 4 The wheel bearing assemblies may be removed from each wheel half by first removing the snap rings that secure the grease seal retainers and then the retainers grease seals and bearing cones The bearing cups should be removed by tapping out evenly from the inside B Assembly and Installation 1 Ascertain that the bearing cup for each wheel is properly installed Install...

Page 828: ...y be removed from each wheel half by first removing the retainer snap rings that secure the grease seal retainers and then the retainers grease seals and bearing cone The bearing cups should not be removed except for replacement Refer to Nose and Main Wheel Assembly Repairs below for bearing cup replacement instructions B Assembly and Installation 1 Ascertain that the bearing cup for each wheel is...

Page 829: ...nicks using fine 400 grit sandpaper 9 Replace disc if cracked or when disc is worn below 405 in Wheel Brake Assembly Cleaning Inspection and Repair below 3 Nose and Main Wheel Assembly Repairs Repairs are limited to blending out small nicks scratches gouges and areas of slight corrosion plus the replacement of parts which are cracked or badly corroded NOTE Remove corrosion and blend out small nick...

Page 830: ...ng cup from dry ice Install the chilled bearing cup into the bearing bore of the heated wheel half Tap gently to seat evenly in place using a fiber drift pin or suitable arbor press 5 Brake Adjustment and Lining Tolerance No adjustment of the brake lining clearance is necessary as they are self adjusting Inspection of the lining is necessary and it may be inspected visually while installed on the ...

Page 831: ...re refer to Figure 3 Step B 2 Align cylinder body over anchor bolt refer to Figure 3 Step C 3 Use a suitable arbor press and apply pressure on the spot face directly over the anchor bolt hole refer to Figure 3 Step D B Assembly and Installation 1 Lubricate the piston O ring s with fluid MIL H 5606 and install on piston s Slide the piston s in cylinder housing until flush with surface of housing 2 ...

Page 832: ...d use NOTE To inspect the linings check the expansion groove If the groove is not showing replace the lining NOTE Replacement brake linings metallic used on the brake assembly should be conditioned by performing three hard braking applications at 45 to 50 mph Do not allow the brake discs to cool substantially between stops This will wear off any high spots and at the same time generate sufficient ...

Page 833: ...out of cylinder housing NOTE Repairs to the rod and ring assembly and piston are limited to polishing small scratches and burrs and replacement of parts 3 Clean cylinder bore rod and ring assembly and piston with dry type solvent 4 To replace any of the component parts shown in the parts catalog remove retaining ring All parts will slide off rod and ring assembly 5 Soak end fitting O rings one int...

Page 834: ...URFACE OTHERWISE THE INNER SURFACE MAY BECOME SCRATCHED 9 Carefully insert piston and rod and ring assembly into cylinder housing 10 Tighten end fitting to a torque of 13 17 inch lbs 11 Connect cylinder assembly to rudder bar with two nuts bolts and washers 12 Inboard toe brake assemblies only Connect pedal to nose wheel steering rod assembly 13 Connect clevis to rudder pedal by inserting pin wash...

Page 835: ...ing one or two turns 2 On the other main gear slide the hose of the pressure unit over the bleeder fitting then open the fitting one or two turns and pressure fill the brake system with MIL H 5606 fluid 3 With fluid continually flowing through the brake system SLOWLY and together actuate the pedals several times NOTE By watching the fluid pass through the plastic hose at the fluid reservoir and th...

Page 836: ...inal set C If the toe brakes can be pushed forward and feel spongy a leak is present at some point in the system D This leak may appear at any one of the connections throughout the system or internally in the toe brake master cylinder or wheel brake assemblies 10 Parking Brake Valve A Removal 1 Disconnect the parking brake cable from the valve actuating arm 2 Disconnect the fluid lines from the va...

Page 837: ... Clean the valve parts with a suitable solvent and dry thoroughly 2 Inspect valve and seat surfaces of valve body for excessive wear and corrosion 3 Inspect the cam assembly for burrs scratches excess wear loose operating lever etc 4 Check general condition of valves and springs 5 Repair to the valve is largely limited to smoothing burred or scratched surfaces and replacing O rings ...

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Page 841: ...eeve in the forward end of the bellows 3 Reinstall the rod end on the end of the pushrod Then tighten the rod end 1 2 turn 4 Attach the forward end of the steering rod to the steering bellcrank 5 Attach the aft end of the steering rod to the arm on the rudder bar 6 Locate the forward end of the bellows immediately aft of the jam nut on the forward rod end and tighten the hose clamp on the forward ...

Page 842: ...sure bulkhead 3 Slide plate packing ring housing spacer assembly and fire shield forward on steering rod tube 4 Line up holes in pressure bulkhead plate and fire shield install screws washers and nuts NOTE Install all screws except the uppermost one with their shanks pointing aft The uppermost screw s shank should point forward 5 Install steering pushrod per instructions in this chapter 6 Reconnec...

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Page 845: ... Isolate and replace though gear has retracted switches failed switch Nose gear up limit Check gear up adjustment switch out of adjustment and readjust up limit switch Main gear not retracting Check gear up adjustment far enough to actuate switch Red gear unsafe light on One or more down limit Isolate and replace switch though gear is down switches failed and locked Nose gear down limit Readjust d...

Page 846: ...t breaker open and determine cause when power is decreased for open circuit breaker to approximately 15 IN HG MAP and landing gear is retracted Micro switch at throttle Adjust micro switch out of adjustment Micro switch at throttle Replace switch failed Warning horn and light Check wiring circuit wire broken Red gear unsafe light and horn Gear selector handle in up Place handle in down fail to sto...

Page 847: ... and gear is down and through dimming locked resistor instead of instrument panel light control Green gear down light Gear down limit switch Replace switch fails to go out with failed gear in transit or retracted Green gear down lights Green light ground Replace resistor will go out and not dimming resistor dim when position light open switch is turned on though gear is down and locked Green gear ...

Page 848: ...ment See Figure 1 The nose gear up limit switch is located on the right hand side of the wheel well opening The right hand nose wheel door actuates this switch This switch is adjusted by backing off the two nuts on the switch plunger bushing B Down Limit Switch Adjustment The nose gear down limit switch is mounted on the nose gear locking actuator The switch is activated when the cylinder is exten...

Page 849: ...t See Figure 2 A gear up limit switch is located in the wing wheel well beneath the locking actuator There is no adjustment of the switch other than that shown in Figure 2 i e 0 0 to 0 03 inch above the flush line of the lower wing skin B Down Limit Switch Adjustment The main gear down limit switches are mounted in each main gear locking actuator The switch is activated when the cylinder is extend...

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Page 851: ... selector UP control circuit at a strut extension of 8 00 inches maximum and an open gear UP control circuit at a strut extension of 7 70 inches minimum A Jack the airplane refer to 7 10 00 B Compress the strut until 7 875 inches is obtained between the top of the gear fork and the bottom of the gear housing Hold the gear at this measurement C Adjust the switch so that it actuates at this point Se...

Page 852: ...ashers that attach the switch to its mounting bracket 2 Installation a Attach the switch to its mounting bracket with screws nuts and washers b Reconnect the electrical leads at the plug c Slide control quadrant cover down the engine control levers and secure it to the top of the console d Adjust the switch per the following instructions 3 Adjustment PIR FTP2001 8 Rev E This switch is adjusted by ...

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Page 855: ...4G5 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 33 LIGHTS ...

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Page 857: ...es 2 Feb 28 07 33 Table of Contents 1 Feb 28 07 2 Feb 28 07 33 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 33 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 33 30 00 1 Feb 28 07 2 Feb 28 07 33 40 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 CHAPTER SECTION...

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Page 859: ...ing Rheostat 2 4G12 Removal 2 4G12 Installation 2 4G12 Switch Lamps Removal and Installation 7 4G17 Illuminated Switch Assembly Removal and Installation 7 4G17 Environmental De ice Switch Panel 7 4G17 Circuit Breaker Panels Electroluminescent Lighting 7 4G17 Post Installation Setup 8 4G18 PASSENGER COMPARTMENT 33 20 00 1 4G21 Courtesy Rear Baggage Area Lighting 1 4G21 Description 1 4G21 Lamp Repla...

Page 860: ...ON PAGE GRID NO EXTERIOR 33 40 00 1 4H3 Strobe Lights 1 4H3 Description 1 4H3 General Service Information 1 4H3 Position Strobe Lamps Replacement 2 4H4 Strobe Power Supplies Replacement 3 4H5 Taxi Light Replacement 4 4H6 Landing Light Replacement 5 4H7 Wing Inspection Light 5 4H7 Removal 5 4H7 Installation 5 4H7 Changing Light Bulb 5 4H7 Pulse Lights 5 4H7 ...

Page 861: ...ll panel lights except for integral radio equipment lighting are controlled from the dimmer control unit and dimming rheostat Employ conventional troubleshooting methods panel lights full bright first replacing offending individual lamps If not successful measure socket voltage and repair as required If all lamps are OUT check power from bus through circuit breaker harness dimmer control and dimme...

Page 862: ...e to expose the lamp bulb Replace defective bulb and reverse removal procedure Depress Test function to verify lamp function B In S N s 4636132 thru 4636374 pull evenly on the annunciator panel bezel to access the lamp bulbs An extraction tool and four spare bulbs are located behind the bezel Use the extraction tool to replace defective bulb and reverse removal procedure Depress Test function to v...

Page 863: ... S FLAPS RED L T STARTER RED ENGAGE M U WINDSHIELD RED HEAT FAIL N V OXYGEN AMBER Station Station Fig 2 Fig 3 Annunciator Color P GREEN R X OIL AMBER PRESS S Y HYDRAULIC AMBER PUMP T Z SURFACE GREEN DE ICE U AA ANNUNCIATOR AMBER INOP W PITOT HEAT AMBER OFF INOP A VACUUM AMBER NO 1 INOP B VACUUM AMBER NO 2 INOP C GREEN D GREEN E GREEN F FUEL AMBER IMBALANCE SELECT AMBER DE ICE ICE DETECT AMBER FAIL...

Page 864: ... G N B H P C J R D K S E L T F M U J328 2 3 1415 13 1 11 12 10 6 8 9 4 7 17 18 16 5 DIODE IN2071A SOLDER SLEEVE A G N B H P C J R D K S E L T F M U J329 30 31 19 24 10 16 22 11 20 27 21 1 33 34 35 12 DIODE IN2071A SOLDER SLEEVE 36 26 29 17 23 25 18 3 4 22 gauge bus wire Tubing Annunciator Panel Installation Figure 2 Sheet 1 of 3 Effectivity 4636001 thru 4636020 ...

Page 865: ...0 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL A G N B H P C J R D K S E L T F M U BRACKET NUT SELF LOCKING V W X Y Z AA FRONT Annunciator Panel Installation Figure 2 Sheet 2 of 3 Effectivity 4636021 thru 4636131 ...

Page 866: ...PAGE 6 Feb 28 07 4G16 33 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Annunciator Panel Installation Figure 2 Sheet 3 of 3 Effectivity 4636132 thru 4636313 less 4636299 ...

Page 867: ... the panel front and push firmly into the panel cutout until the metal lock tabs snap into position against the rear face of the panel Make sure the electrical connections are completed first 8 Environmental De ice Switch Panel S N s 4636132 and up The Environmental De ice switch panel adjacent to the annunciator in S N s 4636132 and up is a sealed unit lighted with LED s and cannot be repaired in...

Page 868: ...change data on the displayed Main Lighting Page press the small inner right knob CRSR to turn on the cursor Turn the large outside right knob to step through the data fields Turn the small inner right knob to change the data in the field that the cursor is on Press the ENT key to accept the data that is displayed in the selected field Configure a newly installed unit as shown in Chart 2 NOTE Initi...

Page 869: ...t changes Pressing the FUNC key moves on to the next configuration page without saving the changes To exit the configuration pages turn the power off and then on again without holding the FUNC key Configure a newly installed unit as shown in Chart 3 NOTE For the GTX 330 only when the unit is turned on for the first time or an invalid aircraft address is recognized the unit will prompt the user to ...

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Page 871: ...out bayonet base lamp 3 Install replacement check and reinstall lens 2 Courtesy Lights Timer A Removal 1 The courtesy lights timer is located on a frame assembly aft of the lower cabin door 2 Disconnect electrical wires 3 Remove mounting screws and timer assembly B Installation 1 Position timer assembly in place and secure with mounting screws 2 Connect electrical wires 3 Test for proper operation...

Page 872: ...07 4G22 33 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL OFF ON LAMP LAMPHOLDER CUP FLOOD LENS HEX NUT STAR WASHER MAGNIFYING LENS BEZEL SLIDE SWITCH ON OFF Reading and Courtesy Light Figure 1 ...

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Page 875: ...TMENTS All lighting is 24 Vdc Forward Baggage Compartment Lamp Replacement The forward baggage compartment door actuates the door ajar switch controlling the annunciator panel door ajar indicator The baggage light contains its own integral switch A Remove lens B Replace bayonet lamp C Replace lens and check operation ...

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Page 877: ...id state timing circuit After the trigger pulse causes ionization of the Xenon gas in the envelope an intense light is given off for a brief moment as the capacitor discharges Following discharge across the tube the oscillator again chops up the dc aircraft current into alternating current and again develops a higher voltage through transformer action After full voltage is again impressed on the c...

Page 878: ...sing the attached strobe power supply 7 Remove four attachment screws and eight AN960 10 washers separate power supply from access panel Set wing access panel aside to protect paint etc 8 Unplug both power supply connectors and remove power supply from wing 9 Reach into wing and unscrew P109 left wing P209 right wing releasing this connector refer to Figure 1 10 Remove light bracket assembly mount...

Page 879: ...upply attached and wires facing outboard to the wing surface with appropriate mounting screws previously removed 21 Install the light bracket assembly lens lens retainer and plexiglass cover D Strobe Power Supplies Replacement 1 Each wing tip strobe light is powered by its individual power supply which is attached to a wing access panel located on the lower wing surface just inboard of the wing ti...

Page 880: ...obe power supply connectors so access panel with power supply still attached can be set aside This will prevent weight of power supply from pulling on electrical harness refer to Figure 1 D Disconnect taxi light and electrical connectors from rear of light E Remove four bracket retaining screws from the assembly These screw are removed from the external surface of the wing 2 on the bottom and 2 on...

Page 881: ...The longer screw is from the upper aft position 3 Push the light assembly inward 4 Disconnect the wiring harness from the light Refer to item C 2 below 5 Remove the light assembly B Installation 1 Clean any remaining sealant from the light assembly shim and inboard side of doubler 2 Apply GE RTV 1508 sealant to both sides of the shim NOTE The thicker end of the shim should face aft 3 Install the s...

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Page 884: ...PAGE 8 Feb 28 07 4H10 33 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL GRIDS 4H10 THRU 4L24 INTENTIONALLY BLANK ...

Page 885: ...PART NUMBER 761 876 February 28 2007 5A1 AIRPLANE MAINTENANCE MANUAL CARD 5 OF 9 PA 46 350P S N s 4636001 AND UP PIPER AIRCRAFT INC ...

Page 886: ...5A2 Published by Technical Publications Piper Aircraft Inc 2926 Piper Drive Vero Beach Florida 32960 U S A Member General Aviation Manufacturers Association ...

Page 887: ...2 3 4 5 and 6 CR981223 December 23 1998 1 2 3 4 5 and 6 PR000201 February 1 2000 1 2 3 4 5 and 6 PR010515 May 15 2001 1 CR050730 July 30 2005 1 2 3 4 5 6 7 and 8 PR060207 February 7 2006 1 2 3 4 5 6 7 and 8 CR070228 February 28 2007 1 2 3 4 5 6 7 8 and 9 COMPLETE REVISION OF MAINTENANCE MANUAL 761 876 Revisions appear in all Aerofiche Cards Accordingly discard your entire existing Aerofiche Card S...

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Page 889: ...Feb 28 07 Intro Table of Contents 1 Feb 28 07 2 Feb 28 07 Introduction 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 Index 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHA...

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Page 891: ...A9 Effectivity 2 5A10 Serial Number Explanation 2 5A10 Assignment of Subject Material 2 5A10 Pagination 3 5A11 Aerofiche Effectivity 3 5A11 Identifying Revised Material 3 5A11 Indexing 3 5A11 List of Effective Pages 3 5A11 Warnings Cautions and Notes 3 5A11 Accident Incident Reporting 4 5A12 Supplementary Publications 4 5A12 Piper Publications 4 5A12 Vendor Publications 4 5A12 Chapter Section Inde...

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Page 893: ...GENUINE PIPER AIRCRAFT PARTS OR PIPER AIRCRAFT APPROVED PARTS OBTAINED FROM PIPER APPROVED SOURCES IN CONNECTION WITH THE MAINTENANCE AND REPAIR OF PIPER AIRPLANES Genuine PIPER parts are produced and inspected under rigorous procedures to ensure airworthiness and suitability for use in PIPER airplane applications Parts purchased from sources other than PIPER even though identical in appearance ma...

Page 894: ...ane are broken down into subsystems These sub systems are identified by the second element of the standard numbering system The element 40 of the number 28 40 01 concerns itself with the indicating section of the fuel system C Unit Subject The individual units within a sub system section may be identified by the third element of the standard numbering system The element 01 of the number 28 40 01 i...

Page 895: ...his set 8 Identifying Revised Material A revision to a page is defined as any change to the printed matter that existed previously Revisions additions and deletions are identified by a vertical line i e change bar along the left hand margin of the page opposite only that portion of the printed matter that was changed A change bar in the left hand margin opposite the footer i e chapter section subj...

Page 896: ...s Catalog P N 761 878 2 Periodic Inspection Report Form P N 767 011 3 Progressive Inspection Manual 50 hour P N 767 013 B Vendor Publications WARNING FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION S WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT MAY RENDER THE AIRCRAFT UNAIRWORTHY 1 AIR CONDITIONING COMPRESSOR Vendor Address Sanden International USA Inc PH 972 442 8400...

Page 897: ...cialty Systems PH 330 374 3040 Goodrich Corporation FAX 330 374 2290 1555 Corporate Woods Parkway Uniontown Ohio 44685 8799 Technical Assistance PH 800 334 2377 330 374 3743 FAX 330 374 2290 Email dssd support goodrich com http www deicingsystems goodrich com Black Standard Pneumatic De Icer Installation Maintenance and Repair Manual ATA 30 10 31 SmartBoot System ATA 30 10 65 8 ELECTRONIC FLIGHT I...

Page 898: ...ntext See www avantext com or PH 800 998 8857 11 FIRE EXTINGUISHER PORTABLE Vendor Address H3R Inc PH 800 249 4289 43 Magnolia Ave 4 San Francisco California 94123 2911 http www h3r com index htm 12 FORCE APPLICATOR KIT Vendor Address Safe Flight Instrument Corp PH 914 946 9500 20 New King Street White Plains New York 10602 13 FUEL BOOST PUMP Vendor Address Parker Hannifin Corp PH 800 272 7537 Nic...

Page 899: ...ww unisonindustries com index4 html Installation Operation F1100 MASTER SERVICE MANUAL and Maintenance 4300 6300 SERIES MAGNETO MAINTENANCE AND Instructions OVERHAUL MANUAL L 1363 19 NAVIGATION COMMUNICATIONS AND GPS NAV COM GPS Vendor Address Garmin International PH 913 397 8200 1200 East 151ST Street Olathe KS 66062 http www garmin com 20 OXYGEN SYSTEM Vendor Address Scott Aviation PH 716 683 51...

Page 900: ...DAR WEATHER RDR 2000 Vendor Address Honeywell Bendix King See Autoflight above Maintenance Manual Bendix King ART 2000 P N 006 05332 0001 25 RADIO COOLING BLOWER Vendor Address Globe Motors PH 937 228 3171 2275 Stanley Ave FAX 937 229 8531 Dayton Ohio 45404 http www globe motors com home html 26 STARTER Vendor Address Kelly Aerospace See Alternator above or Sky Tec Partners Ltd PH 800 476 7896 350...

Page 901: ...MALIBU MIRAGE MAINTENANCE MANUAL 28 VACUUM PUMP Vendor Address Aero Accessories Inc PH 800 822 3200 1240 Springwood Avenue Gibsonville NC 27249 http www aeroaccessories com index html 29 VACUUM REGULATORS Vendor Address Parker Hannifin Corp see Fuel Boost Pump above ...

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Page 903: ...chapter CHAPTER SECTION TITLE GRID NO 4 AIRWORTHINESS LIMITATIONS 1C1 00 Airworthiness Limitations 5 TIME LIMITS MAINTENANCE CHECKS 1C9 00 General 10 Time Limits 20 Scheduled Maintenance Checks 30 Special Inspections 50 Unscheduled Maintenance Checks 6 DIMENSIONS AND AREAS 1E13 00 General 7 LIFTING AND SHORING 1F1 10 Jacking 8 LEVELING AND WEIGHING 1F9 10 Weighing and Balancing 20 Leveling 9 TOWIN...

Page 904: ...emperature Control 22 AUTOFLIGHT 2F11 10 Autopilot 23 COMMUNICATIONS 2G19 00 General 50 Audio Integrating 60 Static Discharging 24 ELECTRICAL POWER 2H11 00 General 30 DC Generation 40 External Power 60 Electrical Load Distribution 25 EQUIPMENT FURNISHINGS 2J11 10 Flight Compartment 20 Passenger Compartment 50 Cargo Compartments 60 Emergency 26 FIRE PROTECTION 2K15 20 Extinguishing 27 FLIGHT CONTRO...

Page 905: ...rs 60 Propellers Rotors 31 INDICATING RECORDING SYSTEMS 4C1 50 Central Warning Systems 32 LANDING GEAR 4C13 00 General 10 Main Gear and Doors 20 Nose Gear and Doors 30 Extension and Retraction 40 Wheels and Brakes 50 Steering 60 Position and Warning 33 LIGHTS 4G5 10 Flight Compartment 20 Passenger Compartment 30 Cargo and Service Compartments 40 Exterior 34 NAVIGATION 5C1 00 General 10 Flight Envi...

Page 906: ...00 General 10 Investigation Cleanup and Aerodynamic Smoothness 70 Repairs 80 Electrical Bonding 52 DOORS 6G13 10 Passenger Crew 20 Emergency Exit 30 Cargo 70 Monitoring and Operation 55 STABILIZERS 6H13 00 General 10 Horizontal Stabilizers 20 Elevator 30 Vertical Stabilizer 40 Rudder 56 WINDOWS 6I19 00 General 10 Flight Compartment 20 Cabin 30 Door 57 WINGS 6K5 40 Attach Fittings 50 Flight Surface...

Page 907: ... Power Supply 20 Distribution 76 ENGINE CONTROLS 7G17 10 Power Control 77 ENGINE INDICATING 7H3 10 Power 20 Temperature 40 Integrated Engine Instrument Systems 79 OIL 7J3 20 Distribution 30 Indicating 80 STARTING 7J15 10 Cranking 81 TURBINES 7K9 20 Turbo Supercharger 91 CHARTS WIRING DIAGRAMS 8C1 10 Charts 21 and up Electrical Schematics 91 CONT CHARTS WIRING DIAGRAMS CONT 9C1 Electrical Schematic...

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Page 909: ...sion Control Wing 6L3 Attitude Indicator 5D5 Autopilot 2F17 Component Locator 2G2 Installation 2F18 2F20 Maintenance 2F23 Operational Checkout 2F24 Pitch Servo 2G12 Pressure Transducer 2G6 Roll Servo 2G4 Servo Clutch Torque Adjustment 2G15 Trim Monitor 2G3 Trim Servo 2G6 Yaw Amplifier 2G14 Yaw Servo 2G10 Avionics Cooling 2C14 Avionics Master Switch 2H1 B Ball Diameters for Testing Hose Restriction...

Page 910: ...rrection 2I10 Troubleshooting 2I7 2I13 Valve Regulated Lead Acid 2I13 Bonding 6G9 Resistance Index 6G10 Buses Avionics 2H19 Main 2H19 Circuit Breaker Panel 6D22 Electrical Shelf 6E7 External Power 2I19 Load Distribution 2J1 Relay Installation Co Pilot s Side 6E10 K1 thru K8 6E10 Pilot s Side 6E9 Schematics Air Conditioning 8E7 Airspeed Standby 9E19 Altimeter Radar 9F14 Altimeter Standby 9E19 Annun...

Page 911: ...n Light 9E5 WX 500 9F11 XM Receiver 8E23 Switch Panels 6E1 Symbols 8D14 System 2H17 Troubleshooting 2H20 Tie Bus Panel Connections 6E3 Volt Ammeter 2J4 Voltage Regulation and Control 2H19 Wire Coding 8D13 Elevator Balancing 6I3 Control System Installation 3D23 Rigging and Adjustment 3D24 Troubleshooting 3D19 Torque Tube Bearing Changes 3D20 Trim Controls Actuator Assembly 3E3 Corrosion Control 3E4...

Page 912: ...Drain Valve 3G8 Draining 1I19 Draining Moisture 1I18 Fuel Filter 3G7 Fuel Pumps Specifications 3G5 Fuel Quantity Gauge Accuracy Test 3G14 Full Range Check 3G20 Senders 3G13 Leak Test Setup 3G1 Selector Switch and Valve 3G6 Cable Adjustment 3G7 Troubleshooting 3F16 Leak Evaluation 3F22 G GMA 340 Audio Panel Adjustments 2H6 Installation 2H3 System Functional Test 2H4 GNS 430 5F5 GNS 530 5F5 Ground C...

Page 913: ... 4D11 Position and Warning 4F19 Landing Gear Up Power Reduced Warning Switch Adjustment 4G2 Troubleshooting 4F20 Leading Particulars and Principal Dimensions 1E20 Leveling 1F17 Life Limited Parts 1C7 Lifting 1F7 See also 57 40 00 Lights Exterior 4H3 Landing 4H7 Position 4H4 Pulse 4H7 Strobe 4H3 Taxi 4H6 Wing Inspection Light 4H7 Interior 4G11 Annunciator Panel 4G12 Baggage Area 4G21 Forward 4H1 Re...

Page 914: ...g 3K6 Troubleshooting 3J20 Propeller Assembly 7C9 Publications Piper A12 Vendor A12 Q Quad Digital Indicator QDI See Engine Instruments Transicoil EMIS R Radar 5F1 Repairs Fiberglass 6F19 Metal Wire Stitching 6G5 Thermoplastic 6F21 List of Materials 6F24 Window Windshield Acrylic 6J10 Restraint System 2J23 Inertial Reel Adjustment 2J23 Inspection 2J23 Revised Material A11 Robinair 34700 Charging S...

Page 915: ... Bellcrank Centering 4C22 Horn Arm Gap 4C22 Nose Wheel Centering 3C15 4C22 Rudder Pedal Neutral Alignment 3C15 4C22 Rudder Travel Tool 3C15 Torque Conversion 8C20 Torque Wrench Formula 1K2 Towing 1G5 Transponder 5F9 GTX 327 5F9 GTX 330 5F9 Post Installation Setup Procedure 5F10 ARINC 429 Configuration Page 5F11 Display Mode and Key Lighting 5F11 Hexadecimal Conversion 5F13 Operation Configuration ...

Page 916: ...in 6I11 Vertical Speed Indicator 5C18 Volt Ammeter See Electrical W Warnings Cautions and Notes A11 Weather Radar 5F1 Weighing 1F15 Wheel Brake Assembly 4F4 Wheels Bearing Cup 4F4 Main Wheel Assembly 4F2 Nose Wheel Assembly 4F1 Repairs 4F3 Windows and Windshields Door Window 6K3 Heated Windshield Testing 3J15 Troubleshooting 3J15 Inspection and Repair Definitions 6J1 Limitations 6J1 Crack Limitati...

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Page 919: ...5C1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 34 NAVIGATION ...

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Page 921: ...07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 CHAPTER SECTION PAGE DATE 34 20 00 cont 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 19 Feb 28 07 20 Feb 28 07 21 Feb 28 07 22 Feb 28 07 23 Feb 28 07 24 Feb 28 07 25 Feb 28 07 26 Feb 28 07 27 Feb 28 07 28 Feb 28 07 29 Feb 28 07 30 Feb 28 07 31 Feb 28 07 32 Feb 28 0...

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Page 923: ...Altimeter 9 5C20 Troubleshooting 9 5C20 Removal and Installation 9 5C20 Airspeed Indicator 12 5C22 Troubleshooting 12 5C22 Removal and Installation 12 5C22 Outside Air Temperature OAT 13 5C23 S N s 4636021 thru 4636020 13 5C23 Removal 13 5C23 Installation 14 5C24 S N s 4636021 thru 4636374 14 5C24 S N s 4636375 and up 14 5C24 ATTITUDE DIRECTION 34 20 00 1 5D5 Attitude Indicator 1 5D5 Troubleshooti...

Page 924: ...ding Reference System ADAHRS 17 5D21 Magnetic Heading Compensation Calibration 17 5D21 Ground Test Procedure 17 5D21 Avidyne Entegra EFIS 18 5D22 Description 18 5D22 Maintenance 18 5D22 Component Locator 23 5E3 Magnetic Heading Systems S N s 4636160 and 4636248 thru 4636374 26 5E6 Flux Detector 26 5E6 Removal 26 5E6 Installation 26 5E6 Magnetic Heading Compensation Calibration 26 5E6 Standard Inst...

Page 925: ...f Test 2 5F2 DEPENDENT POSITION DETERMINING 34 50 00 COM NAV GPS GNS 430 530 1 5F5 Maintenance 1 5F5 Removal and Installation 1 5F5 Post Installation Lighting Setup 1 5F5 Post Installation Setup Procedure 1 5F5 Transponder 5 5F9 S N s 4636299 and 4636314 thru 4636348 5 5F9 Removal and Installation 5 5F9 Post Installation Lighting Setup 5 5F9 S N s 4636349 and up 5 5F9 Removal and Installation 5 5F...

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Page 927: ...of this system is limited to basic troubleshooting and that is addressed in 34 20 00 2 2006 and up S N s 4636375 and up The Avidyne FlightMax Entegra Electronic Flight Instrument System EFIS is installed as standard equipment This system uses three large 10 4 inch diagonal high resolution sunlight readable full color displays PFD and MFD to provide standard flight instrumentation including attitud...

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Page 929: ...t or in each PFD Avidyne by means of hose and tubing routed through the fuselage In the event the primary static source becomes blocked the system incorporates an external alternate static port located on the bottom of the fuselage aft of F S 241 50 A shutoff valve located below the instrument panel to the left of the pilot opens or closes the alternate static port as required A placard giving ins...

Page 930: ...PAGE 2 Feb 28 07 5C12 34 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Pitot Static System Installation Figure 1 Sheet 1 of 3 Effectivity 4636001 thru 4636374 ...

Page 931: ...PAGE 3 Feb 28 07 5C13 34 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Pitot Static System Installation Figure 1 Sheet 2 of 3 Effectivity with Meggitt EFIS Option ...

Page 932: ...H PITOT ALT STATIC PFD 1 PRI STATIC PFD 1 STANDBY AIRSPEED INDICATOR REF STANDBY ALTIMETER REF CABIN PRESSURIZATION TRIPLE INDICATOR REF PITOT LINE PFD 1 PFD 2 PITOT LINE STATIC LINE STATIC LINE AIRSPEED ALTIMETER CPI TRI PRI STATIC PFD 1 STATIC PFD 2 STATIC PFD 2 105135 G AUTOPILOT TRANSDUCER Effectivity 4636375 and up Pitot Static System Installation Figure 1 Sheet 3 of 3 ...

Page 933: ... the PFD i e EADI 4 When equipped with the Avidyne Entegra turn ON both PFD s 5 Operate the simulator to obtain a reading of 75 knots on the airplane airspeed indicator s 6 Check that the airspeed indicator needles follow in the same direction as the simulator airspeed indicator needle 7 Raise airspeed to 198 knots and wait 15 seconds to allow the airplane airspeed indicators to stabilize 8 Observ...

Page 934: ...5C16 34 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL A A VIEW A A MARKED TOP PART NUMBER DRAIN HOLE ELECTRICAL CONNECTOR PINS B B VIEW B B MAST ASSEMBLY L Shaped Pitot Tube Installation Figure 2 ...

Page 935: ... head 14 Attach static test fixture to the static port and pitot test port of the aircraft Tape over the other static button 15 When equipped with the optional Meggitt EFIS turn ON the PFD i e EADI 16 When equipped with the Avidyne Entegra turn ON the Pilot s PFD 17 Set the aircraft altimeter needles to read zero altitude Operate the static simulator to cause the aircraft altimeter needles to read...

Page 936: ...ead ground the other lead to the metal body of the head assembly There should be no continuity 3 Reinstall the pitot head into the mast assembly and the wing 3 Vertical Speed Indicator NOTE With the Avidyne Entegra EFIS installed this function is performed by the PFD s The Vertical Speed indicator measures the rate of change in static pressure when the airplane is climbing or descending By means o...

Page 937: ...on in pitot head Clean lines and head Pointer oscillates when not Leak in static lines Disconnect all instruments operating in turbulent air connected to the static line Check individual instruments for leaks Reconnect instruments to static line and test installation for leaks Defective mechanism Replace instrument Vertical Speed indicates when Water in static line Disconnect static lines and airc...

Page 938: ... climbs the barber pole design progressively disappears until when at or above 10 000 feet the window is blank The barometric pressure window located on the right side of the indicator dial is set by the knob located on the lower left corner of the instrument The altimeter consists of a sealed aneroid diaphragm that is connected to the pointers through a mechanical linkage The instrument case is v...

Page 939: ...ten instrument screw if missing reset loose Replace instrument if screw is missing Cracked or loose cover glass Case gasket hardened Replace instrument Dull or discolored markings Age Barometric scale and reference Slippage of mating parts Replace instrument markers out of synchronism Barometric scale and reference Drift in mechanism Refer to the latest revision markers out of synchronism of AC 43...

Page 940: ...E If any connections in the static system are opened for maintenance the entire system must be rechecked per FAR 23 1325 With optional Meggitt EFIS installation see Appendix 1 grid 5K19 A Troubleshooting See Chart 4 B Removal and Installation See 39 10 00 Face Mounted Instruments Removal and Installation CHART 4 TROUBLESHOOTING AIRSPEED TUBES AND INDICATOR Trouble Cause Remedy Pointers on instrume...

Page 941: ...into a bracket and protrudes through the airplane s skin 1 Removal a Disconnect the electrical leads from the gauge b Turn the gauge counterclockwise to screw it out of the sunshield It may be necessary to have an assistant hold the sunshield to prevent it from turning with the gauge c Remove the gauge washers and rubber grommet from inside the airplane d Remove the sunshield and lock washer from ...

Page 942: ...emote OAT probe is located on the underside of the right wing mounted to a cover plate at W S 86 50 in S N s 4636021 thru 4636369 and mounted in the wing skin at W S 244 3 in S N s 4636370 thru 4636374 OAT measurement is accomplished by an OAT sensor and the Transicoil Electronic Module Instrument System EMIS See 77 40 00 for more information C S N s 4636375 and up A remote OAT probe is located on...

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Page 947: ...ng See Chart 1 B Removal and Installation See 39 10 00 Face Mounted Instruments Removal and Installation Trouble Cause Remedy Bar fails to respond Insufficient vacuum Check pump and tubing Vacuum System Filter dirty Clean or replace filter Bar does not settle Insufficient vacuum Check line and pump Adjust valve Incorrect instrument Check part number Defective instrument Replace Bar oscillates or s...

Page 948: ...nd level level flight panel instrument Aircraft out of trim Trim aircraft Bar high after 180 Normal if it does not Self correcting turn exceed 1 16th inch CHART 2 TROUBLESHOOTING STANDBY ATTITUDE INDICATOR C Emergency Power Supply A 24Vdc battery operated power supply i e B F Goodrich PS 834A is installed in the aft radar pod compartment to provide emergency power for the standby attitude indicato...

Page 949: ...ired Equipment Power Supply variable 0 32 Vdc 6 0 amps continuous output Voltmeter Fluke 8050A or equivalent Load Resistors 100 0 ohm 2 10 0 W 28 0 V load 13 0 ohm or equivalent 2 5 0 W 5 0 V load b Procedure 1 Disconnect and remove power supply from radar pod 2 Ground J1 pin E or F NOTE Connect directly to the pin s or via a test harness equipped with a MS3106F20 27S or equivalent connector 3 App...

Page 950: ...se or CCW counterclockwise used to electrically drive the remote gyro to correct the heading indication for any precession The system is protected through the 3 amp COMPASS circuit breaker located on the copilot s C B panel A Troubleshooting See Chart 3 B Removal and Installation See 39 10 00 Face Mounted Instruments Removal and Installation Trouble Cause Remedy Heading card frozen 3 amp COMPASS c...

Page 951: ...to errors due to magnetic fields electric instruments etc the directional gyro is only accurate for the heading it has been set for If the gyro is set on 270 for instance and the aircraft is turned to some other heading there can be a large error between the gyro and the magnetic compass due to the error in compass compensation This will appear as gyro precession The gyro should frequently be chec...

Page 952: ...IL THE PROBLEM IS CORRECTED 1 Before applying power verify proper voltage inputs and ground connections as well as all system interfaces 2 Start the PFD in Test Mode by pressing and holding the Baro Pushbutton while applying power until the Initialization page is shown Verify that the Initialization page displays MIRAGE PRIMARY FLIGHT DISPLAY at the top of the screen and is replaced by the Configu...

Page 953: ...m and verify that the PFD Marker Beacon indications are displayed correctly 14 Apply power to the Autopilot system Place the Autopilot Master Switch in the Flight Director position and verify that the flight director bars are displayed correctly 15 Press the Baro pushbutton and verify that the barometric correction displays STD Rotate the Baro Rotary Control clockwise and verify that the barometri...

Page 954: ... Replace PFD Barometric correction does not PFD in test mode Ensure PFD in mission change to standard setting when operational mode Baro pushbutton is pressed Failed PFD Replace PFD Unable to enter test mode when Airspeed equal to or greater Ensure airspeed is less Baro pushbutton is pressed than 40 knots detected than 40 knots Unit not powered off before Ensure unit is powered off Baro Pushbutton...

Page 955: ...izer sensing indications not displayed correctly Failed PFD Replace PFD Marker beacon indications Failed marker beacon system Perform marker beacon not displayed correctly system test Failed PFD Replace PFD Flight director bars not Failed Autopilot system Perform Autopilot system displayed correctly test FD AP switch Check FD AP switch and not functional wired correctly wiring Failed PFD Replace P...

Page 956: ... then use the appropriate test sets to simulate the signals as required CAUTION IF DURING THE FOLLOWING TEST ANY COMPONENT DOES NOT PRODUCE THE EXPECTED RESULTS THAT COMPONENT MUST NOT BE USED IN FLIGHT UNTIL THE PROBLEM IS CORRECTED 1 Before applying power verify proper voltage inputs and ground connections as well as all system interfaces 2 Start the ND in Test Mode by pressing and holding the M...

Page 957: ...ce ND Menu does not appear when Stuck MNU button Check MNU button MNU button is pressed Failed ND Replace ND Menu cursor does not change Stuck and or buttons Check and buttons when and or buttons are pressed Failed ND Replace ND Unable to select menu options Stuck SEL button Check SEL button when SEL button is pressed Failed ND Replace ND Unable to enter Test mode Airspeed equal to or Ensure airsp...

Page 958: ...ng relevant Check status of equipment data to ND failed supplying data to ND Failed ND Check data on relevant ND test page Power on self test status on Failed ND Replace ND Configuration Data page is indicated as FAIL Configuration discrete parity Parity input Configuration Check configuration status on Configuration Data Discrete 7 not wired correctly discrete setting page is indicated as FAIL Ch...

Page 959: ...cross side ND Cross Side Output Interface ARINC Out A and B Bus 2 lines Check wiring Data Page shows valid data is are not connected or are not being Transmitted wired incorrectly Failed ND Replace ND NAV GPS Output Interface ARINC Out A and B Bus 1 lines Check wiring Data Page shows valid data is are not connected or are not being transmitted wired incorrectly Failed ND Replace ND Analog Interfac...

Page 960: ...GATION DISPLAY ND COLOR CODING Display Parameter Color Mission Operational Mode EADI Display Down Mode White A C Symbol Scales Range Rings Digital Readouts Scales Digital Readouts RMI1 Pointer and Annunciation Grey N A Scale Tapes A C Symbol N A Aircraft Symbol Lubber Line Amber Failures and Annunciation s Stall Warning Failures and Annunciation s Red N A Airframe Limits Sky N A Sky Ground N A Gro...

Page 961: ...d frequency annunciations are displayed in the correct colors see Chart 8 Verify that the ND displayed frequencies match the Nav radio frequencies i e RMI1 frequency matches Nav Radio 1 and RMI2 frequency matches Nav Radio 2 The CDI frequency should match the currently selected CDI source frequency Verify that both RMI pointers and the CDI pointer are displayed correctly 14 Select valid ILS freque...

Page 962: ...zel mounted button and verify that the barometric correction continuously decreases in increments of 0 01in Hg 1hPa until the button is released or the minimum barometric correction is reached 26 Press the EADI Display Down switch to shift back to normal mode and verify that the HSI screen format is displayed on the ND Verify that the PFD screen format displays on the PFD 27 Use the bezel mounted ...

Page 963: ...per 8 20 00 and then use NAS1149FN816P washers as required to level the ADAHRS unit a Magnetic Heading Compensation Calibration Perform the Magnetic Heading Compensation Calibration procedure in Magnetic Heading Systems below whenever the ADAHRS unit is installed or replaced b Ground Test Procedure This test procedure included as Appendix 1 grid 5K19 verifies the integrity and accuracy of the air ...

Page 964: ...t as noted below a Primary Flight Display PFD PIR PPS60227 Rev B Use 700 00006 0XX PFD 700 00011 000 Mag OAT ICA Avidyne Document No AVPFD 174 latest revision with the following exceptions 1 In para 6 Troubleshooting Information in the chart where it says OAT Optional cross out optional The OAT is standard in the Piper installation 2 In para 7 2 and Figure 7 where the standard Avidyne installation...

Page 965: ...o select the desired configuration configure the GPS Setup page for the following conditions Receiver 1 GAMA 429 FORMAT Port ARINC 429 RX 1 Speed LOW Receiver 2 GAMA 429 FORMAT Port ARINC 429 RX 2 Speed Low c Press SAVE button 4 Replace 7 3 4 Lightning Sensor Interface and Setup with the following a From the maintenance page depress LSK L3 to access the Lightning Set up page b Using the right oute...

Page 966: ...s the MAP Heading page b Using the right outer concentric knob to select the configuration field and the right inner concentric knob to select the desired configuration configure the Map Heading page for the following conditions Map Heading FMS GPS c Press SAVE button 8 Replace 7 3 11 1 Auxiliary Data 7 3 12 Datalink 7 3 12 1 Narrowcast Datalink Setup and 7 3 12 2 Broadcast Datalink Setup with the...

Page 967: ...nd the right inner concentric knob to select the desired configuration Configure the Radar Setup page for the following conditions Radar Sensor AlliedSignal ART 2000 Park Position Centered Beam Width 7 0 Beam Height 7 0 All boxes CHECKED except Disable Stabilization is NOT CHECKED Press SAVE After pressing save MFD goes to Maintenance Setup Page Calibration The R T Configuration Module must be con...

Page 968: ... To increment the value of the PITCH ANGLE use the left inner knob to change the TILT SETTING to between 5 and UP When the TILT SETTING is set to between 5 and 10 UP the value of the PITCH ANGLE field will slowly increase To decrement the value of the PITCH ANGLE use the left inner knob to change the TILT SETTING to between 5 and 10 DOWN When the TILT SETTING is set to between 5 and 10 DOWN the va...

Page 969: ...he right aft side of the forward pressure bulkhead F S 100 00 see Figure 1 Maintenance is on condition Use 200 00041 000 DAU ICA Avidyne Document No AVSIU 011 with the following exceptions 1 In para 6 in Table 2 DAU Pinout pins J1 2 and J1 21 have No Connection in the Piper installation 2 In para 6 in Table 4 DAU Sensor Compatibility parameter VAC is not used in the Piper installation Configuratio...

Page 970: ... H M P2271 DC MA 37 P3302 P5721 INDUSTRIES POSITRONICS R P43012 P43022 P43062 P3401 P3402 P43011 P43021 P43061 P552 P551 P871 DCM A 37 P3301 P1061 PRIMARY FLIGHT DISPLAY P7332 P730 XMJ1 MULTI FUNCTION DISPLAY P7322 P530 P7331 P7311 P730 P551 P7321 FWD VIEW LOOKING DOWN DC 50 ANTENNA COUPLER DC COUPLER HARNESS P501 TO GNS 430 2 TO MFD TO TOP COMM ANT DC 50 INSTALL MFD WITH 4 CAPTIVE DZUS FASTENERS ...

Page 971: ...C PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL DE ICE TIMER REF F S 100 00 STALL AND GEAR WARN HORN ASSY REF DATA ACQUISITION UNIT DAU INSTRUMENT PANEL REF DEICE LIGHT REF Effectivity 4636375 and up Avidyne EFIS Component Locator Figure 1 Sheet 2 of 2 ...

Page 972: ... SCREWS ARE USED WHEN REINSTALLING a Place the flux detector into position on its mounting bracket and secure with brass screws and washers 3 ea b Connect wiring harness to the connector on top of the flux detector c Seal the connector backshell and base see Figure 2 View A with DOW Corning 4 Electrical Insulating Compound d Reinstall the dorsal fairing NOTE Ensure correct hardware is used when re...

Page 973: ...MIRAGE MAINTENANCE MANUAL FORWARD UP W L 91 446 F S 282 372 FLUX DETECTOR VIEW LOOKING INBOARD LEFT HAND SIDE BRASS SCREW MS 35214 27 BRASS WASHER AN960 B6 3 EACH FAIRING DORSAL SEE VIEW A Flux Detector Installation Figure 2 Effectivity 4636160 and 4636248 thru 4636374 ...

Page 974: ...ading card reading 4 Determine and record on Chart 10 the deviation between the actual magnetic heading and the heading card heading If the heading card reads high the deviation is a plus 5 Repeat steps 3 and 4 for east south and west headings Record actual magnetic headings heading card readings and deviations on Chart 10 6 Plot deviations on the initial deviation graph in Figure 3 7 Realign the ...

Page 975: ...C PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Approx Magnetic Actual Magnetic Heading Card Heading Heading Reading Deviation North East South West CHART 10 DEVIATION CHART ST 180 Deviation Graphs Figure 3 Effectivity 4636160 and 4636248 thru 4636374 ...

Page 976: ... OFF Cabin Blower Fan Low Vent Blower OFF b ADAHRS Unit Alignment Procedure 1 Place the EHSI in the TEST MODE by applying power with the MNU button held in the depressed position until the initialization page is displayed 2 Select ADAHRS test page 2 from the EHSI menu selections 3 Allow the ADAHRS to complete the initialization period and display an attitude sphere on the EADI 4 Verify that the pi...

Page 977: ...UNAUTHORIZED PERSONS SHALL NOT BE CONSTRUED AS THE NEW PIPER AIRCRAFT INC PROGRAM MGR APPD DATE SCALE REV BY APPD DESIGN ENGR BY DATE REV CHECKER REVISION DRAFTSMAN MATERIALS MANUFACTURING OF VERO BEACH FLORIDA SH REF LAYOUT NO S TOL XXX 010 XX 030 X 10 MANUFACTURING PRACTICES SEE PIPER REPORT VB 9 WT DRAWING SIZE LAST SECTION OR VIEW MATERIAL SPECIFICATION ITEM NO ITEM NAME CODE NO SPEC CONTROL D...

Page 978: ...ion is and less than 180 i e 179 then error is For S if indication is and less than 180 i e 179 then error is For W if indication is and less than 90 i e 89 then error is For W if indication is and greater than 90 i e 91 then error is Enter the errors for the four cardinal headings in Chart 11 Add the errors and enter the sum in the TOTAL ERROR block in Chart 11 Divide the Total Error by 4 and ent...

Page 979: ...IBU MIRAGE MAINTENANCE MANUAL Aircraft S N Registration No ND ND Compass Error Heading Rose N E S W Total Error N E S W Index Error Total Error 4 CHART 11 INDEXING DATA ND Compass Heading Rose N 30 60 E 120 150 S 210 240 W 300 330 CHART 12 HEADING SYSTEM CALIBRATION ...

Page 980: ...t 7 Magnetic Heading Systems S N s 4636375 and up Two Magnetometer OAT Sensor Assemblies Mag OAT feed magnetic heading information to the Primary Flight Displays PFD s and the Multifunction Display MFD The Mag OAT s are mounted under the dorsal fairing atop the aft fuselage at F S 282 372 See Figure 6 NOTE The OAT sensors in the Mag OAT assemblies are not used See Outside Air Temperature in 34 10 ...

Page 981: ...PAGE 35 Feb 28 07 5E15 34 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Effectivity 4636375 and up Magnetometer OAT Sensor Assemblies Figure 6 ...

Page 982: ... located away from metal structures and magnetic interference such as that caused by underground power lines etc g Using the bore sight compass align the aircraft to a heading of 360 1 h Enter the System Setup mode on the pilot and copilot PFD s i Press the Perform Mag Cal Line Select Key L2 j Follow the directions on the Magnetometer Calibration Page and press the Calibrate Heading button and wai...

Page 983: ...istant to within 1 h Follow the directions on the Magnetometer Calibration Page and press the Calibrate Heading button and wait until Done is displayed i Align the aircraft to each of the remaining 11 consecutive 30 headings using steps g through h and press the Calibrate Heading LSK R4 at each of these alignment points after satisfactory alignment is achieved j At the final alignment point 330 re...

Page 984: ...d aircraft in level flight attitude Aircraft master switch alternator switch and all radio switches should be in the ON position All other cockpit controlled electrical switches should be in the OFF position 1 Set adjustment screws of compensator on zero Zero position of adjusting screws is when the dot of the screw is lined up with the dot of the frame 2 Head aircraft on a magnetic North heading ...

Page 985: ...lace instrument Excessive pivot friction or Replace instrument broken jewel Liquid leakage Loose bezel screws Replace instrument Broken cover glass Replace instrument Defective sealing gaskets Replace instrument Discolored markings Age Replace instrument Defective light Burned out lamp or broken Check and replace lamp circuit Check continuity of wiring Card sticks Altitude compensating Replace ins...

Page 986: ...filled with damping fluid In the previous example It would indicate the airplane is slipping By utilizing rudder and aileron to establish the airplane in a desired rate of turn will eventually establish the airplane in a coordinated turn at the desired rate A Troubleshooting See Chart 14 B Removal and Installation See 39 10 00 Face Mounted Instruments Removal and Installation CHART 14 TROUBLESHOOT...

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Page 991: ...of the instrument panel and the ART 2000 antenna transceiver AA2010H antenna array and CM 2000 configuration module mounted in a teardrop shaped pod hung from the right wing at the joint between the outboard and center wing sections See Figure 1 NOTE In S N s 4636375 and up the IN 182A display is replaced by the Avidyne Entegra MFD See 34 20 00 Avidyne Entegra EFIS Maintenance Multifunction Displa...

Page 992: ...na transceiver array assembly and secure with screws 4 Torque screws 60 to 70 inch pounds 3 Connect ground wires antenna transceiver connector and configuration module connector 4 Position the radome and secure with screws 13 C Self test S N s 4636001 thru 4636374 only The following displays basic system fault information and tests antenna clearance Use the GAIN TILT and function knobs and the RNG...

Page 993: ...P Wx WxA BRT GAIN NAV TILT PULL STAB OFF UP DN RNG RNG TRK TRK LOG ON TST SBY OFF BENDIX KING RT CALIBRATION DATA PRESS Wx TO RETURN GAIN POT 2 31 0 FAULTS PITCH ANGLE 0 0U 400 REF TILT SETTING 0 0U GYRO ROLL ANGLE 0 0R H V ROLL TRIM 0 0R AFC 400 HZ REF 0 0 AGC AZIMUTH COUNT 45 XMITTER ANTENNA ELEVATION ELV L 0 0U C 0 0U R 0 0U IN 182A Maintenance Menu Figure 2 Effectivity 4636001 thru 4636374 IN ...

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Page 995: ...n this manual is intended solely to aid the removal and installation of the GNS 430 530 transceiver display units their associated wiring and antennas B Removal and Installation See 39 10 00 C Post Installation Lighting Set up See 33 10 00 Post Installation Lighting Set up D Post Installation Setup Procedure PIR PPS 60199 Rev New PIR PPS 60199 2 Rev I 1 Aircraft Preparation and Configuration Setup...

Page 996: ...art 5 c Deselect the cursor and rotate the inner concentric knob on the right side of the unit to display the MAIN LIGHTING page Configure per Chart 6 MAIN ARINC 429 CONFIG Page 1 GNS 530 2 GNS 530 BUS SPEED DATA SPEED DATA GPS ARINC IN 1 HIGH GARMIN GTX 330 HIGH GARMIN GTX 330 HIGH AIRDATA W IHAS HIGH AIRDATA W IHAS GPS ARINC IN 2 HIGH OFF HIGH OFF GPS ARINC OUT HIGH GAMA 429 GRAPHICS W INT HIGH ...

Page 997: ...L 1 OFF AVIATION NO ALT OFF OFF CHNL 2 OFF OFF OFF OFF HW EGPWS W IHAS CHNL 3 CROSSFILL CROSSFILL CROSSFILL CROSSFILL CHNL 4 OFF OFF OFF OFF CHNL 5 OFF OFF OFF OFF CHNL 6 OFF OFF OFF OFF Dual 530 w Meggitt or w Mechanical Indicators Dual 430 w Avidyne Entegra OFF with Avidyne Entegra CHART 5 MAIN RS 232 CONFIG PAGE PIR PPS 60199 2 REV I MAIN LIGHTING PAGE DISPLAY KEY LIGHTING NO SETTING NO SETTING...

Page 998: ...he OBS card e Deselect the cursor and rotate the inner concentric knob on the right side of the unit to display the COM SETUP page Change only the SPACING setting to display Select 25 0 KHz f Deselect the cursor and rotate the inner concentric knob on the right side of the unit to display the VOR LOC GS CDI page Change only the DME CHNL MODE setting to display Parallel 2x5 g VOR LOC GS ARINC 429 C...

Page 999: ...ed in this manual is intended solely to aid the removal and installation of the GTX 327 transceiver display unit its associated wiring and antenna 1 Removal and Installation See 39 10 00 2 Post Installation Lighting Set up See 33 10 00 Post Installation Lighting Set up B GTX 330 S N s 4636349 and up A Garmin GTX 330 Transponder is installed as standard equipment Maintenance of the GTX 330 is on co...

Page 1000: ...select a configuration mode starting page without having to step through all of the pages Press the CRSR key and sequence through to the desired section with the 8 and 9 keys Jump to the selection by pressing the CRSR key again with the desired selection highlighted The FUNC key steps to the next configuration page after which the START STOP key reverses until stopping at the JUMP TO menu page Fol...

Page 1001: ... 4 OFF OFF 429 OUTPUT DATA DATA CHANNEL 1 OFF OFF CHANNEL 2 GARMIN W TIS GARMIN W TIS GARMIN W IHAS GARMIN W IHAS CHART 11 ARINC 429 CONFIGURATION PAGE STANDARD INSTALLATION S N s 4636001 THRU 4636374 DISPLAY MODE AUTO LEVEL 75 BKLT AUTO LVL Not Selectable RSP TIME 4 MIN 8 BKLT SRCE PHOTO SLOPE 50 OFFSET 50 KEY AUTO LVL Not Selectable RSP TIME 4 MIN 5 KEY SRCE 28V SLOPE 20 OFFSET 30 CONTRAST MODE ...

Page 1002: ...ATA CHANNEL 1 OFF OFF CHANNEL 2 GARMIN W TIS GARMIN W TIS GARMIN W IHAS GARMIN W IHAS 1 GTX 330 2 GTX 330 429 INPUT SPEED DATA SPEED DATA CHANNEL 1 LOW GPS FMS LOW GPS FMS CHANNEL 2 HIGH ADC W ALT HIGH ADC W ALT CHANNEL 3 LOW OFF LOW OFF CHANNEL 4 OFF OFF 429 OUTPUT DATA DATA CHANNEL 1 OFF OFF CHANNEL 2 OFF W IHAS OFF W IHAS GARMIN W TIS GARMIN W TIS W O IHAS W O IHAS RS 232 CONFIG GTX 232 INPUT I...

Page 1003: ...xt one repeating the process until the complete number is entered d When finished press the CRSR key to accept the number entry e For entering the Flight ID number press the CRSR key one time f Repeat steps b and c g When finished press the CRSR key to accept the number entry 2 Non US Registered Aircraft a For entering Non U S Aircraft Registration press the CRSR key one time then 8 or 9 to select...

Page 1004: ...elect the numeric entry field Enter the next character as stated in step e then move onto the next one repeating the process until the complete number is entered g For FLIGHT ID select CONFIG ENTRY and enter the Hex code or select POWER UP ENTRY h When finished press the CRSR key to accept the number entry e On the MODE S Aircraft Type Page select 15 5k Lb for AC TYPE and 300 kt for MAX AIRSPEED f...

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Page 1007: ...5K19 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL APPENDIX 1 GROUND TEST PROCEDURE MEGGITT MAGIC AIR DATA HEADING REFERENCE SYSTEM ADAHRS AND PITOT STATIC SYSTEM ...

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Page 1009: ...Effective Pages 2 Feb 28 07 APP1 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 19 Feb 28 07 20 Feb 28 07 21 Feb 28 07 22 Feb 28 07 23 Feb 28 07 24 Feb 28 07 25 Feb 28 07 26 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 1011: ...1 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Ground Test Procedure Meggitt MAGIC ADAHRS and Pitot Static System PIR Meggitt S TEC Doc No 97 9001 001 Rev 3 ...

Page 1012: ... Feb 28 07 5K24 APPENDIX 1 Ground Test Procedure Sheet 2 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1013: ... Feb 28 07 5L1 APPENDIX 1 Ground Test Procedure Sheet 3 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1014: ... Feb 28 07 5L2 APPENDIX 1 Ground Test Procedure Sheet 4 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1015: ... Feb 28 07 5L3 APPENDIX 1 Ground Test Procedure Sheet 5 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1016: ... Feb 28 07 5L4 APPENDIX 1 Ground Test Procedure Sheet 6 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1017: ... Feb 28 07 5L5 APPENDIX 1 Ground Test Procedure Sheet 7 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1018: ... Feb 28 07 5L6 APPENDIX 1 Ground Test Procedure Sheet 8 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1019: ... Feb 28 07 5L7 APPENDIX 1 Ground Test Procedure Sheet 9 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1020: ... Feb 28 07 5L8 APPENDIX 1 Ground Test Procedure Sheet 10 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1021: ... Feb 28 07 5L9 APPENDIX 1 Ground Test Procedure Sheet 11 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1022: ... Feb 28 07 5L10 APPENDIX 1 Ground Test Procedure Sheet 12 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1023: ... Feb 28 07 5L11 APPENDIX 1 Ground Test Procedure Sheet 13 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1024: ... Feb 28 07 5L12 APPENDIX 1 Ground Test Procedure Sheet 14 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1025: ... Feb 28 07 5L13 APPENDIX 1 Ground Test Procedure Sheet 15 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1026: ... Feb 28 07 5L14 APPENDIX 1 Ground Test Procedure Sheet 16 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1027: ... Feb 28 07 5L15 APPENDIX 1 Ground Test Procedure Sheet 17 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1028: ... Feb 28 07 5L16 APPENDIX 1 Ground Test Procedure Sheet 18 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1029: ... Feb 28 07 5L17 APPENDIX 1 Ground Test Procedure Sheet 19 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1030: ... Feb 28 07 5L18 APPENDIX 1 Ground Test Procedure Sheet 20 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1031: ... Feb 28 07 5L19 APPENDIX 1 Ground Test Procedure Sheet 21 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1032: ... Feb 28 07 5L20 APPENDIX 1 Ground Test Procedure Sheet 22 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1033: ... Feb 28 07 5L21 APPENDIX 1 Ground Test Procedure Sheet 23 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

Page 1034: ... Feb 28 07 5L22 APPENDIX 1 Ground Test Procedure Sheet 24 of 24 Meggitt MAGIC Air Data and Heading Reference System ADAHRS and Pitot Static System PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL ...

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Page 1036: ...PAGE 26 Feb 28 07 5L24 APPENDIX 1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1037: ...PART NUMBER 761 876 February 28 2007 6A1 AIRPLANE MAINTENANCE MANUAL CARD 6 OF 9 PA 46 350P S N s 4636001 AND UP PIPER AIRCRAFT INC ...

Page 1038: ...6A2 Published by Technical Publications Piper Aircraft Inc 2926 Piper Drive Vero Beach Florida 32960 U S A Member General Aviation Manufacturers Association ...

Page 1039: ...2 3 4 5 and 6 CR981223 December 23 1998 1 2 3 4 5 and 6 PR000201 February 1 2000 1 2 3 4 5 and 6 PR010515 May 15 2001 1 CR050730 July 30 2005 1 2 3 4 5 6 7 and 8 PR060207 February 7 2006 1 2 3 4 5 6 7 and 8 CR070228 February 28 2007 1 2 3 4 5 6 7 8 and 9 COMPLETE REVISION OF MAINTENANCE MANUAL 761 876 Revisions appear in all Aerofiche Cards Accordingly discard your entire existing Aerofiche Card S...

Page 1040: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 1 Feb 28 07 AEROFICHE EFFECTIVITY 6A4 THIS PAGE INTENTIONALLY BLANK ...

Page 1041: ...Feb 28 07 Intro Table of Contents 1 Feb 28 07 2 Feb 28 07 Introduction 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 Index 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHA...

Page 1042: ...PAGE 2 Feb 28 07 INTRO LIST OF EFFECTIVE PAGES 6A6 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1043: ...A9 Effectivity 2 6A10 Serial Number Explanation 2 6A10 Assignment of Subject Material 2 6A10 Pagination 3 6A11 Aerofiche Effectivity 3 6A11 Identifying Revised Material 3 6A11 Indexing 3 6A11 List of Effective Pages 3 6A11 Warnings Cautions and Notes 3 6A11 Accident Incident Reporting 4 6A12 Supplementary Publications 4 6A12 Piper Publications 4 6A12 Vendor Publications 4 6A12 Chapter Section Inde...

Page 1044: ...PAGE 2 Feb 28 07 6A8 INTRO CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1045: ...GENUINE PIPER AIRCRAFT PARTS OR PIPER AIRCRAFT APPROVED PARTS OBTAINED FROM PIPER APPROVED SOURCES IN CONNECTION WITH THE MAINTENANCE AND REPAIR OF PIPER AIRPLANES Genuine PIPER parts are produced and inspected under rigorous procedures to ensure airworthiness and suitability for use in PIPER airplane applications Parts purchased from sources other than PIPER even though identical in appearance ma...

Page 1046: ...ane are broken down into subsystems These sub systems are identified by the second element of the standard numbering system The element 40 of the number 28 40 01 concerns itself with the indicating section of the fuel system C Unit Subject The individual units within a sub system section may be identified by the third element of the standard numbering system The element 01 of the number 28 40 01 i...

Page 1047: ...his set 8 Identifying Revised Material A revision to a page is defined as any change to the printed matter that existed previously Revisions additions and deletions are identified by a vertical line i e change bar along the left hand margin of the page opposite only that portion of the printed matter that was changed A change bar in the left hand margin opposite the footer i e chapter section subj...

Page 1048: ...s Catalog P N 761 878 2 Periodic Inspection Report Form P N 767 011 3 Progressive Inspection Manual 50 hour P N 767 013 B Vendor Publications WARNING FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION S WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT MAY RENDER THE AIRCRAFT UNAIRWORTHY 1 AIR CONDITIONING COMPRESSOR Vendor Address Sanden International USA Inc PH 972 442 8400...

Page 1049: ...cialty Systems PH 330 374 3040 Goodrich Corporation FAX 330 374 2290 1555 Corporate Woods Parkway Uniontown Ohio 44685 8799 Technical Assistance PH 800 334 2377 330 374 3743 FAX 330 374 2290 Email dssd support goodrich com http www deicingsystems goodrich com Black Standard Pneumatic De Icer Installation Maintenance and Repair Manual ATA 30 10 31 SmartBoot System ATA 30 10 65 8 ELECTRONIC FLIGHT I...

Page 1050: ...ntext See www avantext com or PH 800 998 8857 11 FIRE EXTINGUISHER PORTABLE Vendor Address H3R Inc PH 800 249 4289 43 Magnolia Ave 4 San Francisco California 94123 2911 http www h3r com index htm 12 FORCE APPLICATOR KIT Vendor Address Safe Flight Instrument Corp PH 914 946 9500 20 New King Street White Plains New York 10602 13 FUEL BOOST PUMP Vendor Address Parker Hannifin Corp PH 800 272 7537 Nic...

Page 1051: ...ww unisonindustries com index4 html Installation Operation F1100 MASTER SERVICE MANUAL and Maintenance 4300 6300 SERIES MAGNETO MAINTENANCE AND Instructions OVERHAUL MANUAL L 1363 19 NAVIGATION COMMUNICATIONS AND GPS NAV COM GPS Vendor Address Garmin International PH 913 397 8200 1200 East 151ST Street Olathe KS 66062 http www garmin com 20 OXYGEN SYSTEM Vendor Address Scott Aviation PH 716 683 51...

Page 1052: ...DAR WEATHER RDR 2000 Vendor Address Honeywell Bendix King See Autoflight above Maintenance Manual Bendix King ART 2000 P N 006 05332 0001 25 RADIO COOLING BLOWER Vendor Address Globe Motors PH 937 228 3171 2275 Stanley Ave FAX 937 229 8531 Dayton Ohio 45404 http www globe motors com home html 26 STARTER Vendor Address Kelly Aerospace See Alternator above or Sky Tec Partners Ltd PH 800 476 7896 350...

Page 1053: ...MALIBU MIRAGE MAINTENANCE MANUAL 28 VACUUM PUMP Vendor Address Aero Accessories Inc PH 800 822 3200 1240 Springwood Avenue Gibsonville NC 27249 http www aeroaccessories com index html 29 VACUUM REGULATORS Vendor Address Parker Hannifin Corp see Fuel Boost Pump above ...

Page 1054: ...PAGE 10 Feb 28 07 INTRODUCTION 6A18 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1055: ...chapter CHAPTER SECTION TITLE GRID NO 4 AIRWORTHINESS LIMITATIONS 1C1 00 Airworthiness Limitations 5 TIME LIMITS MAINTENANCE CHECKS 1C9 00 General 10 Time Limits 20 Scheduled Maintenance Checks 30 Special Inspections 50 Unscheduled Maintenance Checks 6 DIMENSIONS AND AREAS 1E13 00 General 7 LIFTING AND SHORING 1F1 10 Jacking 8 LEVELING AND WEIGHING 1F9 10 Weighing and Balancing 20 Leveling 9 TOWIN...

Page 1056: ...emperature Control 22 AUTOFLIGHT 2F11 10 Autopilot 23 COMMUNICATIONS 2G19 00 General 50 Audio Integrating 60 Static Discharging 24 ELECTRICAL POWER 2H11 00 General 30 DC Generation 40 External Power 60 Electrical Load Distribution 25 EQUIPMENT FURNISHINGS 2J11 10 Flight Compartment 20 Passenger Compartment 50 Cargo Compartments 60 Emergency 26 FIRE PROTECTION 2K15 20 Extinguishing 27 FLIGHT CONTRO...

Page 1057: ...rs 60 Propellers Rotors 31 INDICATING RECORDING SYSTEMS 4C1 50 Central Warning Systems 32 LANDING GEAR 4C13 00 General 10 Main Gear and Doors 20 Nose Gear and Doors 30 Extension and Retraction 40 Wheels and Brakes 50 Steering 60 Position and Warning 33 LIGHTS 4G5 10 Flight Compartment 20 Passenger Compartment 30 Cargo and Service Compartments 40 Exterior 34 NAVIGATION 5C1 00 General 10 Flight Envi...

Page 1058: ...00 General 10 Investigation Cleanup and Aerodynamic Smoothness 70 Repairs 80 Electrical Bonding 52 DOORS 6G13 10 Passenger Crew 20 Emergency Exit 30 Cargo 70 Monitoring and Operation 55 STABILIZERS 6H13 00 General 10 Horizontal Stabilizers 20 Elevator 30 Vertical Stabilizer 40 Rudder 56 WINDOWS 6I19 00 General 10 Flight Compartment 20 Cabin 30 Door 57 WINGS 6K5 40 Attach Fittings 50 Flight Surface...

Page 1059: ... Power Supply 20 Distribution 76 ENGINE CONTROLS 7G17 10 Power Control 77 ENGINE INDICATING 7H3 10 Power 20 Temperature 40 Integrated Engine Instrument Systems 79 OIL 7J3 20 Distribution 30 Indicating 80 STARTING 7J15 10 Cranking 81 TURBINES 7K9 20 Turbo Supercharger 91 CHARTS WIRING DIAGRAMS 8C1 10 Charts 21 and up Electrical Schematics 91 CONT CHARTS WIRING DIAGRAMS CONT 9C1 Electrical Schematic...

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Page 1061: ...sion Control Wing 6L3 Attitude Indicator 5D5 Autopilot 2F17 Component Locator 2G2 Installation 2F18 2F20 Maintenance 2F23 Operational Checkout 2F24 Pitch Servo 2G12 Pressure Transducer 2G6 Roll Servo 2G4 Servo Clutch Torque Adjustment 2G15 Trim Monitor 2G3 Trim Servo 2G6 Yaw Amplifier 2G14 Yaw Servo 2G10 Avionics Cooling 2C14 Avionics Master Switch 2H1 B Ball Diameters for Testing Hose Restriction...

Page 1062: ...rrection 2I10 Troubleshooting 2I7 2I13 Valve Regulated Lead Acid 2I13 Bonding 6G9 Resistance Index 6G10 Buses Avionics 2H19 Main 2H19 Circuit Breaker Panel 6D22 Electrical Shelf 6E7 External Power 2I19 Load Distribution 2J1 Relay Installation Co Pilot s Side 6E10 K1 thru K8 6E10 Pilot s Side 6E9 Schematics Air Conditioning 8E7 Airspeed Standby 9E19 Altimeter Radar 9F14 Altimeter Standby 9E19 Annun...

Page 1063: ...n Light 9E5 WX 500 9F11 XM Receiver 8E23 Switch Panels 6E1 Symbols 8D14 System 2H17 Troubleshooting 2H20 Tie Bus Panel Connections 6E3 Volt Ammeter 2J4 Voltage Regulation and Control 2H19 Wire Coding 8D13 Elevator Balancing 6I3 Control System Installation 3D23 Rigging and Adjustment 3D24 Troubleshooting 3D19 Torque Tube Bearing Changes 3D20 Trim Controls Actuator Assembly 3E3 Corrosion Control 3E4...

Page 1064: ...Drain Valve 3G8 Draining 1I19 Draining Moisture 1I18 Fuel Filter 3G7 Fuel Pumps Specifications 3G5 Fuel Quantity Gauge Accuracy Test 3G14 Full Range Check 3G20 Senders 3G13 Leak Test Setup 3G1 Selector Switch and Valve 3G6 Cable Adjustment 3G7 Troubleshooting 3F16 Leak Evaluation 3F22 G GMA 340 Audio Panel Adjustments 2H6 Installation 2H3 System Functional Test 2H4 GNS 430 5F5 GNS 530 5F5 Ground C...

Page 1065: ... 4D11 Position and Warning 4F19 Landing Gear Up Power Reduced Warning Switch Adjustment 4G2 Troubleshooting 4F20 Leading Particulars and Principal Dimensions 1E20 Leveling 1F17 Life Limited Parts 1C7 Lifting 1F7 See also 57 40 00 Lights Exterior 4H3 Landing 4H7 Position 4H4 Pulse 4H7 Strobe 4H3 Taxi 4H6 Wing Inspection Light 4H7 Interior 4G11 Annunciator Panel 4G12 Baggage Area 4G21 Forward 4H1 Re...

Page 1066: ...g 3K6 Troubleshooting 3J20 Propeller Assembly 7C9 Publications Piper A12 Vendor A12 Q Quad Digital Indicator QDI See Engine Instruments Transicoil EMIS R Radar 5F1 Repairs Fiberglass 6F19 Metal Wire Stitching 6G5 Thermoplastic 6F21 List of Materials 6F24 Window Windshield Acrylic 6J10 Restraint System 2J23 Inertial Reel Adjustment 2J23 Inspection 2J23 Revised Material A11 Robinair 34700 Charging S...

Page 1067: ... Bellcrank Centering 4C22 Horn Arm Gap 4C22 Nose Wheel Centering 3C15 4C22 Rudder Pedal Neutral Alignment 3C15 4C22 Rudder Travel Tool 3C15 Torque Conversion 8C20 Torque Wrench Formula 1K2 Towing 1G5 Transponder 5F9 GTX 327 5F9 GTX 330 5F9 Post Installation Setup Procedure 5F10 ARINC 429 Configuration Page 5F11 Display Mode and Key Lighting 5F11 Hexadecimal Conversion 5F13 Operation Configuration ...

Page 1068: ...in 6I11 Vertical Speed Indicator 5C18 Volt Ammeter See Electrical W Warnings Cautions and Notes A11 Weather Radar 5F1 Weighing 1F15 Wheel Brake Assembly 4F4 Wheels Bearing Cup 4F4 Main Wheel Assembly 4F2 Nose Wheel Assembly 4F1 Repairs 4F3 Windows and Windshields Door Window 6K3 Heated Windshield Testing 3J15 Troubleshooting 3J15 Inspection and Repair Definitions 6J1 Limitations 6J1 Crack Limitati...

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Page 1070: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 10 Feb 28 07 INDEX 6B10 GRIDS 6B10 THRU 6B24 INTENTIONALLY BLANK ...

Page 1071: ...6C1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 35 OXYGEN ...

Page 1072: ...6C2 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1073: ... MANUAL CHAPTER SECTION PAGE DATE CHAPTER SECTION PAGE DATE 35 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 35 Table of Contents 1 Feb 28 07 2 Feb 28 07 35 10 00 1 Feb 28 07 2 Feb 28 07 35 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 CHAPTER 35 LIST OF EFFECTIVE PAGES ...

Page 1074: ...PAGE 2 Feb 28 07 35 LIST OF EFFECTIVE PAGES 6C4 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1075: ...MAINTENANCE MANUAL CHAPTER 35 OXYGEN TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO CREW 35 10 00 1 6C7 Fixed Oxygen Generator System 1 6C7 PASSENGER 35 20 00 1 6C9 Description 1 6C9 Fixed Oxygen Generator System 1 6C9 100 Hour Inspection 1 6C9 Removal 2 6C10 Installation 2 6C10 ...

Page 1076: ...PAGE 2 Feb 28 07 6C6 35 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1077: ...and for approximately 15 minutes i e long enough for the airplane to be flown to an altitude of 10 000 feet or less The pilot s and copilot s oxygen generators are located in a tray under the copilot s seat A drawer containing two masks opens inboard The basic system is the same as that installed for the passengers See 35 20 00 for detailed information on removal installation and inspection ...

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Page 1079: ...eless handling is to be avoided The generators have a percussion cap igniter on one end which must be protected with a plastic cover when the generator s are removed from the mounting tray drawer Do not remove this plastic protective cover until the generator is installed reinstalled in the mounting tray drawer and the system is rearmed NOTE Installed generators are normally removed only when expe...

Page 1080: ...PAGE 2 Feb 28 07 6C10 35 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Oxygen System Installation Figure 1 ...

Page 1081: ...during removal and handling 6 Remove generator from mounting tray drawer C Installation NOTE New generators are delivered from the factory with the lanyards and firing pin installed and the hammer armed A plastic protective cover protects the percussion cap from being ignited if the firing pin is inadvertently pulled during handling If the firing pin has been pulled during handling verify that the...

Page 1082: ...LASTIC PROTECTIVE COVER FROM THE PERCUSSION CAP WILL PREVENT THE GENERATOR FROM IGNITING WHEN THE LANYARD IS PULLED 7 Remove the plastic protective cover see Figure 2 from the percussion cap on the newly installed generator 8 Install mounting tray drawer in aircraft 9 Connect the wiring harness turn ON the master switch and verify the annunciator panel warning light remains out If not recheck that...

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Page 1085: ...6C15 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 37 VACUUM ...

Page 1086: ...6C16 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1087: ...ECTION PAGE DATE 37 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 37 Table of Contents 1 Feb 28 07 2 Feb 28 07 37 00 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 37 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 37 20 00 1 Feb 28 07 2 Feb 28 07 CHAPTER SECTION PAGE DATE ...

Page 1088: ...PAGE 2 Feb 28 07 37 LIST OF EFFECTIVE PAGES 6C18 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1089: ...1 6C21 Troubleshooting 1 6C21 DISTRIBUTION 37 10 00 1 6D3 Hoses and Clamps 1 6D3 Gyro Filter 1 6D3 Vacuum Pump s 2 6D4 Inspection 2 6D4 Removal 3 6D5 Installation 3 6D5 Replacing Pump Fittings 3 6D5 Vacuum Regulator s 4 6D6 Removal 4 6D6 Installation 4 6D6 Service Tips 4 6D6 Adjustment 4 6D6 INDICATING 37 20 00 1 6D11 Vacuum Suction Gauge S N s 4636001 thru 4636020 only 1 6D11 Service Tips 4 6D11 ...

Page 1090: ...PAGE 2 Feb 28 07 6C20 37 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1091: ...low button will protrude should the counterclockwise rotating pump fail The total vacuum pressure which is displayed on the vacuum gauge is normally regulated between 4 8 and 5 2 inches of mercury in Hg In S N s 4636021 and up the vacuum gauge has been incorporated into the Transicoil Electronic Module Instrument System see 77 40 00 A transducer mounted on the rear of the forward pressure bulkhead...

Page 1092: ...1 thru 4636020 CLOCKWISE ROTATING VACUUM PUMP VACUUM REGULATOR AIR INLET FILTER VACUUM PRESSURE SWITCH FIREWALL PRESSURE BULKHEAD INSTRUMENT PANEL AIRCRAFT VACUUM MANIFOLD CHECK VALVE CO PILOTS AIR DRIVEN GYROS OPTIONAL COUNTER CLOCKWISE ROTATING VACUUM PUMP C L VACUUM GAUGE ATTITUDE GYRO CABIN PRESSURE CONTROLLER TO CABIN PRESSURE SYSTEM 89680 AJ ...

Page 1093: ...RE SWITCH FIREWALL PRESSURE BULKHEAD INSTRUMENT PANEL AIRCRAFT VACUUM MANIFOLD CHECK VALVE CO PILOTS AIR DRIVEN GYROS OPTIONAL COUNTER CLOCKWISE ROTATING VACUUM PUMP C L VACUUM GAUGE Located in EMIS stack PILOT S ATTITUDE GYRO CABIN PRESSURE CONTROLLER TO CABIN PRESSURE SYSTEM 89680 AJ VACUUM TRANSDUCER Vacuum System Figure 1 Sheet 2 of 3 Effectivity 4636021 thru 4636374 ...

Page 1094: ...SE ROTATING VACUUM PUMP VACUUM REGULATOR AIR INLET FILTER VACUUM PRESSURE SWITCH FIREWALL PRESSURE BULKHEAD AIRCRAFT VACUUM MANIFOLD CHECK VALVE COUNTER CLOCKWISE ROTATING VACUUM PUMP C L TO CABIN PRESSURE SYSTEM VACUUM TRANSDUCER 89680 AJ Vacuum System Figure 1 Sheet 3 of 3 Effectivity 4636375 and up ...

Page 1095: ...ustments in this section Line from gyros to filter Repair or replace line restricted Line between pumps and Check all lines and manifold or between gyros fittings and manifold leaking In S N s 4636001 thru 4636020 only Vacuum gauge reading 4 8 to Clockwise rotating vacuum Replace lower vacuum 5 2 in Hg but left red button pump inoperative pump on gauge protruding or Vacuum gauge reading 4 8 to Cou...

Page 1096: ...de Regulator sticky Clean regulator Vacuum correct but pilot Regulator sticky Clean regulator reports pressure erratic or shows complete loss in flight Oil in pump due to leaky Replace pump engine seal or cleaning fluid blown into pump while cleaning engine Pressure can only be maintained Leak in system Repair or replace lines at full throttle on ground Worn pump Replace pump Stuck regulator Clean...

Page 1097: ...D Ensure hoses are clear and clean by blowing them out with shop air Remove from aircraft as required CAUTION DO NOT WIGGLE HOSE FROM SIDE TO SIDE DURING INSTALLATION WIGGLING COULD CAUSE PARTICLES TO BE CUT FROM INNER WALL OF HOSE WHICH WOULD DAMAGE THE PUMP E Where hose clearance is tight making it difficult to reinstall it onto a fitting or barb spray the fitting or barb with silicone Let dry t...

Page 1098: ...est Dry Air Vacuum Pumps are factory installed in S N s 4636339 up and as service replacements The following inspection applies only to those pumps The vacuum pump s feature a wear indicator inspection port on the back cover which allows direct observation of pump vane wear Beginning at 500 hours time in service and each 100 hours thereafter remove the inspection port plug and observe vane wear as...

Page 1099: ...nect hoses to pump and secure with hose clamps 5 Reinstall engine cowling D Replacing Pump Fittings CAUTION WHEN REPLACING ANY OF THE THREADED FITTINGS DO NOT USE PIPE DOPE THREADLUBE OR TAPE PIPE DOPE TAPE PARTICLES INGESTED BY THE VACUUM PUMP COULD CAUSE THE PUMP TO FAIL USE ONLY SILICONE SPRAY LETTING IT DRY BEFORE ASSEMBLY 1 Before installing any fittings on pump check for any external damage ...

Page 1100: ...mselves act as a limiting device to keep the vacuum power applied from exceeding safe levels NOTE If the panel gauge has been checked and found OK and the vacuum gauge reading does not repeat within the normal operating range as marked on the gauge then the regulating valve should be changed Observe the usual precautions for maintaining system cleanliness to avoid premature pump service D Adjustme...

Page 1101: ...L 7 Uncap the line that goes to the vacuum regulator valve and connect it to the valve 8 Disconnect line going to the other vacuum regulator valve 9 Wrap or cap the end of line with a clean porous cloth to prevent foreign matter and debris from entering the system 10 Repeat Steps 3 through 7 ...

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Page 1105: ...ervice and usually is replaced when malfunctions occur NOTE Suction gauge failure in a properly operating vacuum system does not impair safety of flight NOTE Two different models of vacuum gauge may be installed in PA 46 350P airplanes One is marked with a normal operating range of 4 8 to 5 2 in hg and the other is marked with a normal operating range of 4 5 to 5 2 in hg The vacuum system in a par...

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Page 1107: ...6D13 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 39 ELECTRICAL ELECTRONIC PANELS ...

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Page 1109: ...ive Pages 2 Feb 28 07 39 Table of Contents 1 Feb 28 07 2 Feb 28 07 39 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 39 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 CHAPTER SECTION PAGE ...

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Page 1111: ...NTENTS SUBJECT SECTION PAGE GRID NO INSTRUMENT AND CONTROL PANELS 39 10 00 1 6D19 General 1 6D19 Face Mounted Instruments 1 6D19 Removal 1 6D19 Installation 3 6D21 Rack Mounted Avionics 3 6D21 Removal 3 6D21 Installation 3 6D21 Circuit Breaker Panels 3 6D21 Switch Panels 7 6E1 ACCESSORY COMPARTMENTS 39 20 00 1 6E7 Electrical Shelf and Panels 1 6E7 ...

Page 1112: ...PAGE 2 Feb 28 07 6D18 39 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1113: ... each fitting NOTE For those instruments which remove through the front of the panel disconnecting and tagging plumbing and or electrical connectors can be done after the instrument retaining screws are removed and the instrument is slid gently forward to expose the connections at the rear b Remove the screws that secure the instrument in the panel cutout c Remove the instrument from the panel I N...

Page 1114: ...AGE 2 Feb 28 07 6D20 39 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Instrument Panel Installations Typical Figure 2 S N s 4636001 THRU 4636020 ONLY TIE BUS CIRCUIT BREAKER PANEL ...

Page 1115: ...icantly inset from the panel If so correct the tray rack installation before proceeding NOTE The high insertion forces required to seat a unit with high density connectors tend to limit the effectiveness of the first seating attempt Accordingly the following procedure requires sequential applications of force and subsequent tightening of the jackscrew to ensure all connectors seat properly a Slide...

Page 1116: ...PAGE 4 Feb 28 07 6D22 39 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Circuit Breaker Placard Screw Screw Profile View Circuit Breaker Panel Figure 3 Sheet 1 of 2 ...

Page 1117: ...RN FUEL MGT FLIGHT SYSTEMS MAP LIGHT FLAP MOTOR FLAP WARN R BOOST L BOOST EMERG FUEL PUMPS STANDBY VAC LANDING GEAR INDICATION WARNING HYDRAULIC PUMP CONTROL POWER ALTERNATOR NO 1 NO 2 HOUR METER AIR CONDITIONING CONTROL POWER CABIN FANS CABIN LIGHTS COPILOT Front View Typical Pilot s Fwd Panel Shown TURN COORD ENGINE START CABIN PRESS DUMP Circuit Breaker Panel Figure 3 Sheet 2 of 2 ...

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Page 1119: ...he cockpit overhead panel b Squeeze retainer blades on top and bottom of the switch together and push switch from the panel c Make note of the placement of wires on the switch to facilitate installation d Disconnect wires from the switch Remove switch 2 Installation a Connect wires to switch b Push switch into the panel Squeeze retainer blades on top and bottom of the switch together if required c...

Page 1120: ...PAGE 8 Feb 28 07 6E2 39 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Environmental Deice Switch Panel Figure 4 Effectivity 4636132 thru 4636374 ...

Page 1121: ...PAGE 9 Feb 28 07 6E3 39 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Tie Bus Panel Connections Figure 5 ...

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Page 1125: ...ess for service due to the tight quarters involved and to prevent unnecessary tugging on the electrical cable pressure seal where it passes through the pressure bulkhead External Power Contactor Start Contactor Battery Master Contactor Current Limiter Current Limiter SPKR AMP CIG LIGHTER COMM CLOCK COURTESY LIGHTS STEREO A A VIEW A A LOOKING INBOARD FROM LEFT UNDER THE FORWARD BAGGAGE COMPARTMENT ...

Page 1126: ...tivity 4636375 and up Electrical Shelf Typical Figure 1 Sheet 2 of 2 CLOCK LIGHTS COURTESY AMP SPKR CIG LIGHTER STEREO COMM A A X1 X2 A2 BATTERY MSTR CONTACTOR K401 A1 105134 A K404 START CONTACTOR EXT PWR CONTACTOR K403 VIEW A A LOOKING INBOARD FROM LEFT UNDER THE FORWARD BAGGAGE COMPARTMENT FLOOR ...

Page 1127: ...7 00 F S 108 00 104310 B 104088 NEW 89799 F CURRENT SENSOR CURRENT SENSOR S N S 4636021 THRU 4636247 ONLY FLASHER ASSY S N S 4636248 AND UP COVER PANEL ANNUNCIATOR DIMMING ASSY STARTING VIBRATOR ASSY START RELAY START VIBRATOR Relay Installation Pilot s Side Figure 2 Effectivity 4636001 thru 4636186 ...

Page 1128: ...T GROUND CLEAR STALL FAIL TERMINAL BOARD SPEEDBRAKE LOGIC CONTROL GROUND STRAP GROUND STRAP EMERGENCY GEAR RELEASE CABLE REF PANEL COVER FLAP CONTROL CABLE REF F S 108 00 J317 P317 SQUAT SW NO 1 RELAY 104310 B 104088 NEW 89799 F 101309 F S N S 4636299 AND 4636314 UP WITH SPEEDBRAKE OPTION IN S N S 4636187 UP P3 TO SB J3 P2 TO SB J2 J1 TO SB P1 K1 thru K8 Relay Installation Co Pilot s Side Figure 3...

Page 1129: ...PAGE 5 Feb 28 07 6E11 39 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL K1 thru K8 Relay Installation Co Pilot s Side Figure 3 Sheet 2 of 8 Effectivity 4636001 thru 4636186 ...

Page 1130: ... REQ N C N O C COIL 27 A 5 1 3 K4 B 2 4 6 25 A 5 3 1 K3 B 4 6 2 29 31 32 3 20 6 10 2 A 1 3 5 K6 B 6 4 2 A 1 5 9 4 5 13 1110 1 14 21 K1 B 3 11 7 4 8 12 A 1 9 5 24 22 23 8 2 26 12 K2 B 2 6 10 4 8 3 7 11 TO R317 TO R329 TO R329 19 28 6 7 9 TO R317 RESISTOR CHT SCANNER LIGHTS DIMMING RESISTOR SPEEDBRAKE ANNUN DIMMING R317 R329 TO K2 1 TO K2 7 TO K2 3 TO K2 5 J317 101305 E G SHT 1 TO TERMINAL BOARD TER...

Page 1131: ...5 B K6 2 4 6 A B K1 10 2 6 1 5 9 3 4 7 8 11 12 A B K2 10 5 9 1 8 12 4 2 6 7 11 3 25 27 29 31 5 32 4 3 11 13 10 1 24 21 14 22 23 2 8 20 26 1928 6 TO R329 TO R317 7 J317 R329 R317 TO J317 12 TO K2 1 TO K2 3 TO K2 7 RESISTOR CHT SCANNER LIGHTS DIMMING RESISTOR SPEEDBRAKE ANNUN DIMMING TO J317 3 TO K2 5 TO R317 12 15 TO J317 15 TO J317 12 101305 E G SHT 2 K1 thru K8 Relay Installation Co Pilot s Side ...

Page 1132: ...5 27 29 31 32 15 12 3 4 13 5 10 11 14 1 21 23 6 2 8 19 20 26 28 7 TO TERMINAL BOARD J317 R317 101305 G G SHT 3 A B A B A B A B A B 1 3 5 2 4 6 N C N O C 1 3 5 2 4 6 1 3 5 2 4 6 10 2 6 1 5 9 3 4 7 8 11 12 10 2 6 1 5 9 3 4 7 8 11 12 IN4719 DIODE 2 REQ TO J317 15 TO J317 12 TERMINAL BOARD RESISTOR SPEEDBRAKE ANNUN DIMMING TO J317 12 TO K2 1 TO J317 3 TO K2 5 K4 K3 K6 K1 K2 TO R317 TO R317 IN2071A DIO...

Page 1133: ...R AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Effectivity 4636001 thru 4636131 K7 K5 7 9 10 11 12 13 8 3 4 5 6 J387 1 3 5 4 6 2 B A 1 3 5 6 4 2 A B 89896 E K1 thru K8 Relay Installation Co Pilot s Side Figure 3 Sheet 6 of 8 ...

Page 1134: ...00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL K7 K5 7 15 16 14 9 10 11 12 13 8 3 4 5 6 J387 1 3 5 4 6 2 B A 1 5 9 2 6 10 12 11 7 8 4 3 89896 F K1 thru K8 Relay Installation Co Pilot s Side Figure 3 Sheet 7 of 8 ...

Page 1135: ...ru K8 Relay Installation Co Pilot s Side Figure 3 Sheet 8 of 8 Effectivity 4636299 4636314 and up K7 1 5 9 2 6 10 12 11 8 4 3 A 5 3 1 B 6 4 2 J387 10 9 1 7 6 4 K5 N C N O COM 3 MIL W 81044 12 18 9 2 16 14 11 12 13 8 4 8 12 11 9 10 3 7 5 1 2 6 5 17 18 N C N O COM 20 K8 1N2071A DIODE 7 24 23 104311 A B ...

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Page 1137: ...6F1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 51 STRUCTURES ...

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Page 1139: ...b 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 51 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 51 70 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 51 80 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 CHAPTER SECT...

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Page 1141: ...rms of Corrosion 1 6F11 Conditions Affecting Corrosion 1 6F11 Inspection 3 6F13 Corrosion Removal and Control 3 6F13 Corrosion Prone Areas 4 6F14 REPAIRS 51 70 00 1 6F19 Fiberglass Repairs 1 6F19 Touch up and Surface Repairs 1 6F19 Fracture and Patch Repairs 2 6F20 Thermoplastic Repairs 3 6F21 Pressure Sensitive Safety Walk Installation 10 6G4 Metal Wire Stitch Repair 11 6G5 ELECTRICAL BONDING 51 ...

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Page 1143: ...11 7 11 11 12 10 11 11 11 9 15 9 15 5 6 1 6 NUMBER MATERIAL THICKNESS 1 2024 0 020 2 2024 0 025 3 2024 0 032 4 2024 0 040 5 2024 0 025 6 2024 0 032 7 2024 0 040 8 2024 0 063 9 2024 T3 020 10 2024 T3 025 11 2024 T3 032 12 2024 T3 040 13 2024 T3 040 14 5052 H34 025 15 FIBERGLASS 16 2024 T3 016 HEAT TREAT TO T42 Skin Material Specifications Figure 1 Sheet 1 of 2 GENERAL ...

Page 1144: ...MALIBU MIRAGE MAINTENANCE MANUAL 15 5 15 6 11 11 12 11 6 6 6 12 5 15 11 11 9 9 15 11 11 11 4 9 10 11 11 11 11 11 9 10 11 12 11 11 11 11 11 10 12 11 10 10 10 12 16 11 10 12 11 10 10 10 12 16 10 10 10 10 16 16 6 6 Skin Material Specifications Figure 1 Sheet 2 of 2 ...

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Page 1147: ...y way to find it before structural failure is by disassembly and inspection Insulating is necessary between two contacting dissimilar surfaces 2 to 3 coats of zinc chromate on each surface plus if one of the surfaces is magnesium a 0 003 inch thick piece of vinyl tape 3 Intergranular Corrosion is difficult to detect in its early stages When severe it causes the surface of the metal to exfoliate fl...

Page 1148: ... metal protecting until iron appears surfaces from which cadmium has been depleted Chromium plating May pit in chloride environment Polishing and buffing NOTES 1 Red rust generally shows on bolts nuts and other aircraft hardware Rust in these areas is generally not dangerous however it shows a need for maintenance and the possibility of corrosive attack in more critical areas Any surface corrosion...

Page 1149: ...inted surfaces See Per Specific Operation Operating Environment 5 30 00 3 Inspection for corrosion must be performed by personnel familiar with corrosive problems and remedies a Daily and preflight inspection must include engine frontal areas all intake vents engine compartments gaps seams and faying surfaces in exterior skins wheel and wheel well areas battery compartment fuel cell all other drai...

Page 1150: ...ng potential moisture entry points in the spot weld filled with a sealant or preservative compound On an aluminum spot welded assembly a chromate conversion coating before paint is applied will help prevent corrosion 4 Areas exposed to exhaust gases may have their finish damaged by deposits These deposits may result in an aggressive attack on the metal by corrosion Heat from the exhaust may also b...

Page 1151: ...e treatment proper insulation due to dissimilar metal corrosion and paint coatings 13 Electrical components and connectors must be checked Inspection frequency is based on operational environment and past trouble 14 Skin joints and lap overs are two areas that can trap and hold moisture Corrosion in these areas may go unnoticed unless particular attention is paid to them during inspection 15 Hoses...

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Page 1155: ...air kit A Touch up and Surface Repairs 1 Remove wax oil and dirt from around the damaged area with acetone Methylethylketone or equivalent and remove paint to gel coat 2 The damaged area may be scraped with a fine blade knife or a power drill with a burr attachment to roughen the bottom and sides of the damaged area Feather the edge surrounding the scratch or cavity Do not undercut the edge If the...

Page 1156: ...inum formed to a similar contour may be placed over the area The aluminum should also be covered with cellophane 6 Prepare a patch of fiberglass mat and cloth to cover an area two inches larger than the hole 7 Mix a small amount of resin and catalyst enough to be used for one step at a time according to kit instructions 8 Thoroughly wet mat and cloth with catalyzed resin Daub resin on mat first an...

Page 1157: ...ld cleaners have proven most effective in removing surface dirt 2 Preliminary cleaning of the damaged area with perchlorethylene or V M P Naphtha will generally ensure a good bond between epoxy compounds and thermoplastic B Surface Scratches Abrasion or Ground in Dirt See Figure 1 1 Shallow scratches and abraded surfaces are usually repaired by following directions on containers of conventional au...

Page 1158: ...PAGE 4 Feb 28 07 6F22 51 70 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Deep Scratches Shallow Nicks and Small Holes Figure 2 Surface Scratches Abrasions or Ground in Dirt Figure 1 ...

Page 1159: ...PAGE 5 Feb 28 07 6F23 51 70 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Mixing of Epoxy Patching Compound Figure 3 Welding Repair Method Figure 4 ...

Page 1160: ...quires a hot air gun and ABS rods To weld the gun should be held to direct the flow of hot air into the fusion repair zone heating the damaged area and rod simultaneously The gun should be moved continuously in a fanning motion to prevent discoloration of the material Pressure must be maintained on the rod to ensure good adhesion see Figure 4 11 After the repair is completed sanding is allowed to ...

Page 1161: ...patch should be made of the same material and cut slightly larger than the section being repaired 2 When appearances are important large holes cracks tears etc should be repaired by cutting out the damaged area and replacing it with a piece of similar material 3 When cutting away the damaged area under cut the perimeter and maintain a smooth edge The patch and or plug should also have a smooth edg...

Page 1162: ...PAGE 8 Feb 28 07 6G2 51 70 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Various Repairs Figure 6 ...

Page 1163: ...commended that parts be cleaned prior to painting with a commercial cleaner or a solution made from one fourth cup of detergent mixed with one gallon of water 3 The paint used for coating thermoplastic can be either lacquers or enamels depending on which is preferred by the repair facility or customer NOTE It is extremely important that solvent formulations be considered when selecting a paint bec...

Page 1164: ...nated remove the contamination with clean dry rags or paper wipers moistened with MIL S 18718 Safety Solvent 3 Prior to applying the safety walk wipe the applicable surface with a clean dry cloth ensuring that no moisture remains on the surface B Application Procedure 1 Do not apply when surface temperature is below 50 2 Peel back the full width of the protective liner leading edge approximately t...

Page 1165: ...te Rivet Method of Joining 1 Substitute two rivets in lieu of each staple where stitching was previously used or is specified Maintain a minimum of 75 inch spacing between rivets 2 When materials being joined include Stainless Steel Galvanized Steel or Steel use a MS20615M4 Rivet Monel and NAS1149CN432R Washer See Figure 9 b Install with manufactured factory head against hardest material Install w...

Page 1166: ...PAGE 12 Feb 28 07 6G6 51 70 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Metal Wire Stitching Repair Figure 9 ...

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Page 1169: ...in any way with the operation of moveable components of the aircraft C No self tapping screws used for bonding purposes D Exposed conducting frames or parts of electrical or electronic equipment should have a low resistance bond of less than 2 5 millohms to structure If the equipment design includes a ground terminal or pin which is internally connected to such exposed parts a ground wire connecti...

Page 1170: ...Exterior Lights Mounted on Non Conductive Material 003 Avionics Black Boxes 003 NOTE Harnesses should be installed and connected for this check internal chassis wiring through the connector to ground is permissible for this grounding Battery Ground Point 010 Static wick mounting plates TCO Model B 4 P N 452 094 1 00 NOTE Where jumper wires or cables are used to accomplish a proper bond resistance ...

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Page 1173: ...6G13 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 52 DOORS ...

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Page 1175: ...52 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 52 Table of Contents 1 Feb 28 07 2 Feb 28 07 52 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 52 20 00 1 Feb 28 07 2 Feb 28 07 52 30 00 1 Feb 28 07 2 Feb 28 07 52 70 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 1177: ... 1 6G19 Upper Half 1 6G19 Removal 1 6G19 Installation 2 6G20 Lower Half 2 6G20 Removal 2 6G20 Installation 2 6G20 Door Latching Mechanism 2 6G20 Description 2 6G20 Upper Door 2 6G20 Removal 2 6G20 Installation 5 6G23 Adjustment 5 6G23 Lower Door 5 6G23 Removal 5 6G23 Installation 6 6G24 Door Seal 6 6G24 Removal 6 6G24 Installation 6 6G24 EMERGENCY EXIT 52 20 00 1 6H5 Emergency Exit Door 1 6H5 Remo...

Page 1178: ...HAPTER 52 DOORS TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO MONITORING AND OPERATION 52 70 00 1 6H9 Cabin Door Ajar Warning 1 6H9 Troubleshooting 1 6H9 Switches 1 6H9 Removal 1 6H9 Installation 1 6H9 Adjustment 2 6H10 Checks 2 6H10 Baggage Door Ajar Warning 2 6H10 Adjustment 2 6H10 Checks 2 6H10 ...

Page 1179: ...lieve the weight of the door from the hinge pin to facilitate hinge pin removal e Remove the hinge pin and lift off the door 2 Installation a Align the door hinge with the fuselage hinge and insert the hinge pin b Attach the door holder assembly to the door B Lower Half 1 Removal a Open both upper and lower doors to full open position b Remove the screw washers and nut which secures the cable asse...

Page 1180: ...wn into the door An auxiliary lock is installed in the upper door under the interior handle to prevent inadvertent opening of the door When opening the door from inside the airplane the auxiliary lock handle must be pulled inboard to allow the door handle to rotate The lower door locking mechanism is similar to the upper mechanism except that it has no latch hooks and only one handle Lifting the l...

Page 1181: ...PAGE 3 Feb 28 07 6G21 52 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Door Locking Mechanism Figure 1 Sheet 1 of 2 ...

Page 1182: ...PAGE 4 Feb 28 07 6G22 52 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Door Locking Mechanism Figure 1 Sheet 2 of 2 ...

Page 1183: ...protrude out of the door 1 00 inch with the door handle in the closed position Make adjustments at the pushrod assembly as required 3 Adjustment a Shut and latch both doors b Check gap of hook and latch plate c Hook may be filed 053 max maintaining the same ramp contour to provide engagement with plate on lower door assembly A gap of up to 0 030 maximum between hook and latch plate with hook fully...

Page 1184: ...cle without friction and binding 5 Door Seal See Figure 2 NOTE In S N s 4636001 thru 4636313 only if door seal has been damaged by upper door latch pins being extended while the door is moved towards the closed position install Piper Kit No 767 387 to preclude reoccurrence A Removal To remove the door seal pull the cemented surfaces free of the retainer and or door edge applying MEK as needed to h...

Page 1185: ...PAGE 7 Feb 28 07 6H1 52 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Door Seal Installation Figure 2 ...

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Page 1189: ... the entire door towards the center of the aircraft B Installation To install the door insert the lower lip of the door on the outboard side of the two stops and push the door outwards until the handle snaps into place on the catch assembly 2 Seal A Removal Remove the seal by pulling it away from the skin B Installation 1 Prepare the surface by removing any remaining trace of the old seal or old c...

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Page 1191: ...he door support from the door 3 Lift the door slightly and support it while removing the hinge pin B Installation 1 Align the door hinge with the hinge on the fuselage and install the pin It is recommended that a new pin be used 2 Reconnect the door support to the door 3 Lubricate the pin and close the door C Seal Installation 1 Remove any traces of the old seal 2 Clean the surface to be bonded wi...

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Page 1193: ...ed approximately four 4 inches in front of each of the forward door locking pins b Disconnect the two electrical leads per switch c Loosen the jam nut on the switch and turn the switch body out of the pin support tube assembly 2 Installation a Turn the switch body into the pin support tube assembly Do not tighten the jam nut at this time b Adjust the switches per the following paragraph c Reconnec...

Page 1194: ...an audible click is heard Release the pin noting another audible click c Replace any switch in which the click action and mechanical function is doubtful d Ensure that the DOOR AJAR light in the annunciator panel comes on when the switch is activated 2 Baggage Compartment Door Ajar Warning The baggage door ajar switch is located behind the baggage door latch in the longeron at W L 55 46 A DOOR AJA...

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Page 1197: ...6H13 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 55 STABILIZERS ...

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Page 1199: ...eb 28 07 2 Feb 28 07 55 00 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 55 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 55 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 55 30 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 55 40 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 CHAPTER SECTION PAGE DATE CHAPTER 55 LIST OF E...

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Page 1201: ...tion 1 6H23 Attach Fittings Corrosion Control 1 6H23 ELEVATOR 55 20 00 1 6I3 Elevator 1 6I3 Removal 1 6I3 Installation 1 6I3 Balancing 1 6I3 Balancing Equipment 2 6I4 Elevator Trim Tab Push Rods Attach Brackets 4 6I6 Elevator Trim Tab Rods Corrosion Control 4 6I6 VERTICAL STABILIZER 55 30 00 1 6I11 Vertical Fin 1 6I11 Removal 1 6I11 Installation 1 6I11 Attach Fitting Corrosion Control 1 6I11 RUDDE...

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Page 1203: ...PAGE 1 Feb 28 07 6H19 55 00 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Empennage Installation Figure 1 Sheet 1 of 2 GENERAL ...

Page 1204: ...363P 2 REQ MS21042 3 TORQUE 38 43 IN LBS 3 PLACES NAS1149F0463P AND OR NAS1149F0432 USE ANY COMBINATION OF THICK AND THIN WASHERS TO ELIMINATE GAP BETWEEN BOTTOM OF RUDDER TORQUE TUBE AND TOP OF QUADRANT RUDDER SECTOR AN6 7A NAS1149F0663P 2 REQ MS21042 6 TORQUE 240 270 IN LBS 2 PLACES VERTICAL FIN A B MS21250 06008 MS21299 C6 UNDER HEAD NAS1149F0663P 2 REQ UNDER NUT NAS 1804 6 TORQUE 300 320 IN LB...

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Page 1207: ... and repair replacement is completed reapply Dinitrol AV 8 P N 89500 800 Corrosion Inhibiting Compound NOTE For all fittings inspection of the exposed portion is sufficient unless obvious or extensive corrosion is apparent NOTE Any part exhibiting flaking of the metal due to rust must be replaced NOTE If aluminum skin or structure is corroded beyond a light surface oxidation the area must be repai...

Page 1208: ...D Spray directly into faying surfaces and mating points E Ensure entire attach fitting is treated Spray inside where the fitting is attached to the structure F Apply to approximately 8 mils in thickness Avoid puddling and running Allow to dry 1 to 1 1 2 hours before airplane use Full drying takes 6 to 8 hours Horizontal Stabilizer Attach Fittings Figure 1 ...

Page 1209: ...PAGE 3 Feb 28 07 6I1 55 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Horizontal Stabilizer Forward Attach Fitting Access Figure 2 ...

Page 1210: ...PAGE 4 Feb 28 07 6I2 55 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1211: ...ating plate d Connect the elevator trim actuating rods to the actuator clevis e Check elevator trim and elevator operation refer to 27 30 00 C Balancing See Figure 1 To balance the elevator the assembly must be complete including the trim tab without the tab pushrods elevator tips and all attaching screws Before balancing tape the trim tab in its neutral position with a small piece of tape Ensure ...

Page 1212: ... the neutral position NOTE Because paint is a considerable balance factor it is recommended that existing paint be removed prior to repainting a control surface 2 Place hinge bolts through control surfaces and place control surface on a holding fixture 3 Calibrate the tool a Avoiding rivets place the balancing tool on the control surface with the tool s hinge centerline directly over the hinge lin...

Page 1213: ...PAGE 3 Feb 28 07 6I5 55 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Control Surfaces Balancing Tool Figure 2 ...

Page 1214: ...corrosion and condition Repair replace as required When inspection and repair replacement is completed reapply Dinitrol AV 8 P N 89500 800 Corrosion Inhibiting Compound NOTE For all fittings inspection of the exposed portion is sufficient unless obvious or extensive corrosion is apparent NOTE Any part exhibiting flaking of the metal due to rust must be replaced The elevator trim tab actuator push ...

Page 1215: ...PAGE 5 Feb 28 07 6I7 55 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Elevator Trim Tab Rods Figure 3 ...

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Page 1218: ...PAGE 8 Feb 28 07 6I10 55 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1219: ... corrosion and condition Repair replace as required When inspection and repair replacement is completed reapply Dinitrol AV 8 P N 89500 800 Corrosion Inhibiting Compound NOTE For all fittings inspection of the exposed portion is sufficient unless obvious or extensive corrosion is apparent NOTE Any part exhibiting flaking of the metal due to rust must be replaced NOTE If aluminum skin or structure ...

Page 1220: ...rtical Stabilizer Attach Fittings Figure 1 E Ensure entire attach fitting is treated Spray inside where the fitting is attached to the structure F Apply to approximately 8 mils in thickness Avoid puddling and running Allow to dry 1 to 1 1 2 hours before airplane use Full drying takes 6 to 8 hours ...

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Page 1222: ...PAGE 4 Feb 28 07 6I14 55 30 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1223: ...ue tube Torque the three 3 nuts as specified in Figure 1 55 00 00 5 Attach the rudder cables to the sector if the cables were previously removed 6 Set tension on cables per 27 20 00 7 Check rigging and operation of rudder control system per 27 20 00 8 Install the aft fuselage access panel C Balancing See Figure 1 To balance the rudder the assembly must be complete Place the complete assembly horiz...

Page 1224: ...PAGE 2 Feb 28 07 6I16 55 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Balancing Rudder Figure 1 ...

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Page 1226: ...PAGE 4 Feb 28 07 6I18 55 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1227: ...6I19 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 56 WINDOWS ...

Page 1228: ...6I20 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1229: ... Contents 1 Feb 28 07 2 Feb 28 07 56 00 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 56 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 56 20 00 1 Feb 28 07 2 Feb 28 07 56 30 00 1 Feb 28 07 ...

Page 1230: ...PAGE 2 Feb 28 07 56 LIST OF EFFECTIVE PAGES 6I22 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1231: ...crylic Window Cabin Inspection 7 6J7 Crack Inspection Acrylic Windows and Windshields 8 6J8 Window Windshield Repair Rework Procedure 10 6J10 Water Leak Check 12 6J12 FLIGHT COMPARTMENT 56 10 00 1 6J15 Windshield 1 6J15 Removal 1 6J15 Installation 1 6J15 Pilot s Copilot s Window 4 6J18 Removal 4 6J18 Installation 4 6J18 Storm Window S N s 4636001 thru 4636076 only 6 6J20 Removal 6 6J20 Installatio...

Page 1232: ...PAGE 2 Feb 28 07 6I24 56 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1233: ...ration extending through the entire thickness of the transparent material Craze Fissure on the surface of the transparent material that does not penetrate the full thickness of the material Crazing Mesh of fine hairline cracks that do not penetrate the full thickness of the material located on the surface or within the structure of the transparent material Star Craze A condition where several fiss...

Page 1234: ... FLIGHT PROHIBITED WITH CRACKED OR CRAZED WINDSHIELD The pilot s windshield is a two ply laminated glass containing a heating element 1 Critical Area Inspection The area of the laminated glass windshield used for taxiing takeoff climb cruise and landing a Cracks can occur in either the inner outer or both glass plies Cracking in either ply is critical and cause for immediate replacement b Blemishe...

Page 1235: ... area of the heated glass windshield used for general flight vision a Blemishes 1 Blemishes in windshields form in the vinyl plastic interlayer bonding the two glass plies together 2 Blemishes in the critical or semi critical portion of the windshield are not acceptable unless 0 062 inch 1 575 mm or smaller in circumference including distorted area 3 No more than two blemishes at least 12 inches 3...

Page 1236: ...1 5 inches 3 81 cm above the windshield retainer strip 2 Distortion may not be so severe that it restricts vision or diverts runway lines or section lines more than 45 3 Slight horizontal distortion is acceptable if there are no more than two lines they do not occupy more than 25 percent of the windshield area and they are separated by a minimum of six inches 15 24 cm B Acrylic Windshield Co Pilot...

Page 1237: ... replacement at the earliest opportunity 4 Crazing in any portion of the windshield requires replacement b Haze or foggy appearance is not acceptable if the amount of haze fog causes an obstruction of vision in the area used for operation of the aircraft c Scratches 1 Scratches in acrylic windshields may be reworked per Window Windshield Repair Rework below if a They are less than 0 030 inch 0 762...

Page 1238: ...s per Crack Inspection Acrylic Windows and Windshields below b Crazing 1 Crazing in the windows is critical 2 Determine depth of craze using a calibrated depth gauge or scale see Figure 1 3 A craze 0 050 inch 1 270 mm deep is cause for immediate replacement A craze 0 025 inch 0 635 mm deep is cause for replacement at the earliest opportunity 4 Crazing in any portion of a window requires replacemen...

Page 1239: ...than 1 5 inches 3 81 cm above the windshield retrainer strip 2 Distortion may not be so severe that it restricts vision or diverts runway lines or section lines more than 45 3 Slight horizontal distortion is acceptable if there are no more than two lines they do not occupy more than 25 percent of the windshield area and they are separated by a minimum of six inches 15 24 cm D Acrylic Window Cabin ...

Page 1240: ...rosion and structural defects 3 Inspect bolt holes in windows and co pilot s windshield as follows using Window Inspection Kit P N 766 294 A 45 acrylic prism and glycerin may be used if kit not available a Clean area to be inspected with soap and water to ensure surface is free of oil dirt and wax b Determine which immersion oil to use Type A in cold weather Type B in hot weather c Apply a small a...

Page 1241: ...PAGE 9 Feb 28 07 6J9 56 00 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Visual Inspection Figure 2 ...

Page 1242: ...nnot be reworked in accordance with these standards F Window Windshield Repair Rework Procedure Acrylic Windows Co Pilot s Windshield Only The following methods should be used for repairs CAUTION ANY ACRYLIC WINDOW WHICH MAY HAVE BEEN DAMAGED BY PAINT THINNER PAINT REMOVER OR OTHER SOFTENING AGENT MUST BE REPLACED NO REPAIR IS PERMITTED FOR THIS TYPE OF DAMAGE CAUTION DAMAGE LIMITS AND REPAIRS STA...

Page 1243: ...o longer apparent Thoroughly flush the area with water e Using 600A wet or dry abrasive paper repeat step c Continue sanding only until the hairline scratches caused by the coarse sanding are no longer apparent Sand a larger area than that covered by the original sanding operation Thoroughly wash the area f Finish the repair using instructions given in paragraph 1 above ...

Page 1244: ...e tap full open 2 The check shall be conducted with an observer inside the aircraft 3 All cabin and baggage compartment doors and other controllable external closures shall be closed and latched during rainfall simulation 4 The spray shall be aimed directly at the openings around windows for a period of one half to one and one half minutes for each window The nozzle shall be held three to ten feet...

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Page 1246: ...PAGE 14 Feb 28 07 6J14 56 00 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1247: ...ainer a Check fit and trim to fit as required The areas most likely to require trimming are the lower left outboard side and along the bottom edge near the center post b Using the old retainer as a template drill 191 inch screw holes Countersink the screw holes 380 in dia x 100 degrees NOTE For the pilot s heated glass windshield apply a parting agent Polyvinyl Alcohol P N 915 936 or equivalent to...

Page 1248: ... INCH EDGE CLEARANCE BY SANDING PERPENDICULAR TO EDGE WITH MAX 220 GRIT IN AREA SHOWN ONLY REFINISH SANDED EDGE WITH FLAT BLACK ENAMEL PAINT SILICONE RUBBER TUBES WINDSHIELD SEE NOTE 1 SHIM SHIM RIGHT AND LEFT SIDE SILICONE RUBBER TUBE SEE NOTE 1 SHIM RIGHT AND LEFT SIDE SEE NOTE 1 SILCONE RUBBER TUBE WINDSHIELD SEE NOTE 1 SHIM RIGHT AND LEFT SIDE PILOTS WINDOW REF TYPICAL VIEW OF SILCONE RUBBER T...

Page 1249: ...NOTE 1 SHIM RIGHT AND LEFT SIDE SECTION A A STRAP TYPICAL VIEW OF TUBE IN WINDSHIELD REFER TO FIGURE 1 FOR DETAILS SILICONE RUBBER TUBE STRAP SEE NOTE 1 SEE NOTE 1 SILICONE RUBBER TUBE SECTION B B SILICONE RUBBER TUBE SEE NOTE 1 SECTION D D NOTES 1 APPLY SEALANT HERE SEE 91 10 00 CHART 10 SEALANT WINDOWS AND WINDSHIELDS 2 ALL FASTENERS WHICH PENETRATE THE WINDOW SHALL BE TORQUED TO 19 22 INCH POUN...

Page 1250: ...ted 350 hours time in service upon reaching 350 hours and each 50 hours time in service thereafter inspect as follows 1 Examine the exterior of the pilot s side cockpit window in the area between the storm window hinge and the fuselage skin 2 If sealant exists between the storm window hinge and the airframe skin remove the sealant in that area only very carefully with a plastic scraper ensuring th...

Page 1251: ...E 5 Feb 28 07 6J19 56 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Pilot s Side Cockpit Window Inspection Figure 3 HINGE FUSELAGE SKIN LOOKING INBOARD FROM LEFT S N S 4636077 AND UP ...

Page 1252: ...6076 only See Figure 4 A Removal 1 Rotate the latch to open the storm window 2 Remove the nuts washers bolts and screws that attach the storm window hinge to the pilot s window 3 Remove the pilot s window B Installation 1 Position the storm window in the hole in the pilot s window 2 Torque the fasteners that attach the storm window hinge to the window as specified in Figure 4 3 Rotate the latch to...

Page 1253: ...2 Bond the hinge half to the pilot s side window with Dexter Hysol 9446 see A A Figure 5 Take care to ensure the inside edge of the hinge half is bonded flush to the pilot s window Also ensure that a 030 inch gap is left between the bottom edge of the cut out and the inside of the hinge half and that the gap is filled with adhesive 3 When the hinge to window bond is cured slide the latch pin assem...

Page 1254: ...B B SECTION B B VIEW OUT FWD NOTES 1 BOND WITH DEXTER HYSOL 9446 2 BOND WITH PR 1422 3 IF STORM WINDOW FAILS WATER LEAK CHECK ADD UP TO 0 15 RTV 732 P N 279 195 BETWEEN SEAL AND WINDOW RETAINER AND PERFORM WATER LEAK CHECK AGAIN SECTION A A NOTE 1 NOTE 1 BEFORE BONDING REMOVE KNOB FROM STORM WINDOW ASSY AND CENTER LATCH PIN TO THE 5 IN DIAMETER HOLE IN THE STEEL RETAINER PIN MUST BE CENTERED WITHI...

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Page 1256: ...PAGE 10 Feb 28 07 6J24 56 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1257: ... of old sealant from the retainer inboard edge of the window opening and old window 2 All corners must be broken and all edges smooth and free of tool marks 3 If a new window is being installed ensure that it is the same dimensions as the old window 4 Apply PRC 1422 B4 sealant to the outboard surface of the window where it mates with the inboard edge of the window opening Also apply sealant to the...

Page 1258: ...PAGE 2 Feb 28 07 6K2 56 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1259: ... fasten the window retainer to the inner frame of the door 2 Remove the retainer 3 Remove the door window B Installation 1 Remove all remaining traces of a sealant from the inner surface of the door window frame and outboard facing side of the retainer 2 Fit check the new window before applying sealant 3 Apply PRC1422 B4 sealant to the inner surface of the frame and outboard facing side of the ret...

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Page 1261: ...6K5 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 57 WINGS ...

Page 1262: ...6K6 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1263: ... 28 07 57 Table of Contents 1 Feb 28 07 2 Feb 28 07 57 40 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 19 Feb 28 07 20 Feb 28 07 57 50 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 CHAPTER...

Page 1264: ...PAGE 2 Feb 28 07 57 LIST OF EFFECTIVE PAGES 6K8 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1265: ...eneral 1 6K11 Outboard Wing 1 6K11 Removal 1 6K11 Installation 5 6K15 HI LOK Removal and Installation 7 6K17 Inboard Wing 9 6K19 General 9 6K19 Removal 11 6K21 Installation 14 6K24 Attach Fittings Corrosion Control 17 6L3 FLIGHT SURFACES 57 50 00 1 6L7 Aileron 1 6L7 Removal 1 6L7 Installation 1 6L7 Balancing 2 6L8 Balancing Equipment 2 6L8 Wing Flaps 5 6L11 Removal 5 6L11 Installation 5 6L11 ...

Page 1266: ...PAGE 2 Feb 28 07 6K10 57 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1267: ...mplete Wing 766 675 See the PA 46 350P Illustrated Parts Catalog P N 761 878 for further details 2 Outboard Wing A Removal See Figures 1 and 2 1 Drain the fuel from both wings refer to Draining Fuel System 12 10 00 2 Remove the aileron per 57 50 00 If replacing the wing section remove the aileron sector 3 Remove the flap per 57 50 00 4 Carefully remove the wing splice skin W S 107 56 W S 115 25 th...

Page 1268: ...PAGE 2 Feb 28 07 6K12 57 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Wing Installation Figure 1 ...

Page 1269: ...PAGE 3 Feb 28 07 6K13 57 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Outboard Wing Installation Figure 2 Sheet 1 of 3 Effectivity 4636001 thru 4636195 ...

Page 1270: ... of 3 Effectivity 4636196 up SPLICE PLATE IS PART OF OUTBOARD WING ASSY A W S 107 50 SPLICE SKIN AREA REF W S 116 00 OUTBOARD A SPLICE ANGLE IS PART OF OUTBOARD WING ASSY 83000 U STRAP SPLICE ANGLES ARE PART OF OUTBOARD WING ASSY STRAP FWD SECTION A A LOOKING INBOARD HL18 6 4 22 PLACES B B HL18 8 7 2 PLACES HL18 6 6 20 PLACES SEE SHEET 3 ...

Page 1271: ... help maintain true alignment of the wing sections Also extend a string from the wing tip to the stabilizer marking its length and checking this with the opposite wing and stabilizer using the same reference points on both wings and stabilizers 3 While maintaining proper alignment of the wing install the Hi Lok pins and rivets into the spars and splice plates per Figure 3 Refer to the PA 46 350P I...

Page 1272: ... has a 015 025 radius while the 3 16 flush head HL 19 6 series has a 025 030 radius MIN MAX i e 5 16 i e 5 16 MAXIMUM THICKNESS MINIMUM THICKNESS P 572 1 EXAMPLE P 490 EXAMPLE MINIMUM GRIP MAXIMUM PROTRUSION MAXIMUM GRIP MINIMUM PROTRUSION 1 16 TYPE OF HI LOK PIN R HL18 5 SERIES 025 HL18 6 SERIES 015 HL18 8 SERIES HL18 10 SERIES 030 HL19 6 SERIES 020 HI LOK PROTRUSION GAUGE HI SHEAR P N 2 1522 MAY...

Page 1273: ...ok entry 3 HI LOK Removal and Installation NOTE Refer to Hi Shear Catalogs for further information and a complete list of power and hand tools to aid in removal and installation of the Hi Lok fasteners A Hi Lok pins and collars are used at various points in the wing installation Refer to the Piper Parts Catalog P N 761 878 for locations and proper pin and collar part numbers B To remove the Hi Lok...

Page 1274: ...PAGE 8 Feb 28 07 6K18 57 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Special Equipment for Wing Removal and Installation Figure 4 ...

Page 1275: ...ting the procedure see Figure 4 a Cradle to support fuselage Create slings from industrial nylon lifting strap six 6 inches wide Lifting capability needed only if raising fuselage away from wing b Dolly to cradle wing A single jack may be specially adapted for this procedure in order to lower wing away from fuselage c Hoist assembly To be attached to ceiling with sufficient weight bearing capacity...

Page 1276: ...PAGE 10 Feb 28 07 6K20 57 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Removal and Installation of Inboard Wing Figure 5 Sheet 2 of 2 ...

Page 1277: ...e NOTE Perform steps 7 and 8 outside airplane 7 Remove wing to fuselage fairings left and right wing roots Remove bottom fuselage skin panels at wing spar left center and right Remove tee channels and angles below spar 8 Disconnect remove lines as follows Figure 5 Detail A a Disconnect flap drive Remove rods left and right see Figure 2 20 00 00 b Pull aileron cables through wing root and secure ca...

Page 1278: ...lly should already be in place under wing NOTE Perform step 14 both inside and outside airplane 14 Retract landing gear and remove hydraulic lines as follows a Using hydraulic pressure release gear down locks b Retract and tie back main landing gear c Drain off hydraulic pressure d Remove hydraulic lines from wing root and below spar Figure 5 NOTE The following final steps may require additional m...

Page 1279: ...PAGE 13 Feb 28 07 6K23 57 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Hole and Slot Fillets Figure 6 ...

Page 1280: ...in both wing spar and fuselage 9 Apply sealant to top spar and angles each side Use R4 sealant 10 Attach angles to top spar each side with cherry rivets Two 6 11 two 6 9 two 6 10 and two 6 11 CAUTION PROPER SEALING IS CRITICAL TO MAINTAIN PRESSURIZATION OF COCKPIT BE GENEROUS WITH SEALANT PARTICULARLY IN CORNERS WITH WIDE GAPS USE B4 SEALANT 11 Apply sealant to wing spar aft forward left and right...

Page 1281: ...es one on each side of stringer 26 Below fuselage place short tee angles between floor angles and rivet together with four 4 rivets on top Then go inside and rivet both ends to bottom stringer 27 Ensure there are no metal splinters on chips between skins prior to installing close outs 28 Apply sealant to all skins and close out skins on bottom of aircraft See Figure 6 Apply sealant 1 4 inch each s...

Page 1282: ...igure 5 Detail A NOTE Reinstall electrical fuel and hydraulic lines first Then reinstall control cables a Outside airplane 1 Install hydraulic lines in wing root and below spar 2 Connect electrical cannon plugs left and right 3 Install fuel lines in wing root area 4 Pull aileron cables through wing root and secure cables refer to 27 00 00 5 Connect flap drive Reinstall rods left and right see Figu...

Page 1283: ... A When inspection and repair or replacement are completed allow sufficient time for primer to dry and apply Dinitrol AV 8 to 1 Forward wing spar attach fittings 2 Aft wing spar attach fittings NOTE Includes wing and fuselage fittings CAUTION READ PRECAUTIONS ON CONTAINER LABEL AND WEAR A CHARCOAL FILTER MASK WHEN APPLYING DINITROL AV 8 B Apply Dinitrol by spraying or brush Use an air or airless s...

Page 1284: ...PAGE 18 Feb 28 07 6L4 57 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Wing Attach Fittings Corrosion Control Figure 8 ...

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Page 1286: ...PAGE 20 Feb 28 07 6L6 57 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1287: ...t the aileron and remove the two aileron hinge bolts 3 Remove the aileron B Installation WARNING ALL CONTROL SURFACES THAT HAVE BEEN REPLACED OR REPAINTED MUST BE BALANCED BEFORE INSTALLATION PER INSTRUCTIONS IN BALANCING BELOW 1 Position the aileron on the trailing edge of the wing 2 Install the attaching nuts bolts and washers 3 Attach the aileron drive sector to the yoke in the aileron with the...

Page 1288: ...rface should be painted and trim servo tabs should be in the neutral position NOTE Because paint is a considerable balance factor it is recommended that existing paint be removed prior to repainting a control surface B Place hinge bolts through control surfaces and place control surface on a holding fixture C Calibrate the tool 1 Avoiding rivets place the balancing tool on the control surface with...

Page 1289: ...7 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHART 1 AILERON STATIC BALANCE LIMITS PIR PPS50060 Rev I Leading Edge Heavy Trailing Edge Heavy Inch Pounds Inch Pounds 0 5 2 Balancing Aileron Figure 2 ...

Page 1290: ...PAGE 4 Feb 28 07 6L10 57 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Control Surfaces Balancing Tool Figure 3 ...

Page 1291: ...ull the flap straight back off the wing B Installation 1 Position the flap on the trailing edge of the wing 2 Ensure that spacers are in place in the flap tracks 3 Insert bolts washers and nuts Torque the nuts from 38 43 inch pounds and safety with cotter pins Install the teflon faced washers on the center tracks so that the teflon side faces the flap track 4 Connect the two flap drive push rods t...

Page 1292: ...PAGE 6 Feb 28 07 6L12 57 50 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL GRIDS 6L12 THRU 6L24 INTENTIONALLY BLANK ...

Page 1293: ...PART NUMBER 761 876 February 28 2007 7A1 AIRPLANE MAINTENANCE MANUAL CARD 7 OF 9 PA 46 350P S N s 4636001 AND UP PIPER AIRCRAFT INC ...

Page 1294: ...7A2 Published by Technical Publications Piper Aircraft Inc 2926 Piper Drive Vero Beach Florida 32960 U S A Member General Aviation Manufacturers Association ...

Page 1295: ...2 3 4 5 and 6 CR981223 December 23 1998 1 2 3 4 5 and 6 PR000201 February 1 2000 1 2 3 4 5 and 6 PR010515 May 15 2001 1 CR050730 July 30 2005 1 2 3 4 5 6 7 and 8 PR060207 February 7 2006 1 2 3 4 5 6 7 and 8 CR070228 February 28 2007 1 2 3 4 5 6 7 8 and 9 COMPLETE REVISION OF MAINTENANCE MANUAL 761 876 Revisions appear in all Aerofiche Cards Accordingly discard your entire existing Aerofiche Card S...

Page 1296: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 1 Feb 28 07 AEROFICHE EFFECTIVITY 7A4 THIS PAGE INTENTIONALLY BLANK ...

Page 1297: ...Feb 28 07 Intro Table of Contents 1 Feb 28 07 2 Feb 28 07 Introduction 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 Index 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHA...

Page 1298: ...PAGE 2 Feb 28 07 INTRO LIST OF EFFECTIVE PAGES 7A6 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1299: ...A9 Effectivity 2 7A10 Serial Number Explanation 2 7A10 Assignment of Subject Material 2 7A10 Pagination 3 7A11 Aerofiche Effectivity 3 7A11 Identifying Revised Material 3 7A11 Indexing 3 7A11 List of Effective Pages 3 7A11 Warnings Cautions and Notes 3 7A11 Accident Incident Reporting 4 7A12 Supplementary Publications 4 7A12 Piper Publications 4 7A12 Vendor Publications 4 7A12 Chapter Section Inde...

Page 1300: ...PAGE 2 Feb 28 07 7A8 INTRO CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1301: ...GENUINE PIPER AIRCRAFT PARTS OR PIPER AIRCRAFT APPROVED PARTS OBTAINED FROM PIPER APPROVED SOURCES IN CONNECTION WITH THE MAINTENANCE AND REPAIR OF PIPER AIRPLANES Genuine PIPER parts are produced and inspected under rigorous procedures to ensure airworthiness and suitability for use in PIPER airplane applications Parts purchased from sources other than PIPER even though identical in appearance ma...

Page 1302: ...ane are broken down into subsystems These sub systems are identified by the second element of the standard numbering system The element 40 of the number 28 40 01 concerns itself with the indicating section of the fuel system C Unit Subject The individual units within a sub system section may be identified by the third element of the standard numbering system The element 01 of the number 28 40 01 i...

Page 1303: ...his set 8 Identifying Revised Material A revision to a page is defined as any change to the printed matter that existed previously Revisions additions and deletions are identified by a vertical line i e change bar along the left hand margin of the page opposite only that portion of the printed matter that was changed A change bar in the left hand margin opposite the footer i e chapter section subj...

Page 1304: ...s Catalog P N 761 878 2 Periodic Inspection Report Form P N 767 011 3 Progressive Inspection Manual 50 hour P N 767 013 B Vendor Publications WARNING FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION S WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT MAY RENDER THE AIRCRAFT UNAIRWORTHY 1 AIR CONDITIONING COMPRESSOR Vendor Address Sanden International USA Inc PH 972 442 8400...

Page 1305: ...cialty Systems PH 330 374 3040 Goodrich Corporation FAX 330 374 2290 1555 Corporate Woods Parkway Uniontown Ohio 44685 8799 Technical Assistance PH 800 334 2377 330 374 3743 FAX 330 374 2290 Email dssd support goodrich com http www deicingsystems goodrich com Black Standard Pneumatic De Icer Installation Maintenance and Repair Manual ATA 30 10 31 SmartBoot System ATA 30 10 65 8 ELECTRONIC FLIGHT I...

Page 1306: ...ntext See www avantext com or PH 800 998 8857 11 FIRE EXTINGUISHER PORTABLE Vendor Address H3R Inc PH 800 249 4289 43 Magnolia Ave 4 San Francisco California 94123 2911 http www h3r com index htm 12 FORCE APPLICATOR KIT Vendor Address Safe Flight Instrument Corp PH 914 946 9500 20 New King Street White Plains New York 10602 13 FUEL BOOST PUMP Vendor Address Parker Hannifin Corp PH 800 272 7537 Nic...

Page 1307: ...ww unisonindustries com index4 html Installation Operation F1100 MASTER SERVICE MANUAL and Maintenance 4300 6300 SERIES MAGNETO MAINTENANCE AND Instructions OVERHAUL MANUAL L 1363 19 NAVIGATION COMMUNICATIONS AND GPS NAV COM GPS Vendor Address Garmin International PH 913 397 8200 1200 East 151ST Street Olathe KS 66062 http www garmin com 20 OXYGEN SYSTEM Vendor Address Scott Aviation PH 716 683 51...

Page 1308: ...DAR WEATHER RDR 2000 Vendor Address Honeywell Bendix King See Autoflight above Maintenance Manual Bendix King ART 2000 P N 006 05332 0001 25 RADIO COOLING BLOWER Vendor Address Globe Motors PH 937 228 3171 2275 Stanley Ave FAX 937 229 8531 Dayton Ohio 45404 http www globe motors com home html 26 STARTER Vendor Address Kelly Aerospace See Alternator above or Sky Tec Partners Ltd PH 800 476 7896 350...

Page 1309: ...MALIBU MIRAGE MAINTENANCE MANUAL 28 VACUUM PUMP Vendor Address Aero Accessories Inc PH 800 822 3200 1240 Springwood Avenue Gibsonville NC 27249 http www aeroaccessories com index html 29 VACUUM REGULATORS Vendor Address Parker Hannifin Corp see Fuel Boost Pump above ...

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Page 1311: ...chapter CHAPTER SECTION TITLE GRID NO 4 AIRWORTHINESS LIMITATIONS 1C1 00 Airworthiness Limitations 5 TIME LIMITS MAINTENANCE CHECKS 1C9 00 General 10 Time Limits 20 Scheduled Maintenance Checks 30 Special Inspections 50 Unscheduled Maintenance Checks 6 DIMENSIONS AND AREAS 1E13 00 General 7 LIFTING AND SHORING 1F1 10 Jacking 8 LEVELING AND WEIGHING 1F9 10 Weighing and Balancing 20 Leveling 9 TOWIN...

Page 1312: ...emperature Control 22 AUTOFLIGHT 2F11 10 Autopilot 23 COMMUNICATIONS 2G19 00 General 50 Audio Integrating 60 Static Discharging 24 ELECTRICAL POWER 2H11 00 General 30 DC Generation 40 External Power 60 Electrical Load Distribution 25 EQUIPMENT FURNISHINGS 2J11 10 Flight Compartment 20 Passenger Compartment 50 Cargo Compartments 60 Emergency 26 FIRE PROTECTION 2K15 20 Extinguishing 27 FLIGHT CONTRO...

Page 1313: ...rs 60 Propellers Rotors 31 INDICATING RECORDING SYSTEMS 4C1 50 Central Warning Systems 32 LANDING GEAR 4C13 00 General 10 Main Gear and Doors 20 Nose Gear and Doors 30 Extension and Retraction 40 Wheels and Brakes 50 Steering 60 Position and Warning 33 LIGHTS 4G5 10 Flight Compartment 20 Passenger Compartment 30 Cargo and Service Compartments 40 Exterior 34 NAVIGATION 5C1 00 General 10 Flight Envi...

Page 1314: ...00 General 10 Investigation Cleanup and Aerodynamic Smoothness 70 Repairs 80 Electrical Bonding 52 DOORS 6G13 10 Passenger Crew 20 Emergency Exit 30 Cargo 70 Monitoring and Operation 55 STABILIZERS 6H13 00 General 10 Horizontal Stabilizers 20 Elevator 30 Vertical Stabilizer 40 Rudder 56 WINDOWS 6I19 00 General 10 Flight Compartment 20 Cabin 30 Door 57 WINGS 6K5 40 Attach Fittings 50 Flight Surface...

Page 1315: ... Power Supply 20 Distribution 76 ENGINE CONTROLS 7G17 10 Power Control 77 ENGINE INDICATING 7H3 10 Power 20 Temperature 40 Integrated Engine Instrument Systems 79 OIL 7J3 20 Distribution 30 Indicating 80 STARTING 7J15 10 Cranking 81 TURBINES 7K9 20 Turbo Supercharger 91 CHARTS WIRING DIAGRAMS 8C1 10 Charts 21 and up Electrical Schematics 91 CONT CHARTS WIRING DIAGRAMS CONT 9C1 Electrical Schematic...

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Page 1317: ...sion Control Wing 6L3 Attitude Indicator 5D5 Autopilot 2F17 Component Locator 2G2 Installation 2F18 2F20 Maintenance 2F23 Operational Checkout 2F24 Pitch Servo 2G12 Pressure Transducer 2G6 Roll Servo 2G4 Servo Clutch Torque Adjustment 2G15 Trim Monitor 2G3 Trim Servo 2G6 Yaw Amplifier 2G14 Yaw Servo 2G10 Avionics Cooling 2C14 Avionics Master Switch 2H1 B Ball Diameters for Testing Hose Restriction...

Page 1318: ...rrection 2I10 Troubleshooting 2I7 2I13 Valve Regulated Lead Acid 2I13 Bonding 6G9 Resistance Index 6G10 Buses Avionics 2H19 Main 2H19 Circuit Breaker Panel 6D22 Electrical Shelf 6E7 External Power 2I19 Load Distribution 2J1 Relay Installation Co Pilot s Side 6E10 K1 thru K8 6E10 Pilot s Side 6E9 Schematics Air Conditioning 8E7 Airspeed Standby 9E19 Altimeter Radar 9F14 Altimeter Standby 9E19 Annun...

Page 1319: ...n Light 9E5 WX 500 9F11 XM Receiver 8E23 Switch Panels 6E1 Symbols 8D14 System 2H17 Troubleshooting 2H20 Tie Bus Panel Connections 6E3 Volt Ammeter 2J4 Voltage Regulation and Control 2H19 Wire Coding 8D13 Elevator Balancing 6I3 Control System Installation 3D23 Rigging and Adjustment 3D24 Troubleshooting 3D19 Torque Tube Bearing Changes 3D20 Trim Controls Actuator Assembly 3E3 Corrosion Control 3E4...

Page 1320: ...Drain Valve 3G8 Draining 1I19 Draining Moisture 1I18 Fuel Filter 3G7 Fuel Pumps Specifications 3G5 Fuel Quantity Gauge Accuracy Test 3G14 Full Range Check 3G20 Senders 3G13 Leak Test Setup 3G1 Selector Switch and Valve 3G6 Cable Adjustment 3G7 Troubleshooting 3F16 Leak Evaluation 3F22 G GMA 340 Audio Panel Adjustments 2H6 Installation 2H3 System Functional Test 2H4 GNS 430 5F5 GNS 530 5F5 Ground C...

Page 1321: ... 4D11 Position and Warning 4F19 Landing Gear Up Power Reduced Warning Switch Adjustment 4G2 Troubleshooting 4F20 Leading Particulars and Principal Dimensions 1E20 Leveling 1F17 Life Limited Parts 1C7 Lifting 1F7 See also 57 40 00 Lights Exterior 4H3 Landing 4H7 Position 4H4 Pulse 4H7 Strobe 4H3 Taxi 4H6 Wing Inspection Light 4H7 Interior 4G11 Annunciator Panel 4G12 Baggage Area 4G21 Forward 4H1 Re...

Page 1322: ...g 3K6 Troubleshooting 3J20 Propeller Assembly 7C9 Publications Piper A12 Vendor A12 Q Quad Digital Indicator QDI See Engine Instruments Transicoil EMIS R Radar 5F1 Repairs Fiberglass 6F19 Metal Wire Stitching 6G5 Thermoplastic 6F21 List of Materials 6F24 Window Windshield Acrylic 6J10 Restraint System 2J23 Inertial Reel Adjustment 2J23 Inspection 2J23 Revised Material A11 Robinair 34700 Charging S...

Page 1323: ... Bellcrank Centering 4C22 Horn Arm Gap 4C22 Nose Wheel Centering 3C15 4C22 Rudder Pedal Neutral Alignment 3C15 4C22 Rudder Travel Tool 3C15 Torque Conversion 8C20 Torque Wrench Formula 1K2 Towing 1G5 Transponder 5F9 GTX 327 5F9 GTX 330 5F9 Post Installation Setup Procedure 5F10 ARINC 429 Configuration Page 5F11 Display Mode and Key Lighting 5F11 Hexadecimal Conversion 5F13 Operation Configuration ...

Page 1324: ...in 6I11 Vertical Speed Indicator 5C18 Volt Ammeter See Electrical W Warnings Cautions and Notes A11 Weather Radar 5F1 Weighing 1F15 Wheel Brake Assembly 4F4 Wheels Bearing Cup 4F4 Main Wheel Assembly 4F2 Nose Wheel Assembly 4F1 Repairs 4F3 Windows and Windshields Door Window 6K3 Heated Windshield Testing 3J15 Troubleshooting 3J15 Inspection and Repair Definitions 6J1 Limitations 6J1 Crack Limitati...

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Page 1327: ...7C1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 61 PROPELLER ...

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Page 1329: ...ES CHAPTER SECTION PAGE DATE CHAPTER SECTION PAGE DATE 61 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 61 Table of Contents 1 Feb 28 07 2 Feb 28 07 61 00 00 1 Feb 28 07 2 Feb 28 07 61 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 61 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 ...

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Page 1331: ...1 7C7 Description 1 7C7 PROPELLER ASSEMBLY 61 10 00 1 7C9 Propeller 1 7C9 Removal 1 7C9 Installation 1 7C9 Blade Track 3 7C11 Cleaning Inspection and Repair 3 7C11 Propeller Blade Inspection and Repair 3 7C11 All Metal Blades 3 7C11 Kevlar Composite Blades 3 7C11 CONTROLLING 61 20 00 1 7C17 Propeller Governor 1 7C17 Removal 1 7C17 Installation 2 7C18 Rigging and Adjustment 2 7C18 ...

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Page 1333: ...ded Kevlar composite constant speed propeller is available as an option Both blade models have an 80 inch diameter In all installations the propeller is controlled by an engine mounted Hartzell V 5 2 governor which supplies oil through the propeller shaft Oil pressure increases the blade pitch reduces rpm and blade centrifugal forces reduces the blade pitch increase rpm When propeller heat is inst...

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Page 1335: ...s from around the spinner assembly and remove the spinner 6 Place a drip pan under the propeller to catch oil spillage 7 Remove the six propeller mounting bolts and remove propeller B Installation 1 Ensure master and magneto switches are off 2 Move fuel selector to off position 3 Place mixture control in idle cut off 4 Observe the starter ring gear to make sure it is mounted properly on the engine...

Page 1336: ... 7 Install propeller with blades aligned with mounting bolt hole marked O 8 If not installed already install rear spinner bulkhead using four 4 or six 6 hub clamping bolts two and three blade installations respectively Torque 20 to 24 FT LBS 9 Slide propeller carefully over pilot taking care that O ring is not damaged 10 Install the six propeller mounting bolts and torque 60 to 70 FT LBS 11 Check ...

Page 1337: ...pect the hub parts for cracks 4 Steel hub parts should not be permitted to rust Use aluminum paint to touch up if necessary or replate during overhaul 5 Check all visible parts for wear and safety 6 Check the blades to determine whether they turn freely on the hub pivot tube This can be done by rocking the blades back and forth through the slight freedom allowed by the pitch change mechanism If th...

Page 1338: ...l erosion shield is more likely to have problems than the blade therefore a more thorough coin tapping of the erosion shield is desirable Also slight deformations in the erosion shield may be noticed by careful visual and manual touch inspection Such deformations may be the result of a debond and should be given a careful coin tap inspection e If a suspected delamination or debond is discovered a ...

Page 1339: ...FOR SPECIFIC DAMAGE LIMITS AND APPROVED REPAIR PROCEDURES THE FOLLOWING INFORMATION IS ADVISORY ONLY Procedures for the following minor repairs are provided in latest revision Hartzell Manual No 135 Maintenance Manual for Composite Propeller Blades a Nickel Erosion Shield Debond extending to trailing edge or crack Gouge Missing area of trail side or inboard end b Blade Cuff Cracks at the root end ...

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Page 1343: ...crankcase Remove the governor as follows 1 Remove the upper cowl and left side of the nose cowl to gain access to the governor 2 Disconnect the governor control cable end from the governor control arm 3 Remove the governor mounting nuts and withdraw the governor with control bracket from the mounting pad Cover the mounting pad to prevent foreign material from entering the engine Propeller Governor...

Page 1344: ...takeoff must be conducted during which the engine rpm should reach 2 460 2 500 rpm and remain steady 3 If the engine rpm does not read 2 460 2 500 rpm in flight the high rpm setting must be adjusted as follows a Land and shut down the engine b Adjust the governor by means of the fine adjustment screw for 2 460 2 500 rpm To do this loosen the high rpm fine adjustment screw locknut and turn the scre...

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Page 1347: ...7C21 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 70 STANDARD PRACTICES ENGINE ...

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Page 1349: ... INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 70 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 70 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 70 Table of Contents 1 Feb 28 07 2 Feb 28 07 70 00 00 1 Feb 28 07 2 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 1351: ...b 28 07 7D1 70 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 70 STANDARD PRACTICES ENGINE TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO GENERAL 70 00 00 1 7D3 Procedures 1 7D3 ...

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Page 1353: ...stopped immediately and the item removed even if considerable time and labor is required E Ensure all parts are thoroughly clean before assembling especially during engine build up F Never reuse any lockwire lock washers tablocks tab washers or cotter pins G All lockwire and cotter pins must fit snugly in holes drilled in specific hardware On castellated nuts the cotter pin head must fit into a re...

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Page 1355: ...7D5 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 71 POWER PLANT ...

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Page 1357: ... 71 Table of Contents 1 Feb 28 07 2 Feb 28 07 71 00 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 71 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 71 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 71 70 00 1 Feb 28 07 2 Feb 28 07 C...

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Page 1359: ...Troubleshooting 1 7D11 Engine 7 7D17 Removal 7 7D17 Installation 8 7D18 COWLING 71 10 00 1 7E1 Engine Cowling 1 7E1 Removal 1 7E1 Installation 1 7E1 Cleaning Inspection and Repair 1 7E1 MOUNTS 71 20 00 1 7E5 Engine Mount 1 7E5 Inspection 1 7E5 100 Hour 1 7E5 Corrosion Inspection Immersion in Water 3 7E7 Installation 4 7E8 Engine Shock Mounts Replacement 4 7E8 DRAINS 71 70 00 1 7E11 Cylinder Head D...

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Page 1361: ...ared starter and dual pneumatic vacuum pumps Engine mounts are steel tubing construction attached at the firewall and incorporate vibration absorbing dynafocal mounts From the exhaust stacks gases are directed to individual turbocharger exhaust plenums through or around the turbo turbine as required and overboard at bottom rear of the engine cowling on each side The lubrication system is of the pr...

Page 1362: ...h of its range Defective spark plugs Clean and adjust or replace spark plugs Defective ignition wire Check with electric tester and replace any defective wires Defective battery Replace with charged battery Improper operation of Clean points Check magneto breaker internal timing of magnetos Lack of sufficient fuel Disconnect fuel line at fuel flow injector and check fuel flow Water in fuel injecto...

Page 1363: ...e kick back during cranking electrically connected in due to advance timing of circuit due to a poor ignition connection Inspect retard points to see if they close Check for proper contact at the Switch and Retard leads at magneto and at the vibrator Check wiring Vibrator magneto Turn engine in proper combination not putting direction of rotation until out electrically retard points just open No 1...

Page 1364: ...ion system Check entire ignition system Insufficient fuel pressure Adjust fuel pressure Leak in air bleed nozzle Check connection and balance line replace if necessary Plugged fuel injector nozzle Clean or replace nozzle Flow divider fitting plugged Clean fitting Low power and uneven Mixture too rich as indicated Readjustment of fuel running by sluggish engine injector by authorized operation red ...

Page 1365: ...ottle lever adjustment Improper fuel flow Check strainer gauge and flow at fuel injector inlet Restriction in air scoop Examine air scoop and remove restrictions Improper fuel Drain and refill tank with recommended fuel Plugged fuel injector nozzle Clean or replace nozzle Propeller out of rig Adjust propeller Faulty ignition Tighten all connections Check system with tester Check ignition timing Ro...

Page 1366: ... Dirty oil strainers Remove and clean oil strainers High oil temperature See High Oil Temperature in Trouble column below Defective pressure gauge Replace gauge Stoppage in oil pump Check line for obstruction intake passage Clean suction strainer High oil temperature Insufficient air cooling Check air inlet and outlet for deformation or obstruction Insufficient oil supply Fill oil sump to proper l...

Page 1367: ...F THE AIRPLANE BEFORE REMOVING THE ENGINE NOTE All hoses lines and wires should be tagged identified to facilitate installation Open fuel oil and vacuum lines and fittings should be covered to prevent contamination 1 Turn off all electrical switches in the cockpit and then disconnect the battery ground wire at the battery 2 Move the fuel selector lever in the cockpit to OFF 3 Remove the engine cow...

Page 1368: ... engine after the engine was removed from the aircraft Remove any protective caps and identification tags as each item is installed 1 Attach a one half ton minimum hoist to the engine and swing the engine into alignment with its attaching points NOTE Refer to Figure 1 for the arrangement of the shock mount assemblies The top shock mounts are assembled so the silver shocks are aft and the gold shoc...

Page 1369: ... heat muff 23 Connect the propeller governor control cable to the governor Secure the control cable with the clamps 24 Connect the starter positive and ground leads to the starter Secure the leads with the clamps 25 Connect the air conditioning compressor lines if the air conditioning is installed 26 Ensure that any other lines hoses or electrical leads that were disconnected during removal of the...

Page 1370: ...PAGE 10 Feb 28 07 7D20 71 00 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Engine Installation Figure 1 Sheet 1 of 2 ...

Page 1371: ...PAGE 11 Feb 28 07 7D21 71 00 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Engine Installation Figure 1 Sheet 2 of 2 ...

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Page 1375: ...ove the five upper and two lower screws attaching the right half of the nose cowl to the left half c Remove nose bowl cowl B Installation 1 Place the nose cowl halves around the propeller drive shaft and secure them to each other and to the induction air panel assembly with MS24695 S50 screws 2 Position both halves of the lower cowling in place and secure them to the nose cowl and firewall flange ...

Page 1376: ... 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Engine Cowling Figure 1 UPPER COWLING NOSE COWL HALVES QUICK DISCONNECT FASTENERS ENGINE OIL DIPSTICK ACCESS LOWER COWLING MS24694 S50 SCREWS MS24694 S49 SCREWS ...

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Page 1379: ... c Inspect the welded area of the nose gear actuator attach feet see Figure 1 Sheet 2 for cracks 1 First inspect visually If no cracks are detected using that method then 2 Perform a liquid penetrant inspection per latest revision of AC 43 13 1 d If cracking is detected in either of the actuator attach feet the entire engine mount assembly must be replaced before further flight e If no cracks are ...

Page 1380: ...PAGE 2 Feb 28 07 7E6 71 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL 100 Hour Engine Mount Inspection Figure 1 Sheet 2 of 2 ...

Page 1381: ...Using a syringe inserted into the end of the plastic tube pump linseed oil into the upper end of the engine mount tube while rotating the syringe plastic tube assembly to assure maximum coverage Continue pumping until the lower end of the engine mount tube is filled with linseed oil to the level of the inspection hole 4 Now draw the plastic tube out of the upper end of the engine mount tube and re...

Page 1382: ...cedure described in this paragraph is with the engine installed A Remove the engine cowling B Attach a one half ton minimum hoist to the engine hoisting hooks and relieve tension from the shock mounts C Loosen the upper shock mount attachment nuts D Remove the lower mount attachment nuts washers forward shock mounts and spacers E Remove the lower attachment bolts just far enough to allow the aft s...

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Page 1385: ... intake plenum The drain valve is connected to the cylinder head drain lines which come from both banks of cylinders A drain tube goes from the drain valve through the lower cowling The drain valve is closed by manifold pressure when the engine is running When the engine is shut down the lack of manifold pressure allows the drain valve to open thus draining any excess fuel from the cylinder heads ...

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Page 1387: ...7E13 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 73 ENGINE FUEL CONTROL ...

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Page 1389: ...PTER 73 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 73 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 73 Table of Contents 1 Feb 28 07 2 Feb 28 07 73 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 73 30 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 1391: ...1 7E19 Lubrication 1 7E19 Fuel Injector 1 7E19 Removal 1 7E19 Installation 3 7E21 Storage Preparation 3 7E21 Fuel Air Bleed Nozzle 3 7E21 Removal 3 7E21 Installation 4 7E22 Cleaning and Inspection 4 7E22 INDICATING 73 30 00 1 7F1 Fuel Flow Gauge 1 7F1 Troubleshooting 1 7F1 Removal 1 7F1 Installation 1 7F1 Fuel Pressure Low Warning Light 1 7F1 Fuel Pump 1 7F1 Adjustment 1 7F1 Pressure Operational C...

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Page 1393: ...uring periodic inspection of the engine a Check tightness and lock of all nuts and screws which fasten the injector to the engine b Check all fuel lines for tightness and evidence of leakage A slight fuel stain adjacent to the air bleed nozzles is not cause for concern c Check throttle and mixture control rods and levers for tightness and lock d Remove and clean the injector fuel inlet strainer at...

Page 1394: ...vented to Deck Pressure Fuel Nozzle Flow Divider Deck Turbochargers Engine Driven Fuel Pump Seal Drain Firewall Electric Emergency Fuel Pump Supply Line Fuel Selector Handle Fuel Selector Valve Metering Unit Right Tank Vent Line Drain Fuel Quantity Guage Finger Screens Fuel Lines Filler Cap Collector Tank To Intake Manifold Fuel Flow Transducer Filter and Drain ON Fuel Pressure Switch Differential...

Page 1395: ...edure CAUTION DO NOT EXCEED 15 PSI AIR PRESSURE AS INTERNAL DAMAGE TO THE INJECTOR MAY RESULT 1 Remove plugs and drain all fuel from the injector If available apply 10 15 psi air pressure to the fuel inlet until all fuel is discharged from the injector 2 Replace plugs and apply flushing oil filtered through a 10 micron filter at 13 15 psi to the injector fuel inlet until oil is discharged from the...

Page 1396: ...stall the spring and spring retainer on the nozzle stem 5 Connect the fuel line to the nozzle and clamp the fuel lines as described in latest revision of Lycoming Service Bulletin No 335 6 Install the engine cowl C Cleaning and Inspection 1 Clean the nozzle with acetone or equivalent and blow out all foreign particles Do not use wire or other hard objects to clean orifices Refer to the latest revi...

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Page 1399: ...ews securing the instrument to th e panel 4 Remove the instrument from the panel C Installation 1 Place the instrument in its proper panel cutout and secure with screws 2 Install the post light s and secure Do not overtighten the nut 3 Connect the electrical connector to the gauge 2 Fuel Pressure Low Warning Light Illumination of the FUEL PRESS annunciator light indicates impending fuel starvation...

Page 1400: ...essory case just below the left magneto A Removal 1 Disconnect electrical leads going to transducer 2 Disconnect B nut on transducer fuel outlet line 3 Remove the nuts washers and bolts securing transducer to mounting bracket 4 Remove transducer mounting bracket from engine 5 Disconnect transducer from fuel pump B Installation 1 Coat all pipe threads with PST 563 sealant Do not coat the orifice in...

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Page 1403: ...7F5 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 74 IGNITION ...

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Page 1405: ...ts 1 Feb 28 07 2 Feb 28 07 74 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 19 Feb 28 07 20 Feb 28 07 74 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28...

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Page 1407: ... Troubleshooting 1 7F11 Replacement Magnetos 1 7F11 Overhaul 1 7F11 Magnetos 1 7F11 100 Hour Inspection 1 7F11 Removal 4 7F14 500 Hour Inspection and Cleaning 4 7F14 Disassembly 6 7F16 Assembly 10 7F20 Testing 17 7G3 Installation 18 7G4 DISTRIBUTION 74 20 00 1 7G7 Harness 1 7G7 Inspection 1 7G7 Removal 1 7G7 Installation 1 7G7 Disassembly 1 7G7 Assembly 2 7G8 Spark Plugs 6 7G12 Removal 6 7G12 Inst...

Page 1408: ...PAGE 2 Feb 28 07 7F10 74 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1409: ...ting cycle B Troubleshooting See Chart 1 C Replacement Magnetos NOTE Check the magneto dataplate to verify the specific model number and series of the magneto being worked on D Overhaul Overhaul is required as conditions indicate but in no case may Slick 6300 series magnetos time in service exceed the TBO for the engine Magnetos must also be overhauled after a lightning strike or following a sudde...

Page 1410: ...eplace or or loose ground repair Defective vibrator Replace vibrator Failure of engine to idle Faulty ignition system Check entire ignition properly system Improper spark plug Check spark plug gap setting for altitude Low power and uneven Defective spark plugs Clean or replace sparkplug running engine Magneto not working Check timing of magneto properly Defective ignition wire Check wire with elec...

Page 1411: ... POSITION THE MAGNETOS WILL FIRE THE SPARK PLUGS IF THE PROPELLER IS ROTATED FATAL INJURY IS POSSIBLE d Turn ignition switch ON e Rotate the magneto in its mounting in the direction of normal operating rotation until the timing light indicates the contact breaker points are open f Slowly rotate the magneto opposite normal rotation of the magneto on the engine mounting until the timing light or aud...

Page 1412: ...MARY CIRCUIT OF THE ENGINE IS GROUNDED BEFORE WORKING ON THE ENGINE Before removing the magnetos make sure the magneto switches are OFF WARNING THE MAGNETO IS NOT INTERNALLY GROUNDED WHEN THE GROUND LEAD IS DISCONNECTED THE MAGNETO IS HOT REMOVING THE HARNESS ASSEMBLY FIRST AND INSTALLING THEM LAST MINIMIZES THE DANGER OF STARTING THE ENGINE ACCIDENTALLY WHEN THE GROUND LEAD IS REMOVED FROM THE MA...

Page 1413: ...spect the condenser for signs of corrosion Replace if required d Inspect the condenser P lead stud for twisting or pulled condition Replace if required e Test the electrical properties of the condenser using appropriate calibrated test equipment Test for capacitance value with condenser charged to 400 volts DC Service limit 35 microfarad 10 percent Test for resistance measured between condenser le...

Page 1414: ...nt gaskets as gasket contains a metal mesh to ensure proper ground between magneto frame and housing Inspect screw gaskets for wear Replace as required 13 Inspect harness cap O ring for wear Replace as required D Disassembly See Figures 3 and 4 NOTE Use of the Slick T 100 Assembly and Timing Kit Figure 3 is strongly recommended The tools contained in this kit will greatly facilitate magneto disass...

Page 1415: ...PAGE 7 Feb 28 07 7F17 74 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Slick T 100 Assembly and Timing Tool Kit Figure 3 ...

Page 1416: ...e primary contact points are secured by a BLACK anodized screw The retard breaker contact points are secured by a SILVER screw a Disconnect coil lead wire from primary contact breaker assembly b Remove cam by prying straight up with a screwdriver blade c Remove screws and washers from primary contact breaker assembly d Remove primary contact breaker assembly e Remove screws and washers from retard...

Page 1417: ... end down Using T 125 assembly fixture press rotor shaft removing bearing cap assembly b Reverse rotor shaft and insert T 121 bearing puller both halves between the drive end bearing and the rotor magnet head c Place rotor and T 121 on T 152 spacer CAUTION DO NOT ALLOW ROTOR TO COME INTO CONTACT WITH METAL CHIPS OR FILINGS ROTOR IS MAGNETIZED d Press rotor shaft and remove drive end bearing 10 Rem...

Page 1418: ...neto frame c Insert rotor and frame assembly plug T 102 into the T handle d Turn T handle until the bearing cap bottoms in the frame Place cap over end of rotorshaft first e Place T 151 cam and rotor set onto the end of the rotor shaft and turn T handle until the shaft bottoms in magneto frame f Install bearing clamps and the hold down screws g Torque screws to 20 24 in lbs 3 Install oil seal see ...

Page 1419: ...11 Feb 28 07 7F21 74 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Bearing Installation with T 125 Assembly Fixture Figure 6 Oil Seal Installation with T 125 Assembly Fixture Figure 7 ...

Page 1420: ...urate 1 Place the magneto on the T 125 assembly fixture flange down with the T 509 timing base adapter removed 2 Install the T 123 timing plug on the rotor shaft before placing the magneto on the T 125 assembly fixture 3 Looking directly down on the magneto align the magneto so that the coil is oriented in the 12 o clock position 4 Insert T 150 E Gap Gauge between the pole laminations in the rotor...

Page 1421: ...ker magnetos the primary points must be set first The retard i e secondary points are set in reference to the primary points and accordingly the primary points must be set correctly or the retard contact settings will not be accurate 1 Set primary points according to instructions above Do not remove T 150 E Gap Gauge and do not remove magneto frame from T 125 assembly fixture NOTE Retard points ar...

Page 1422: ...on the timing disk corresponding to the index mark on the T 125 base This represents a point of reference for primary point E gap See Figure 9 NOTE The actual number at the timing disk index mark is not critical This index mark will be used as a point of reference for setting the retard points a specified number of degrees from the primary points 6 Note the lag angle and direction of rotation from...

Page 1423: ...NELED SECURELY UNDER CONDENSER FAILURE TO DO SO MAY CAUSE THE LEAD WIRE TO INTERFERE WITH ROTOR GEAR MOVEMENT OR POINT OPERATION 10 Assemble the condenser into the distributor housing being sure to rotate the condenser wire the same rotation as the condenser is tightened in the housing For left magneto only ensure retard breaker contact lead is channeled underneath condenser 11 Distributor gear as...

Page 1424: ...utor gear in place with the T 118 timing pin through the appropriate hole in the block and gear Then a Place distributor block spacers on magneto frame b Place distributor block on magneto frame The distributor gear and rotor gear are properly meshed when the index mark on the rotor gear aligns with the index mark on the distributor block c Secure distributor block to frame with screws provided 19...

Page 1425: ...utput lead to a 5mm spark gap 3 Coming in Speed a Determine the lowest speed at which the magneto can be turned and still spark all 5mm gaps without missing b The test gap must fire consistently at 200 RPM on both magnetos 4 Pressure Testing After magneto reassembly install a pressurized harness cap and apply 15 psi filtered air to the inlet nozzle of the magneto see Figure 12 Air flow at 15 psi i...

Page 1426: ... thumb Rotate crankshaft until pressure is felt on thumb b Remove plug in front of number six cylinder Rotate crankshaft slowly to observe timing mark on alternator drive gear When the mark on the gear is centered in the viewing hole number one piston is at 20 BTC NOTE Verify correct engine timing for the airplane being worked on by checking the engine dataplate 6 Place a new gasket on magneto fla...

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Page 1429: ...ssembly mounted on the engine However should repair require replacement of more than one lead assembly or of a cable outlet plate the harness should be removed from the engine and sent to an overhaul shop B Removal 1 Disconnect the clamps that secures the wires to the engine and accessories 2 Loosen the coupling nuts at the spark plugs and remove the insulators from the spark plug barrel well Use ...

Page 1430: ...coiled conductor approximately 0 375 inch deep refer to Figure 4 7 On spark plug end of wire install M 1462 Nut followed by M 1459 Female Taper Hex Ferrule refer to Figure 5 8 After installation of nut and ferrule bend and rotate the silicone insulation as illustrated in Figure 6 to flare out the shielding so a drive ferrule can be inserted Take care not to cut the silicone insulation with the sha...

Page 1431: ... 28 07 7G9 74 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Stripping Tool Figure 1 Cutting Insulation Figure 3 Removing Silicone Rubber from Wire Figure 4 Inserting Stripping Tool Figure 2 ...

Page 1432: ...b 28 07 7G10 74 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Installation of Plug Endnut Figure 5 Installation of Ferrule Figure 7 Driving Tool Figure 8 Flaring Out the Shielding Figure 6 ...

Page 1433: ...74 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Installation in Housing Figure 9 Installation of Electrical Screw Figure 11 Installation of Insulator Screw Figure 12 Securing Wire in Housing Figure 10 ...

Page 1434: ...l insulator NOTE Do not use a torque wrench to remove spark plugs 2 Remove the spark plug from the engine In the course of engine operation carbon and other combustion products will be deposited on the end of the spark plug and will penetrate the lower threads to some degree As a result greater torque is frequently required for removing a plug than for installing it Accordingly the torque limitati...

Page 1435: ...ly insert the terminal insulator in the spark plug and tighten the coupling unit C Inspection and Cleaning 1 Visually inspect each spark plug for the following non repairable defects a Severely damaged shell or shield threads nicked up stripped or cross threaded b Badly battered or rounded shell hexagons c Out of round or damaged shielding barrel d Chipped cracked or broken ceramic insulator porti...

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Page 1439: ...7G17 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 76 ENGINE CONTROLS ...

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Page 1441: ...50P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER SECTION PAGE DATE 76 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 76 Table of Contents 1 Feb 28 07 2 Feb 28 07 76 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 CHAPTER SECTION PAGE DATE CHAPTER 76 LIST OF EFFECTIVE PAGES ...

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Page 1443: ...ANUAL CHAPTER 76 ENGINE CONTROLS TABLE OF CONTENTS SUBJECT CHAPTER PAGE GRID NO POWER CONTROL 76 10 00 1 7G23 Engine Setup Procedures 1 7G23 Idle Speed and Mixture Adjustment 1 7G23 Variable Pressure Controller 2 7G24 Controller Throttle Rigging 2 7G24 Adjustment for Manifold Pressure 2 7G24 ...

Page 1444: ...PAGE 2 Feb 28 07 7G22 76 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1445: ...s stabilized move the cockpit mixture control with a smooth steady pull toward the Idle Cut Off position and observe the tachometer for any change during the leaning process Caution must be exercised to return the mixture control to the Full Rich position before the rpm drops to a point of engine cut out An increase of more than 50 rpm while leaning out indicates an excessively rich idle mixture A...

Page 1446: ...ropeller control is at full rpm 2 500 rpm 3 Slowly advance the throttle lever to full throttle or 42 0 in Hg manifold pressure 4 If the throttle reaches full forward prior to the manifold pressure reaching 42 0 in Hg INCREASE manifold pressure by turning the controller adjustment bolt counterclockwise NOTE A general relationship between the number of turns on the controller adjustment and manifold...

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Page 1449: ...7H3 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 77 ENGINE INDICATING ...

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Page 1451: ...7 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 CHAPTER SECTION PAGE DATE 77 40 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 19 Feb 28 07 20...

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Page 1453: ...tion Analyzer Gauge 4 7H16 Description 4 7H16 Troubleshooting 4 7H16 Cylinder Head Temperature CHT Scanner 7 7H19 Description 7 7H19 Troubleshooting 7 7H19 CHT Indicator Calibration Check 8 7H20 Testing 8 7H20 Adjustment 8 7H20 Validation 10 7H22 Securing the System 10 7H22 INTEGRATED ENGINE INSTRUMENT SYSTEMS 77 40 00 1 7I1 Transicoil Electronic Module Instrument System EMIS 1 7I1 Dual Analog Mod...

Page 1454: ...GRID NO INTEGRATED ENGINE INSTRUMENT SYSTEMS cont 77 40 00 cont Fuel Load Entry Mode 12 7I12 Outside Air Temperature OAT 14 7I14 Fuel Imbalance Alarm 14 7I14 Automatic Exceedance Warning Mode 17 7I17 Exceedance Review Mode 17 7I17 Remote Exceedance Memory Reset Control 21 7I21 Servicing 21 7I21 Percent Power 23 7I23 Calibration 23 7I23 Avidyne FlightMax Entegra EFIS 25 7J1 ...

Page 1455: ... manifold of the engine is transmitted to the instrument through a line A pointer indicates the manifold pressure available at the engine in inches of mercury A manual drain is provided in the line The drain line leads from a tee on the back of the manifold air pressure gauge to the drain which is mounted forward of the elevator trim wheel on the left hand side B Troubleshooting See Chart 1 Troubl...

Page 1456: ...s The correct tolerance at 2 500 rpm is 25 rpm 0 rpm B Troubleshooting See Chart 2 CHART 2 TROUBLESHOOTING TACHOMETER INDICATOR Trouble Cause Remedy No reading on indicator Inoperative instrument Replace instrument either permanent or intermittent Loose cable connections Tighten cable Pointer oscillates Inoperative instrument Replace instrument excessively Excessive friction in Replace instrument ...

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Page 1459: ...g See Chart 1 C Gauge and Probe Cleaning and Inspection CAUTION DO NOT CONNECT OHMMETER ACROSS METER IT WILL BURN OUT THE MOVEMENT OF THE METER Unless mechanical damage is evident broken glass bent or broken pointer or broken case the following checks should be performed before removing the instrument 1 Remove the engine cowling as necessary to expose the exhaust transition 2 Loosen the nut which ...

Page 1460: ... should be replaced immediately 1 Remove the engine cowling as required to expose the exhaust transition 2 Remove the existing T I T probe mounted in a boss welded to the upper portion of the exhaust transition 3 Install a new T I T probe into the hole in the waste gate transition assembly and tighten 4 Run the aircraft and operationally check for a proper T I T reading 5 Re install the engine cow...

Page 1461: ... is permissible to construct the circuit shown in Figure 2 and connect this circuit to the aircraft battery as shown in Figure 3 4 Once this calibration configuration is established allow the aircraft to remain in the hanger for at least 3 hours for the system temperature to stabilize CAUTION DO NOT TOUCH THE CONTACTS ON THE BACK OF THE T I T INDICATOR WITH YOUR HANDS IF CONTACT IS MADE ALLOW THE ...

Page 1462: ...r verify that the pointer is at the lower edge of the red radial 1750 F if not replace indicator 8 Re install the glareshield 2 Combustion Analyzer Gauge S N s 4636001 thru 4636020 only A Description In S N s 4636001 thru 4636020 only a multi channel combustion analyzer is optional When installed it is located on the instrument panel The combustion analyzer measures the cylinder head temperature i...

Page 1463: ...PAGE 5 Feb 28 07 7H17 77 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL TIT System Calibration Set up Figure 3 ...

Page 1464: ...induction ice Decrease in EGT for Intake valve not opening Check valve lift one cylinder fully faulty valve lifter Scored cylinder or broken Check spark plugs Clean ring to cause low compression or replace if necessary EGT may increase due to Check compression plug fouling from oil consumption Slow rise in EGT Burned exhaust valve Check compression Decrease in peak and Detonation usually the Check...

Page 1465: ...onnecting this pin to ground before the heartbeat will step the scanner to Cylinder No 2 Now Cylinder No 2 will be displayed on the gauge for the heartbeat period Upon the next heartbeat the gauge will again display the hottest cylinder Continuing to momentarily connect this pin to ground before the heartbeat will step the scanner to the next cylinder in rotation 3 4 5 6 etc By maintaining a groun...

Page 1466: ...CHT scanner must be operating during these tests 6 If the CHT indicator meets the specified limits go to Securing the System below If the CHT indicator does not meet the specified limits proceed to Adjustment or Validation below depending on aircraft serial number B Adjustment P N 599 588 only original equipment in S N s 4636021 thru 4636131 only NOTE P N s 602 299 or 602 247 installed as original...

Page 1467: ...PAGE 9 Feb 28 07 7H21 77 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHT Test Box Construction and Lead Connection Figure 4 Effectivity 4636021 and up ...

Page 1468: ...dicator fails to meet the specified limits on 3 cylinder also replace CHT VAC dual analog module indicator 3 If CHT indicator meets the specified limits on 3 cylinder troubleshoot CHT probe and harness on 1 cylinder and repeat test in Testing above D Securing the System 1 Replace foil sticker over trim potentiometers if removed 2 Reinstall CHT VAC dual analog module indicator in instrument panel i...

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Page 1471: ...A rear connector is provided for system interface and analog sensor inputs Alarm outputs are provided where applicable 1 Features Each Dual Analog Module Indicator features the following See Figure 1 a Two parallax free dials each featuring Return to Zero pointers which hold just below 0 or the lowest graduation when power is removed b Four status indicator LEDs two green and two red with the exce...

Page 1472: ...DI as communication is established between it and the dual analog indicator The following test functions will occur a Both pointers will drive to the 9 o clock position b All indicator LEDs illuminate c External audible alarm s sound for the last two 2 seconds of self test 2 Normal Digital Display Characteristics Press the select button adjacent to the analog indicator that is to be displayed digi...

Page 1473: ...r yellow LED will remain on until the reading returns to the normal range Once the parameter in exceedance is acknowledged the exceeding indicator will return to its normal display operation 4 Retrieval of Exceedances Characteristics The QDI EDI stores data concerning an exceedance event which can be retrieved at any time While the QDI EDI is displaying this data both LEDs will flash on the analog...

Page 1474: ...st lines graduation point Faulty sensor Change sensor Oil pressure analog instrument Faulty connection between Check aircraft wire goes into exceedance when RPM module connector pin harness RPM instrument is below 1400 5 and VAC module connector RPM pin 4 Faulty internal circuit in either Return RPM and OP RPM or OP module s instrument modules to the factory VAC analog instrument goes into Faulty ...

Page 1475: ...icator reading The EDI top line is dedicated to engine manifold pressure and RPM the middle displays selected analog indicators and the lower displays OAT and PWR Electrical interface is provided by a single 25 pin male D subminiature connector The QDI EDI contains EMI and RFI protection An independent signal conditioning circuit is provided for Outside Air Temperature OAT 1 Functions include a Au...

Page 1476: ...PAGE 6 Feb 28 07 7I6 77 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Transicoil Electronic Module Instrument System EMIS Figure 2 ...

Page 1477: ... analog module The Green Arc 100 245 F oil temperature may also be displayed in digital form on the QDI EDI Yellow Arc None display by pushing the function switch adjacent to the analog dial Red Radial 245 F Oil Pressure Indicator Range 0 120 PSI Housed in the dual oil pressure oil temperature analog module The Green Arc 55 95 PSI oil temperature may also be displayed in digital form on the QDI ED...

Page 1478: ...viously been recorded must be called up manually by the operator c Upon reaching the 9 o clock self test pointer position any analog indicator s can be taken out of self test by depressing and then releasing the select switch associated with the analog indicator s you wish to see The selected indicator s will display current sensor readings The rest of the system stack will complete the self test ...

Page 1479: ...PAGE 9 Feb 28 07 7I9 77 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Quad Digital Indicator Overview Figure 3 Effectivity 4636021 thru 4636131 ...

Page 1480: ...In the event no fuel flow is detected the flight time remaining will be displayed as See Figure 7B When the calculated flight time remaining has expired 0 0 will be displayed See Figure 7C 4 To view the fuel consumed momentarily press the FUEL button a third time The fuel consumed will be displayed in gallons See Figure 8A As long as fuel flow is detected the fuel computer will continue to update ...

Page 1481: ...PAGE 11 Feb 28 07 7I11 77 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Digital Enhancement Mode i e Normal Display Figure 4 ...

Page 1482: ...ning if no change is made 2 Max Fuel Load While in the fuel entry mode press and release the E button with FILL adjacent to it The LCD will display FUEL 120 and return to the fuel management mode See Figure 5C b EDI S N s 4636132 thru 4636374 1 Prior to engine start a new fuel loading can be entered into the EDI by selecting the fuel posting mode Press the S button on the left side of the display ...

Page 1483: ...PAGE 13 Feb 28 07 7I13 77 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Fuel Modes Figure 5 ...

Page 1484: ...he INST mode See Figure 4 2 When in INST mode the OAT display can be cycled from F to C by pressing the SET button 10 Fuel Imbalance Alarm If a fuel imbalance greater than 10 gallons is sensed between the left and right fuel tanks the alarm output for an external annunciator will be activated after 60 seconds As soon as the imbalance is corrected the alarm will deactivate 11 Automatic Exceedance W...

Page 1485: ...PAGE 15 Feb 28 07 7I15 77 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Flight Time Remaining QDI Figure 7 Effectivity 4636021 thru 4636131 ...

Page 1486: ...PAGE 16 Feb 28 07 7I16 77 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Fuel Used Figure 8 ...

Page 1487: ...Average and Time duration of exceedance The exceedance history is presented in reverse chronological order for each indicator during review with the most recent exceedance event listed first CAUTION WHEN THE MEMORY ALLOCATED FOR EXCEEDANCE RECORDING IS FULL NO NEW EXCEEDANCES WILL BE RECORDED IT WILL BE NECESSARY FOR THE OPERATOR TO HAVE A QUALIFIED MECHANIC PERIODICALLY RESET THIS MEMORY THIS MEM...

Page 1488: ...a The push button functions used to review the limitation exceedance events in the exceedance review mode PEAK DISPLAY Figure 10 are Down Arrow This button will cause the EDI display to post all the exceedance events for the indicator under examination Each time the down arrow button is pressed the posted data will change to the next peak exceedance for the same indicator N Next This button allows...

Page 1489: ...PAGE 19 Feb 28 07 7I19 77 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Exceedance Review Figure 9 ...

Page 1490: ...indicator is illustrated in Figure 10 An analog indicator with an exceedance displayed is identified by both the red or yellow and green LEDs flashing The operation of the analog indicator is not affected during exceedance review 2 The peak value of the exceedance will be displayed digitally above the analog indicator under review 3 The opposite display window will contain an E and two numbers The...

Page 1491: ...D The QDI EDI is configured to accept a remote exceedance memory reset control See Remote Switch Controls External Alarm External Interface Overview above Upon receipt of the control signal the QDI EDI will reset clear its NVRAM exceedance memory This control can be initiated at any time 14 Servicing The Quad Digital Indicator Enhanced Digital Indicator cannot be serviced in the field Should any o...

Page 1492: ...PAGE 22 Feb 28 07 7I22 77 40 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Exceedance Review Analog Indicator Figure 12 ...

Page 1493: ...the display The power range is that which can be selected is from 45 to 80 in 5 increments b As power is changed a suggested approximate value for manifold pressure and fuel flow will be displayed If a different RPM is desired the select button can be depressed to toggle the active parameter to the RPM display and the up down arrow buttons can be used to vary the RPM in 100 RPM increments This var...

Page 1494: ...DICATOR SHALL MEET THE CRITERIA SPECIFIED BELOW WITH ITS APPLICABLE SENDER UNIT TEST POINT C 40 20 0 20 55 MAXIMUM OHMS 85 07 93 00 100 84 108 63 122 16 MINIMUM OHMS 83 47 91 32 99 16 106 95 120 48 TEST POINT IN HG ABS 10 20 30 42 45 MAXIMUM VDC 1 814 2 599 3 385 4 328 4 564 MINIMUM VDC 1 759 2 544 3 330 4 273 4 509 TEST POINT RPM 500 1400 2000 2500 2700 MAXIMUM HZ 13 05 35 55 50 55 63 05 68 05 MI...

Page 1495: ...ses the raw sensor input and provides a refined data stream to the PFD and MFD which actually display the data See 28 40 00 and 91 77 40 for more information WARNING FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION S WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT MAY RENDER THE AIRCRAFT UNAIRWORTHY SEE INTRODUCTION SUPPLEMENTARY PUBLICATIONS Line maintenance of this syst...

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Page 1497: ...7J3 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 79 OIL ...

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Page 1499: ... MAINTENANCE MANUAL CHAPTER 79 LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 79 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 79 Table of Contents 1 Feb 28 07 2 Feb 28 07 79 20 00 1 Feb 28 07 2 Feb 28 07 79 30 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 CHAPTER SECTION PAGE DATE ...

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Page 1501: ...ANUAL CHAPTER 79 OIL TABLE OF CONTENTS SUBJECT SECTION PAGE GRID NO DISTRIBUTION 79 20 00 1 7J9 Oil System 1 7J9 INDICATING 79 30 00 1 7J11 Engine Oil Pressure Gauge 1 7J11 Description 1 7J11 Troubleshooting 1 7J11 Engine Oil Temperature Gauge 2 7J12 Description 2 7J12 Troubleshooting 2 7J12 ...

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Page 1503: ... the engine driven gear type oil pump Outlet oil is directed to a full flow replaceable element oil filter A bypass valve is incorporated in the filter The oil pump has an oil pressure relief valve in the housing A second gear driven pump located below the starter scavenges oil from the turbochargers Engine oil is cooled by ram air passing through the oil cooler on the rear of the engine Oil is di...

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Page 1505: ...ATING NOTE In S N s 4636375 and up oil temperature and pressure data is collected by the Data Acquisition Unit DAU and is displayed on the Multi Function Display MFD and Primary Flight Display PFD See Electronic Flight Instrument System 34 20 00 and 91 77 40 for more information 1 Engine Oil Pressure Gauge A Description NOTE Serial numbers 4636021 thru 4636374 incorporate the Transicoil Electronic...

Page 1506: ...emperature indication of the engine oil in degrees Fahrenheit The instrument has a temperature bulb heat sensitive probe located between the magnetos B Troubleshooting See Chart 2 Trouble Cause Remedy Instrument fails to show Broken or damaged bulb Check engine unit and any reading Wiring open wiring to instrument Excessive scale error Improper calibration Repair or replace adjustment Pointer fail...

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Page 1509: ...7J15 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 80 STARTING ...

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Page 1511: ...IST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 80 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 80 Table of Contents 1 Feb 28 07 2 Feb 28 07 80 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 CHAPTER SECTION PAGE DATE ...

Page 1512: ...PAGE 2 Feb 28 07 80 LIST OF EFFECTIVE PAGES 7J18 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1513: ...Cranking Limitations 1 7J21 Kelly Aerospace Starter 1 7J21 Description 1 7J21 Troubleshooting 1 7J21 Removal 1 7J21 Installation 2 7J22 Cranking Tests 5 7K1 Sky Tec Starter 6 7K2 Description 6 7K2 Troubleshooting 6 7K2 Installation as a Service Replacement 8 7K4 Removal 9 7K5 Installation 9 7K5 Shear Pin Replacement 10 7K6 Starter Control Circuit 11 7K7 Starting with External Power 11 7K7 ...

Page 1514: ...PAGE 2 Feb 28 07 7J20 80 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1515: ...ction gear the Bendix drive pinon meshes with the starter drive gear by inertia and action of the spiral grooves within the Bendix unit A detent pin engages in a notch in the screw threads which prevents demeshing if the engine fails to start When the engine does start and reaches a predetermined speed centrifugal action forces the detent pin to release and allows the pinion to demesh from the sta...

Page 1516: ...faces and mounting hardware All ground points or straps must be clean and tight 2 Place starting motor in position with no stresses or binding forces being present and install three 3 each flat washers internal tooth star lock washers and mounting nuts and one 1 each flat washer internal tooth star lock washer and mounting bolt Torque bolt and nuts to 204 in lbs or as specified in Lycoming SSP 177...

Page 1517: ...should be wiped clean with a gasoline undoped moistened cloth A new brush should be run in until at least 50 seated however if facilities are not available for running in brushes then the brush should be properly seated by inserting a strip of No 0000 sandpaper between the brush and commutator with the sanded side next to the brush CAUTION DO NOT USE COARSE SANDPAPER OR EMERY CLOTH Pull sandpaper ...

Page 1518: ...peed lubricated motor or starter inspect and relubricate replacing ball bearings if worn See electrical causes See remedies listed for listed under Stater fails Stater fails to operate to operate above above Excessive arcing of starter Binding worn or improperly See information above brushes seated brush or brushes dealing with this trouble with excessive side play Dirty rough pitted or Clean as o...

Page 1519: ...th a hydrometer to make sure it is fully charged and filled to the proper level A load test should be made on the battery to verify proper condition before proceeding 2 Check all starter circuit wiring making sure all connections including battery terminals are clean and tight and that all insulation is sound and complete 3 A voltage loss test should be made to locate any high resistance connectio...

Page 1520: ...y Tec 149 NL high performance starters have significant differences from the earlier starters made by Kelly Aerospace Electrosystems and Prestolite The Sky Tec starters use a more modern more reliable bendix free design No periodic maintenance is required The recommended TBO is 2700 hours Engine cranking speed may be up to twice as fast as with previous starters The light weight of these starters ...

Page 1521: ...hen cold suspect battery When hot suspect cables terms sols Record voltage at the starter while cranking the starter in its failure mode Record voltages between each and every cable terminal and across solenoids while cranking the starter in its failure mode Record voltages between battery ground and starter ground while cranking the starter in its failure mode Pretest Considerations If possible v...

Page 1522: ...he Magneto system thoroughly Make sure that the magnetos are in compliance with all service bulletins Make sure that the magneto impulse coupling is within service specifications Kickbacks will shear a drive pin Check the impulse couplers prior to attempting even a single start 3 Inspect the voltage supply system If the Sky Tec starter fails to turn the engine significantly faster than the OEM sta...

Page 1523: ...ces and mounting hardware All ground points or straps must be clean and tight 2 Place starting motor in position with no stresses or binding forces being present and install three 3 each flat washers internal tooth star lock washers and mounting nuts and one 1 each flat washer internal tooth star lock washer and mounting bolt Torque bolt and nuts to 100 in lbs CAUTION TAKE CARE NOT TO OVER TORQUE ...

Page 1524: ...ear does not rotate and neither does the flywheel engine and propeller then the shear pin has done its job and must be replaced 1 Remove starter from airplane per Removal above 2 Lift the insulating boot on the motor lead and remove the M8 locking nut with a 12mm wrench and remove the motor lead wire from the stud 3 Remove the two M5 x 25MM hex screws and locking tab washers holding the motor adap...

Page 1525: ...ood ground connection B Check the voltage loss across the switch contacts during normal starting If loss is in excess of 0 2 volts per 100 amperes the solenoid should be replaced C If solenoid fails to operate when the manual starting switch is turned on or if it fails to release when the manual starting switch is released it should be removed and tested to specifications if available If either op...

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Page 1527: ...7K9 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 81 TURBINES ...

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Page 1529: ... CHAPTER SECTION PAGE DATE 81 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 81 Table of Contents 1 Feb 28 07 2 Feb 28 07 81 20 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHAPTER SECTION PAGE DATE CHAPTER 81 LIST OF EFFECTIVE PAGES ...

Page 1530: ...PAGE 2 Feb 28 07 81 LIST OF EFFECTIVE PAGES 7K12 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1531: ...CT CHAPTER PAGE GRID NO TURBO SUPERCHARGER 81 20 00 1 7K15 Turbocharger System 1 7K15 Description 1 7K15 Troubleshooting 1 7K15 Turbocharger Pre Lubrication 1 7K15 Inspections 6 7K20 Turbocharger and Exhaust System Visual Inspection 6 7K20 Intercooler Attachment Clips Inspection Replacement 7 7K21 V Band Coupling 100 Hour Inspection 8 7K22 ...

Page 1532: ...PAGE 2 Feb 28 07 7K14 81 CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1533: ...es to each cylinder Metered fuel is injected into the cylinder head upstream of the intake valve After combustion in the cylinder exhaust gases flow into the exhaust manifold to the turbocharger turbines where exhaust energy is extracted to drive the turbines which in turn drives or turns the compressor B Troubleshooting See Chart 1 2 Turbocharger Pre Lubrication Following engine oil and filter ch...

Page 1534: ...impeller or turbine Excessive dirt build up Thoroughly clean in compressor compressor assembly Service air cleaner and check for leakage Leak in engine intake or Tighten loose connections exhaust or replace manifold gaskets as necessary Rotating assembly bearing Overhaul turbocharger seizure Restriction in return lines Remove and clean lines from actuator to exhaust bypass controller Exhaust bypas...

Page 1535: ...en Metering jet in Remove actuator and actuator plugged clean jet Actuator piston seal If there is oil leakage at failed and leaking actuator drain clean excessively cylinder and replace piston seal Exhaust bypass valve sticking Clean and free action Engine surges or smokes Air in oil lines or actuator Bleed system Controller metering valve stem Replace controller seal leaking oil into manifold Cl...

Page 1536: ...DIC MAINTENANCE PROCEDURES FOR THE ENGINE THE SCREENS MUST NOT BE LEFT IN PLACE AFTER THE INITIAL RUN IN PERIOD OPERATION OF THE TURBOCHARGERS WITH CLOGGED SCREENS WILL CAUSE TURBOCHARGER FAILURE DUE TO LACK OF LUBRICATION CAUTION MAKE ENTRY IN AIRPLANE LOGBOOK TO ENSURE THAT SCREENS ARE REMOVED AFTER THE INITIAL ENGINE RUN IN PERIOD HAS BEEN COMPLETED CAUTION TAG LINES WITH A SUITABLE TAG TO REMI...

Page 1537: ...PAGE 5 Feb 28 07 7K19 81 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Turbocharger System Diagram Figure 1 ...

Page 1538: ...ting components 3 Reconnect the air ducting to the compressor air inlet and tighten attaching parts securely 2 Check the air duct connections between the compressor and the engine intake manifold and between the intake manifold and engine Tighten any loose connections 3 Verify the engine air cleaner has been properly serviced see Induction Air Filter 12 10 00 4 Inspect the exhaust system for leaka...

Page 1539: ...he engine cowling 2 Remove and inspect the left and right intercooler clips for evidence of cracks or damage 3 Replace any damaged intercooler clips as required with the improved P N 89082 005 clips 4 Install four flange support shims P N 89082 010 one under each intercooler flange as shown in Figure 2 Ensure that the radius side of the shim faces the intercooler flange 5 Install intercooler clips...

Page 1540: ...gure 4 Effectivity 4636001 thru 4636194 only Lockwiring V Band Couplings Figure 5 C V Band Coupling 100 Hour Inspection See Figure 5 Each 100 hours inspect lockwiring on V band couplings for condition and security If lockwiring is found broken inspect T bolt for stretching cracking or any other damage Replace coupling as required ...

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Page 1542: ...PAGE 10 Feb 28 07 7K24 81 20 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL GRIDS 7K24 THRU 7L24 INTENTIONALLY BLANK ...

Page 1543: ...PART NUMBER 761 876 February 28 2007 8A1 AIRPLANE MAINTENANCE MANUAL CARD 8 OF 9 PA 46 350P S N s 4636001 AND UP PIPER AIRCRAFT INC ...

Page 1544: ...8A2 Published by Technical Publications Piper Aircraft Inc 2926 Piper Drive Vero Beach Florida 32960 U S A Member General Aviation Manufacturers Association ...

Page 1545: ...2 3 4 5 and 6 CR981223 December 23 1998 1 2 3 4 5 and 6 PR000201 February 1 2000 1 2 3 4 5 and 6 PR010515 May 15 2001 1 CR050730 July 30 2005 1 2 3 4 5 6 7 and 8 PR060207 February 7 2006 1 2 3 4 5 6 7 and 8 CR070228 February 28 2007 1 2 3 4 5 6 7 8 and 9 COMPLETE REVISION OF MAINTENANCE MANUAL 761 876 Revisions appear in all Aerofiche Cards Accordingly discard your entire existing Aerofiche Card S...

Page 1546: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 1 Feb 28 07 AEROFICHE EFFECTIVITY 8A4 THIS PAGE INTENTIONALLY BLANK ...

Page 1547: ...Feb 28 07 Intro Table of Contents 1 Feb 28 07 2 Feb 28 07 Introduction 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 Index 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHA...

Page 1548: ...PAGE 2 Feb 28 07 INTRO LIST OF EFFECTIVE PAGES 8A6 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1549: ...A9 Effectivity 2 8A10 Serial Number Explanation 2 8A10 Assignment of Subject Material 2 8A10 Pagination 3 8A11 Aerofiche Effectivity 3 8A11 Identifying Revised Material 3 8A11 Indexing 3 8A11 List of Effective Pages 3 8A11 Warnings Cautions and Notes 3 8A11 Accident Incident Reporting 4 8A12 Supplementary Publications 4 8A12 Piper Publications 4 8A12 Vendor Publications 4 8A12 Chapter Section Inde...

Page 1550: ...PAGE 2 Feb 28 07 8A8 INTRO CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1551: ...GENUINE PIPER AIRCRAFT PARTS OR PIPER AIRCRAFT APPROVED PARTS OBTAINED FROM PIPER APPROVED SOURCES IN CONNECTION WITH THE MAINTENANCE AND REPAIR OF PIPER AIRPLANES Genuine PIPER parts are produced and inspected under rigorous procedures to ensure airworthiness and suitability for use in PIPER airplane applications Parts purchased from sources other than PIPER even though identical in appearance ma...

Page 1552: ...ane are broken down into subsystems These sub systems are identified by the second element of the standard numbering system The element 40 of the number 28 40 01 concerns itself with the indicating section of the fuel system C Unit Subject The individual units within a sub system section may be identified by the third element of the standard numbering system The element 01 of the number 28 40 01 i...

Page 1553: ...his set 8 Identifying Revised Material A revision to a page is defined as any change to the printed matter that existed previously Revisions additions and deletions are identified by a vertical line i e change bar along the left hand margin of the page opposite only that portion of the printed matter that was changed A change bar in the left hand margin opposite the footer i e chapter section subj...

Page 1554: ...s Catalog P N 761 878 2 Periodic Inspection Report Form P N 767 011 3 Progressive Inspection Manual 50 hour P N 767 013 B Vendor Publications WARNING FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION S WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT MAY RENDER THE AIRCRAFT UNAIRWORTHY 1 AIR CONDITIONING COMPRESSOR Vendor Address Sanden International USA Inc PH 972 442 8400...

Page 1555: ...cialty Systems PH 330 374 3040 Goodrich Corporation FAX 330 374 2290 1555 Corporate Woods Parkway Uniontown Ohio 44685 8799 Technical Assistance PH 800 334 2377 330 374 3743 FAX 330 374 2290 Email dssd support goodrich com http www deicingsystems goodrich com Black Standard Pneumatic De Icer Installation Maintenance and Repair Manual ATA 30 10 31 SmartBoot System ATA 30 10 65 8 ELECTRONIC FLIGHT I...

Page 1556: ...ntext See www avantext com or PH 800 998 8857 11 FIRE EXTINGUISHER PORTABLE Vendor Address H3R Inc PH 800 249 4289 43 Magnolia Ave 4 San Francisco California 94123 2911 http www h3r com index htm 12 FORCE APPLICATOR KIT Vendor Address Safe Flight Instrument Corp PH 914 946 9500 20 New King Street White Plains New York 10602 13 FUEL BOOST PUMP Vendor Address Parker Hannifin Corp PH 800 272 7537 Nic...

Page 1557: ...ww unisonindustries com index4 html Installation Operation F1100 MASTER SERVICE MANUAL and Maintenance 4300 6300 SERIES MAGNETO MAINTENANCE AND Instructions OVERHAUL MANUAL L 1363 19 NAVIGATION COMMUNICATIONS AND GPS NAV COM GPS Vendor Address Garmin International PH 913 397 8200 1200 East 151ST Street Olathe KS 66062 http www garmin com 20 OXYGEN SYSTEM Vendor Address Scott Aviation PH 716 683 51...

Page 1558: ...DAR WEATHER RDR 2000 Vendor Address Honeywell Bendix King See Autoflight above Maintenance Manual Bendix King ART 2000 P N 006 05332 0001 25 RADIO COOLING BLOWER Vendor Address Globe Motors PH 937 228 3171 2275 Stanley Ave FAX 937 229 8531 Dayton Ohio 45404 http www globe motors com home html 26 STARTER Vendor Address Kelly Aerospace See Alternator above or Sky Tec Partners Ltd PH 800 476 7896 350...

Page 1559: ...MALIBU MIRAGE MAINTENANCE MANUAL 28 VACUUM PUMP Vendor Address Aero Accessories Inc PH 800 822 3200 1240 Springwood Avenue Gibsonville NC 27249 http www aeroaccessories com index html 29 VACUUM REGULATORS Vendor Address Parker Hannifin Corp see Fuel Boost Pump above ...

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Page 1561: ...chapter CHAPTER SECTION TITLE GRID NO 4 AIRWORTHINESS LIMITATIONS 1C1 00 Airworthiness Limitations 5 TIME LIMITS MAINTENANCE CHECKS 1C9 00 General 10 Time Limits 20 Scheduled Maintenance Checks 30 Special Inspections 50 Unscheduled Maintenance Checks 6 DIMENSIONS AND AREAS 1E13 00 General 7 LIFTING AND SHORING 1F1 10 Jacking 8 LEVELING AND WEIGHING 1F9 10 Weighing and Balancing 20 Leveling 9 TOWIN...

Page 1562: ...emperature Control 22 AUTOFLIGHT 2F11 10 Autopilot 23 COMMUNICATIONS 2G19 00 General 50 Audio Integrating 60 Static Discharging 24 ELECTRICAL POWER 2H11 00 General 30 DC Generation 40 External Power 60 Electrical Load Distribution 25 EQUIPMENT FURNISHINGS 2J11 10 Flight Compartment 20 Passenger Compartment 50 Cargo Compartments 60 Emergency 26 FIRE PROTECTION 2K15 20 Extinguishing 27 FLIGHT CONTRO...

Page 1563: ...rs 60 Propellers Rotors 31 INDICATING RECORDING SYSTEMS 4C1 50 Central Warning Systems 32 LANDING GEAR 4C13 00 General 10 Main Gear and Doors 20 Nose Gear and Doors 30 Extension and Retraction 40 Wheels and Brakes 50 Steering 60 Position and Warning 33 LIGHTS 4G5 10 Flight Compartment 20 Passenger Compartment 30 Cargo and Service Compartments 40 Exterior 34 NAVIGATION 5C1 00 General 10 Flight Envi...

Page 1564: ...S 6F1 00 General 10 Investigation Cleanup and Aerodynamic Smoothness 70 Repairs 80 Electrical Bonding 52 DOORS 6G13 10 Passenger Crew 20 Emergency Exit 30 Cargo 70 Monitoring and Operation 55 STABILIZERS 6H13 00 General 10 Horizontal Stabilizers 30 Vertical Stabilizer 40 Rudder 56 WINDOWS 6I19 00 General 10 Flight Compartment 20 Cabin 30 Door 57 WINGS 6K5 40 Attach Fittings 50 Flight Surfaces 61 P...

Page 1565: ... Power Supply 20 Distribution 76 ENGINE CONTROLS 7G17 10 Power Control 77 ENGINE INDICATING 7H3 10 Power 20 Temperature 40 Integrated Engine Instrument Systems 79 OIL 7J3 20 Distribution 30 Indicating 80 STARTING 7J15 10 Cranking 81 TURBINES 7K9 20 Turbo Supercharger 91 CHARTS WIRING DIAGRAMS 8C1 10 Charts 21 and up Electrical Schematics 91 CONT CHARTS WIRING DIAGRAMS CONT 9C1 Electrical Schematic...

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Page 1567: ...sion Control Wing 6L3 Attitude Indicator 5D5 Autopilot 2F17 Component Locator 2G2 Installation 2F18 2F20 Maintenance 2F23 Operational Checkout 2F24 Pitch Servo 2G12 Pressure Transducer 2G6 Roll Servo 2G4 Servo Clutch Torque Adjustment 2G15 Trim Monitor 2G3 Trim Servo 2G6 Yaw Amplifier 2G14 Yaw Servo 2G10 Avionics Cooling 2C14 Avionics Master Switch 2H1 B Ball Diameters for Testing Hose Restriction...

Page 1568: ...rrection 2I10 Troubleshooting 2I7 2I13 Valve Regulated Lead Acid 2I13 Bonding 6G9 Resistance Index 6G10 Buses Avionics 2H19 Main 2H19 Circuit Breaker Panel 6D22 Electrical Shelf 6E7 External Power 2I19 Load Distribution 2J1 Relay Installation Co Pilot s Side 6E10 K1 thru K8 6E10 Pilot s Side 6E9 Schematics Air Conditioning 8E7 Airspeed Standby 9E19 Altimeter Radar 9F14 Altimeter Standby 9E19 Annun...

Page 1569: ...n Light 9E5 WX 500 9F11 XM Receiver 8E23 Switch Panels 6E1 Symbols 8D14 System 2H17 Troubleshooting 2H20 Tie Bus Panel Connections 6E3 Volt Ammeter 2J4 Voltage Regulation and Control 2H19 Wire Coding 8D13 Elevator Balancing 6I3 Control System Installation 3D23 Rigging and Adjustment 3D24 Troubleshooting 3D19 Torque Tube Bearing Changes 3D20 Trim Controls Actuator Assembly 3E3 Corrosion Control 3E4...

Page 1570: ...Drain Valve 3G8 Draining 1I19 Draining Moisture 1I18 Fuel Filter 3G7 Fuel Pumps Specifications 3G5 Fuel Quantity Gauge Accuracy Test 3G14 Full Range Check 3G20 Senders 3G13 Leak Test Setup 3G1 Selector Switch and Valve 3G6 Cable Adjustment 3G7 Troubleshooting 3F16 Leak Evaluation 3F22 G GMA 340 Audio Panel Adjustments 2H6 Installation 2H3 System Functional Test 2H4 GNS 430 5F5 GNS 530 5F5 Ground C...

Page 1571: ... 4D11 Position and Warning 4F19 Landing Gear Up Power Reduced Warning Switch Adjustment 4G2 Troubleshooting 4F20 Leading Particulars and Principal Dimensions 1E20 Leveling 1F17 Life Limited Parts 1C7 Lifting 1F7 See also 57 40 00 Lights Exterior 4H3 Landing 4H7 Position 4H4 Pulse 4H7 Strobe 4H3 Taxi 4H6 Wing Inspection Light 4H7 Interior 4G11 Annunciator Panel 4G12 Baggage Area 4G21 Forward 4H1 Re...

Page 1572: ...g 3K6 Troubleshooting 3J20 Propeller Assembly 7C9 Publications Piper A12 Vendor A12 Q Quad Digital Indicator QDI See Engine Instruments Transicoil EMIS R Radar 5F1 Repairs Fiberglass 6F19 Metal Wire Stitching 6G5 Thermoplastic 6F21 List of Materials 6F24 Window Windshield Acrylic 6J10 Restraint System 2J23 Inertial Reel Adjustment 2J23 Inspection 2J23 Revised Material A11 Robinair 34700 Charging S...

Page 1573: ... Bellcrank Centering 4C22 Horn Arm Gap 4C22 Nose Wheel Centering 3C15 4C22 Rudder Pedal Neutral Alignment 3C15 4C22 Rudder Travel Tool 3C15 Torque Conversion 8C20 Torque Wrench Formula 1K2 Towing 1G5 Transponder 5F9 GTX 327 5F9 GTX 330 5F9 Post Installation Setup Procedure 5F10 ARINC 429 Configuration Page 5F11 Display Mode and Key Lighting 5F11 Hexadecimal Conversion 5F13 Operation Configuration ...

Page 1574: ...in 6I11 Vertical Speed Indicator 5C18 Volt Ammeter See Electrical W Warnings Cautions and Notes A11 Weather Radar 5F1 Weighing 1F15 Wheel Brake Assembly 4F4 Wheels Bearing Cup 4F4 Main Wheel Assembly 4F2 Nose Wheel Assembly 4F1 Repairs 4F3 Windows and Windshields Door Window 6K3 Heated Windshield Testing 3J15 Troubleshooting 3J15 Inspection and Repair Definitions 6J1 Limitations 6J1 Crack Limitati...

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Page 1577: ...8C1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 91 CHARTS WIRING DIAGRAMS ...

Page 1578: ...8C2 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1579: ...1 23 30 1 Feb 28 07 2 Feb 28 07 91 23 50 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 CHAPTER SECTION PAGE DATE 91 List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 91 Table of Contents 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 91 10 00 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 ...

Page 1580: ...eb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 91 27 30 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 91 27 50 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 91 27 60 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 91 28 20 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 91 28 40 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 91 29 1...

Page 1581: ...eb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 91 31 50 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 19 Feb 28 07 20 Feb 28 07 21 Feb 28 07 22 Feb 28 07 23 Feb 28 07 24 Feb 28 07 91 32 60 1 Feb 28 07 2 Feb 28 07 3 Feb 28 0...

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Page 1583: ...PAGE 5 Feb 28 07 8C7 91 LIST OF EFFECTIVE PAGES PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

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Page 1585: ...20 8H1 2840 8H5 2910 8H9 3010 8H13 3030 8I1 3040 8I7 3060 8I11 3130 8I17 3150 8J1 3260 8K1 3310 9C11 3320 9D11 3340 9D19 3420 9E16 3440 9F9 3450 9F17 3510 9G10 3720 9G14 5270 9G16 7330 9G18 ATA Code Grid No 7420 9G20 7710 9H2 7720 9H4 7740 9H14 7930 9I18 Subject Grid No Air Conditioning 8E7 Airspeed Standby 9E19 Altimeter Radar 9F14 Altimeter Standby 9E19 Annunciator 8J1 Attitude Indicator Standby...

Page 1586: ... GNS 430 9F2 9F17 Ground Blocks 8F20 Ground Clearance 8E17 GTX 330 9F3 9F22 Hour Meter 8I17 Hydraulic Pump 8H9 Subject Grid No Ice Detection System 8H18 Ice Light 9E5 IHAS Integrated Hazard Alert System 9F12 Instrument Panel Switch Lights 9C23 Junction Blocks 8F22 KMC 850 9F12 KMH 820 9F12 KN 63 9F24 KPA 900 9F10 KR 87 9G1 KRA 10A 9F14 Landing Gear Position and Warning 8K1 Landing Light 9E9 Lift C...

Page 1587: ...obe Lights 9D19 Summing Amp 8F4 9F12 9F14 Tachometer 9H2 9H19 9I13 Tail Light Optional 9D22 9E1 Taxi Lights 9E9 TIT Indicator 9H4 9I1 9I13 Turn Coordinator s 9E16 Vacuum Indicator 9I5 9I13 Vacuum Low Indicator 9G14 Vent Blowers 8E7 Vent Defogger 8E3 Weather Radar 9F9 Wing Inspection Light 9E5 WX 500 9F11 XM Receiver 8E23 NOTE Card 9 grid numbers above may be erroneous if Card 9 has been updated su...

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Page 1591: ...iodically to assure accuracy and recheck frequently B If the fastener screw or nut is listed in Chart 2 but the mating fastener is not listed tighten only to the low end of the torque range specified for the listed fastener In addition the following limitations shall apply 1 Fastener and nut threads shall be clean and dry free of lubricants If the subject chapter section requires the fastener and ...

Page 1592: ...the torque range When the nut is stationary and the fastener is torqued use the higher side of the torque range In this case ensure one 1 washer is installed under the head as follows a If the subject chapter section does not specify the use of a washer under the head install one 1 NAS1149 032 thick washer under the head If additional washers are required under nut to adjust for grip length variat...

Page 1593: ...this for all fasteners common to the gapped interface If no gap exists after accomplishing the above finish torquing to final torque If a gap remains consult your Piper Dealer s Service Advisor DSA for further assistance D After the final torque apply a slippage mark to the nut or bolt or screw head as applicable NOTE For more details on torquing refer to FAA AC 43 13 1 latest revision 2 Conversio...

Page 1594: ...4 160 190 95 110 200 250 120 150 75 110 45 70 7 16 20 450 500 270 300 520 630 300 400 180 280 110 170 1 2 20 480 690 290 410 770 950 450 550 280 410 160 260 9 16 18 800 1 000 480 600 1 100 1 300 650 800 380 580 230 360 5 8 18 1 100 1 300 660 780 1 250 1 550 750 950 550 670 270 420 3 4 16 2 300 2 500 1 300 1 500 2 650 3 200 1 600 1 900 950 1 250 560 880 7 8 14 2 500 3 000 1 500 1 800 3 550 4 350 2 ...

Page 1595: ...679 FINE THREAD SERIES INCLUDES FRICTION DRAG Nut Bolt Torque Limits Torque Limits Torque Limits Torque Limits Torque Limits Torque Limits Size In Lbs In Lbs In Lbs In Lbs In Lbs In Lbs Min Max Min Max Min Max Min Max Min Max Min Max 10 32 38 43 30 33 43 48 33 38 28 33 23 28 1 4 28 65 100 60 70 110 130 80 90 60 75 45 60 5 16 24 160 200 120 145 180 205 130 150 100 125 85 100 3 8 24 240 270 175 190 ...

Page 1596: ...1 25 3 456 27 5 3 802 30 4 148 32 5 4 493 35 4 839 37 5 5 185 40 5 530 42 5 5 876 45 6 222 47 5 6 567 50 6 913 52 5 7 258 55 7 604 57 5 7 950 60 8 295 62 5 8 641 65 8 987 67 5 9 332 70 9 678 72 5 10 024 75 10 369 77 5 10 715 80 11 060 82 5 11 406 85 11 752 87 5 12 097 90 12 443 92 5 12 789 95 13 134 97 5 13 480 100 13 826 105 14 517 110 15 208 FT LBS MKG 115 15 900 120 16 591 125 17 282 130 17 974...

Page 1597: ...PAGE 7 Feb 28 07 8C21 91 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHART 4 DECIMAL CONVERSIONS ...

Page 1598: ...37 78 280 536 0 17 8 0 32 0 143 33 290 554 0 12 22 10 50 0 148 89 300 572 0 6 67 20 68 0 154 44 310 590 0 1 11 30 86 0 160 00 320 608 0 4 44 40 104 0 165 56 330 626 0 10 00 50 122 0 171 11 340 644 0 15 56 60 140 0 176 67 350 662 0 21 11 70 158 0 182 22 360 680 0 26 67 80 176 0 187 78 370 698 0 32 22 90 194 0 193 33 380 716 0 27 78 100 212 0 198 89 390 734 0 43 33 110 230 0 204 44 400 752 0 38 89 1...

Page 1599: ...ERS GAL U S LIQ 231 0 CU IN 0 1337 CU FT 3 785 LITERS 0 8327 IMPERIAL GAL 128 FLUID OZ IN 2 540 CM 08333 FT JOULES 0 000948 BTU 0 7376 FT LB MULTIPLY BY TO OBTAIN KILOGRAMS 2 205 LB 35 27 OZ 1000 GRAMS LITERS 1000 CU CM 61 03 CU IN 0 03532 CU FT 0 2642 U S GAL 0 22 IMPERIAL GAL 1 057 QUARTS METERS 39 37 IN 3 281 FT 1000 MM METER KILOGRAM 7 233 FT LB 9 807 JOULES OUNCES AVDP 0 0625 LB AVDP 28 35 GR...

Page 1600: ...371 1 397 1 422 1 447 1 473 1 498 0 06 1 524 1 549 1 574 1 600 1 625 1 651 1 676 1 701 1 727 1 752 0 07 1 778 1 803 1 828 1 854 1 879 1 905 1 930 1 955 1 981 2 006 0 08 2 032 2 057 2 082 2 108 2 133 2 159 2 184 2 209 2 235 2 260 0 09 2 286 2 311 2 336 2 362 2 387 2 413 2 438 2 463 2 489 2 514 INCHES 0 00 0 01 0 02 0 03 0 04 0 05 0 06 0 07 0 08 0 09 MILLIMETER 0 0 0 254 0 508 0 762 0 016 1 270 1 52...

Page 1601: ... 0 037 0 9398 23 64 0 3593 9 1262 13 64 0 2031 5 1594 35 0 110 2 794 64 0 036 0 9144 T 0 358 9 1281 7 0 201 5 1054 7 64 0 1093 2 7781 65 0 035 0 899 S 0 346 8 7884 8 0 199 5 0546 36 0 1065 2 7051 66 0 033 0 8382 11 32 0 3437 8 7300 9 0 196 4 9784 37 0 104 2 6416 1 32 0 0312 0 7937 R 0 339 8 6106 10 0 1935 4 9149 38 0 1015 2 5781 67 0 032 0 8128 Q 0 332 8 4328 11 0 191 4 8514 39 0 0995 2 5273 68 0 ...

Page 1602: ...r and year hose manufacturer s identification Uses Hose is approved for use in aircraft hydraulic pneumatic coolant fuel and oil systems Operating Temperatures Sizes 3 thru 12 Minus 65 F to plus 250 F Sizes 16 thru 48 Minus 40 F to plus 275 F NOTE Maximum temperatures and pressures should not be used simultaneously TUBE HOSE HOSE RECOMMENDED MIN MAX MIN MIL SIZE SIZE SIZE OPER BURST PROOF BEND PAR...

Page 1603: ...o Anti Seize Compound TT A 580 Armite Product Armite Laboratories White Lead Base JAN A 669 Anti Seize Thread Fel Pro C5 A Fel Pro Incorporated Compound HIGH TEMPERATURE Buffing and Rubbing Automotive Type DuPont Company Compounds DuPont 7 Ram Chemical 69 Ram Chemicals Compound for Mirror Glaze Mirror Bright Polish Polishing Co Incorporated Plexiglas Polish P P 560 Part Number 403D Permatex Co Inc...

Page 1604: ... Company Braycote 627S Mobil Grease 27 Mobil Oil Corporation B P Aero Grease 31B B P Trading Limited Grease Aircraft MIL G 3278 Unitemp E P Texaco Incorporated Instrumentation Gear and Actuator RPM Aviation Grease Standard Oil of Calif Screw Temp Range 5 Supermil Grease 65 F to 250 F No 8723 Aeroshell Grease 7A Shell Oil Corporation Royco 78 Royal Lubricants Company L 1212 Sinclair Refining Co 191...

Page 1605: ...Company Alvania E P Grease 2 Aeroshell Grease 5 Grease 77 Mobilux Mobil Oil Corporation E P 2 Royco 45A Royal Lubricants Co L 1231 Sinclair Refining Company Grease Aircraft MIL G 7711 Regal AFB2 Regal Texaco Incorporated General Purpose Starfak Premium PED 3040 Standard Oil of Calif Aeroshell Grease 6 Shell Oil Company Royco II Royal Lubricants Co Grease Lubricating MIL G 21164 Aeroshell Grease Sh...

Page 1606: ...lic Texaco Incorporated Oil AA RPM Aviation Oil Standard Oil Company No 2 Code of California PED 2585 PED 3337 3126 Hydraulic Oil Exxon Company U S A Univis 40 Aeroshell Fluid 4 Shell Oil Company SL 7694 Aero HF Mobil Oil Corporation Royco 756 756A Royal Lubricants Co and 756B Isopropyl Alcohol Fed Spec TT I 735 Local Supplier Isocryl Tape PMS C1012 2 Schnee Moorehead Chemicals Incorporated Kevlar...

Page 1607: ... Oil Company Low Temperature Sinclair Aircraft Sinclair Refining Orbit Lube Company 1692 Low Temp Oil Texaco Incorporated Aviation Instrument Standard Oil Company Oil of California Royco 363 Royal Lubricants Co Rain Repellent FSCM 50150 Repcon Unelco Corporation Safety Walk Flextred 300 Wooster Products Pressure Sensitive Incorporated Sealant MIL S 11031B PRC 5000 Products Research PRC 383 Company...

Page 1608: ...Mining and Manufacturing Industrial Specialties Division EC 612 Leak Marker or Weather Stripping etc RTV 157 General Electric Piper P N 279 021 Silicone Products Department G E SS 4004 Primer General Electric RTV 88 with Silicone Products RTV 9811 Department Sealant AMS 3333 Type II EC 801 1063 3M Company Windshield Windows Class B 2 Piper P N 279 047 PR 1425 Products Research Piper P N 279 019 Co...

Page 1609: ... Products Inc Teflon Tape 003 x 5 wide 1 Minnesota Mining and Manufacturing Company Shamban W S and Co 003 x 25 wide 2 Johnson Johnson Inc Permacel Division Thread Sealant MIL T 27730 Permacel 412 Johnson Johnson Inc for High Pressure Permacel Division Oxygen System Vinyl Foam 1 in x 1 8 in 530 Series Type I Norton Tape Division Vinyl Foam Tape 1 8 in x 1 in 501 Series Type II Norton Tape Division...

Page 1610: ...PAGE 20 Feb 28 07 8D10 91 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1611: ...ex Chemical P O Box 501 Detroit MI 48232 Dow Corning Corporation Alpha Molykote Plant 64 Harvard Avenue Stanford CT 06902 Dukes Astronautics Co 7866 Deering Avenue Canoga Park CA 91304 DuPont Company Finishes Div DuPont Building Wilmington DE 19898 302 774 1000 E Exxon Oil Company 1251 Avenue of the Americas New York NY 10020 212 398 3093 F Fel Pro Incorporated 7450 N McCormick Blvd Box C1103 Skok...

Page 1612: ...NJ 07936 201 887 3100 S Schnee Moorhead Chemicals Inc Shamban W S and Co 1857 Centinela Avenue Santa Monica CA 90404 213 397 2195 Shell Oil Company 909 Fannin St STE 700 Houston TX 77010 1016 713 220 6697 Sinclair Refining Co 600 Fifth Avenue New York NY 10020 Socony Mobil Oil Co Washington 5 DC 20005 Solar Compounds Corp 1201 W Blancke Street Linden NJ 07036 201 862 2813 Standard Oil of Californi...

Page 1613: ...ENANCE MANUAL CHART 12 ELECTRICAL WIRE CODING CIRCUIT FUNCTION CIRCUITS LETTER A AUTOPILOT C CONTROL SURFACE E ENGINE INSTRUMENT F FLIGHT INSTRUMENT G LANDING GEAR H HEATER VENTILATING DEICING L LIGHTING P POWER Q FUEL OIL RP RADIO POWER RZ RADIO AUDIO J IGNITION W WARNING K STARTER ...

Page 1614: ...OUND TO CHASSIS WITH TERMINAL GROUND OR CIRCUIT RETURN GROUNDS FUSE A DIODES GENERAL ZENER UNIDIRECTIONAL ZENER BIDIRECTIONAL T P SHIELDED TWO CONDUCTOR W GROUND A B HORN HEATED ELEMENT SQUIB ELECTRIC IGNITER A INDICATOR LIGHT LETTER DENOTES COLOR ASTERISK IS NOT PART OF SYMBOL INCANDESCENT LAMP LAMPS FLUORESCENT LAMP MOTOR METER LETTER DENOTES THE TYPE OF METER i e A AMMETER M A POLARITY POSITIVE...

Page 1615: ...ED OPENS ON RISING TEMPERATURE OR t t t t NOTE t symbol shall be replaced by data giving the operating temperature of the device NORMALLY OPEN NORMALLY OPEN HELD CLOSED SELECTOR OR MULTI POSITION SWITCH NORMALLY CLOSED HELD OPEN LIMIT SWITCH DIRECTLY ACTUATED SPRING RETURN NORMALLY OPEN CLOSES ON RISING TEMPERATURE NORMALLY CLOSED OPENS ON RISING TEMPERATURE t t t NORMALLY OPEN INTERNAL HEATER SHO...

Page 1616: ...PAGE 26 Feb 28 07 8D16 91 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1617: ...PAGE 27 Feb 28 07 8D17 91 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1618: ...PAGE 28 Feb 28 07 8D18 91 10 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1619: ... 1 Feb 28 07 8D19 91 21 20 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 B303 Blower 2 CB393 Circuit Breaker 3 Amp Avionics Cooling Figure 1 Sheet 1 of 4 2 1 ...

Page 1620: ... Feb 28 07 8D20 91 21 20 M AVIONICS COOLING WHITE RC1A 22 P327 J327 1 1 CO PILOT S CB PANEL 2 2 GB2 R BLACK RC2A 22 3 A BLOWER 89801 AH 37 0 85508 L 101238 E 101301 C 104051 C CB393 B303 Avionics Cooling Figure 1 Sheet 2 of 4 Effectivity 4636001 thru 4636313 less 4636299 ...

Page 1621: ...MALIBU MIRAGE MAINTENANCE MANUAL 104301 H S 37 0 AVIONICS COOLING CB393 3A RC1A22 J327 1 2 B303 BLOWER P327 WHITE BLACK RC2A22N GB2 R 1 2 AV5 MUFFIN FAN BLACK RED RED BLACK AV BUS Avionics Cooling Figure 1 Sheet 3 of 4 Effectivity 4636299 and 4636314 thru 4636374 ...

Page 1622: ...UAL PAGE 4 Feb 28 07 8D22 91 21 20 AV BUS 1 CB391A22 3A CB391 AVIONICS COOLING P J 3C 6 RC2B22N RC2A22N RC1A22 GB2 R 1 2 AV4 BLOWER RC1B22 AV5 1 2 BLACK RED WHT BLK FAN MUFFIN B303 105115 A 17 0 Avionics Cooling Figure 1 Sheet 4 of 4 Effectivity 4636375 and up ...

Page 1623: ... MANUAL 3 2 1 4 6 Item Designation Description 1 CB333 3 Amp Circuit Breaker 2 A312 Cabin Pressurization Dump Solenoid 3 S310 Cabin Pressurization Dump Switch 4 K7 Squat Switch Relay 5 A314 Cabin Pressure Sensor 6 S103 Squat Switch Assembly Cabin Pressurization Figure 1 Sheet 1 of 4 5 4 ...

Page 1624: ...L P329 24 W6B 22N W6A 22 SQUAT SWITCH RELAY K 7 CABIN PRESSURIZATION SWITCH NORMAL POSITION 2 1 3 6 4 2 A B 7 9 8 LEFT MAIN SQUAT SWITCH CP15A 22N CP17A 22 CP16B 22 CP15B 22 CP14B 22 CP17B 22 P301 J301 P101 P104 J104 P387 J387 C NO 9 10 8 7 11 Y Y CP17C 20 7 9 CP17D 20N DUMP NORM P330 1 3 4 2 6 5 89801 AH 29 0 GB5 A Cabin Pressurization Figure 1 Sheet 2 of 4 Effectivity 4636001 thru 4636020 ...

Page 1625: ...B22N P384 R384 7 7 2 CP15A22N 3 DUMP S310 CB333 CABIN PRESSURE 3A P384 P384 8 8 R384 R384 DUMP CP17B22 CP14A22 CP14B22 S103 SHN ON GND SQ SW SHN WT ON WHEELS L MAIN 8 CP17C20 CP17D20N 9 7 9 7 J101 P101 P301 Y Y A312 P330 A B DUMP SOLENOID SHN ON GND SQUAT SW RELAY NO 2 SHN WT ON WHEELS 4636314 AND UP GND TO DUMP 11 3 7 14 16 SEE 91 77 40 FIGURE 2 J301 4636132 AND UP 85508 L 29 0 101238 E 101301 C ...

Page 1626: ...B22N HOUR METER CB332 1D J P METER M6A20 1 HOUR GB7 L 2 M310 CABIN PRESS B CP15A22N CP15C22 CP16B22 1 3 P 375 J 6 7 8 CB333A22 P330 A 3A DUMP CB333 10 J 1E P CP14A22 P329 4 P A314 SENSOR W6A22 W6B22N 9 1 CP17C22 AV1G22 D14A22N D14B22 7 2 6 3 18 17 A 10 11 4 8 20 1 2 CR8 B CRX K8 12 387 E3V22N CP15D22 CP16C22 E3U22 M5D20 M5B20 GB7 K CP17B22 CP14B22 CP17A22 Y Y P301 J101 P101 P CP17D20N 9 2 6 7 5 3 ...

Page 1627: ...tion 1 CB358 10 Amp Circuit Breaker 2 S333 Vent Defog Switch 3 B402 Vent Defog Blower 4 S344 Cabin Heat Switch 5 F401 100 Amp Current Limiter 6 K407 Cabin Heater Relay 7 A429 Temperature Sensors 8 F409 35 Amp Current Limiter 9 R401 Heater Assembly 6 3 7 9 2 4 1 8 5 Vent Defogger and Cabin Heater Figure 1 Sheet 1 of 3 ...

Page 1628: ...PAGE 2 Feb 28 07 8E4 91 21 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Vent Defogger and Cabin Heater Figure 1 Sheet 2 of 3 Effectivity 4636001 thru 4636131 ...

Page 1629: ...09 GB1A18 J CB357A18 P 3 2E TEMPERATURE A429 EH3A18 SENSORS GB1B18 9 10 8 B B EH3B18 Z P303 a P401 Z a GB1C18 J401 18 A A EH3D18 J 1 P 429 EH1B10 VENT DEFOG P422 1 GRN BLK B402 BLOWER CR406 K407 RELAY EH3E18N HEATER CABIN EH1G10 EH1E10 R401 J 392 P 101238 E 30 0 101301 C 104051 C 104301 NEW S 105115 A 26 0 WITH AVIDYNE ENTEGRA OPTION ONLY Vent Defogger and Cabin Heater Figure 1 Sheet 3 of 3 Effect...

Page 1630: ...PAGE 4 Feb 28 07 8E6 91 21 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1631: ...r Switch 4 CB338 15 Amp Circuit Breaker 5 CB339 5 Amp Circuit Breaker 6 B302 Right Blower Fan Motor 7 A320 High Pressure Switch 8 K501 Condenser Blower Relay 9 K405 Compressor Clutch Assembly 10 A321 Low Pressure Switch 11 CB340 25 Amp Circuit Breaker 12 B501 Condenser Blower Motor Assembly 13 CR405 Diode 14 CR501 Diode 1 8 12 4 5 11 7 10 3 6 2 6 2 9 Vent Blowers and Air Conditioning Figure 1 Shee...

Page 1632: ...PAGE 2 Feb 28 07 8E8 91 21 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Vent Blowers and Air Conditioning Figure 1 Sheet 2 of 5 Effectivity 4636001 thru 4636131 ...

Page 1633: ...PAGE 3 Feb 28 07 8E9 91 21 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Vent Blowers and Air Conditioning Figure 1 Sheet 3 of 5 Effectivity 4636132 thru 4636186 ...

Page 1634: ... AC6C16 TB303 3 P333 g J402 g AC6D16 P304 P402 1 AC6E16 J419 P419 K405 COMPRESSOR CLUTCH CR 405 AIR CONDITIONER POWER 25A CB340 AC7A12 BKHD FEEDTHRU AFT PRESS X1 AC5A16 AC5B16N X2 A2 A1 WHT BLK K501 COND BLWR RELAY B501 CONDENSOR BLOWER CR 501 P392 P397 P392 BLOWER LO SW P397 P397 AC3C16 AC2C16 1 1 2 3 2 HI LOW HI LOW X2 X1 AC2F20N AC2D16 AC2E20 AC3D16 RELAY BLWR HI LO K502 502 CR A2 A1 A4 A3 1013...

Page 1635: ...I SW CB338 FANS CABIN AIR COND CONTROL CB339 NON ESS BUS HI P 5A 15A 392 2 P304 2 P333 1 AC4A20 AC11A16 1D 8 CB339A20 J AC1B20 1 P AC5A16 P402 AC2B16 AC3B16 P395 2 3 1C 3 J CB338A16 P 1 AC1A16 SWITCH COND AIR AC3C16 RELAY HI LO CR502 X2 AC2F20N BLWR AC2E20 A3 A2 X1 AC2D16 AC3D16 K502 A4 A1 HI LOW ORG RED B301 BLK BLOWER BLOWER LOW 2 1 RED HI ORG AC2C16 351 355 LEFT RIGHT B302 BLK BLOWER LO SW P J ...

Page 1636: ...PAGE 6 Feb 28 07 8E12 91 21 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1637: ...PAGE 1 Feb 28 07 8E13 91 22 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1638: ...L Y W X V Z a c d e f g h i b 89848 072 SWITCH CAP 8941K700 SWITCH JB1 N SEE WHT BLU ORG GRN TRIM MASTER SWITCH JB1 J SEE LB2 C SEE WHT BLU ORG P565 BLK BLU SEE GB3A D 3 2 1 3 1 2 P564 WHT BLU ORG GRN BLK RED TRIM SERVO WHT BLU ORG GRN P559 TRIM CB BLK TO P1E 3 GB3A A SEE SEE GB3A B REF TRIM SONALERT CENTER PEDESTAL BLU WHT ORG GRN AUDIO 27 6 8 5 14 3 11 10 1 15 13 2 4 9 7 12 P555 P552 47 50 33 17...

Page 1639: ...7 P551 15 LIGHTS A P GB3A E SEE TRANSDUCER BLU WHT WHT BLU ORG P557 2 3 GB2A L SEE BLK LB2 D SEE GB3A C SEE FD ENABLE MAN TRIM DN MAN TRIM UP TRIM INTERRUPT 8 CWS CWS GND 55X A P P551 RED PILOT C W RED A P F D MASTER SWITCH RED P N 39326 4 P561 RED LB4 F 7 4 TO P565 2 P554 6 11 2 5 9 8 3 Y2A22 SH 1 TO P553 8 SEE GB3A R P566 CO PILOT C W 5 GB3A P SEE BLK 3 B A P567 RELAY 5 9 4 1 6 2 8 3 11 2 6 4 7 ...

Page 1640: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 4 Feb 28 07 8E16 91 22 10 THIS PAGE INTENTIONALLY BLANK ...

Page 1641: ...iption 1 CB376 1 10 Amp Circuit Breaker 2 CB374 2 Amp Circuit Breaker 3 F402 5 Amp Fuse F404 5 Amp Fuse F405 5 Amp Fuse 4 K6 Ground Clearance Relay 5 S313 Ground Clearance Switch Ground Clearance Switch Cap CR6 Diode 3 Amp Circuit Breaker 4636001 thru 4636020 only 4 5 1 2 3 4 Ground Clearance Figure 1 Sheet 1 of 5 5 ...

Page 1642: ...PAGE 2 Feb 28 07 8E18 91 23 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Ground Clearance Figure 1 Sheet 2 of 5 Effectivity 4636001 thru 4636131 ...

Page 1643: ...PAGE 3 Feb 28 07 8E19 91 23 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Ground Clearance Figure 1 Sheet 3 of 5 Effectivity 4636132 thru 4636247 ...

Page 1644: ... AUDIO AMP 2 3 1 RP14A22 RP12A22 P303 RP8A18 RP6A22 RP7A20 RP10A20 P401 E e J401 E e RP7B22 RP10B22 CR6 4 20 3 22 K6 11 13 18 20 10 5 P317 J317 20 18 1 4 2 6 5 3 AVI P366 P366 3 2 NAV GPS 1 5A CB375 1 15 12 COMM 1 1 18 NAV GPS 1 COM 1 GPS N 1 RP16A20 SEE 91 31 50 FIGURE 1 J317 2 104051 C 35 0 104301 B S 5A IN S N S 4636314 AND UP Ground Clearance Figure 1 Sheet 4 of 5 Effectivity 4636248 thru 4636...

Page 1645: ...375A20 AUDIO AMP MKR AV BUS 1 5A 5A 1 3B P J 3 TO P3402 8 P303 e E e E J401 P401 RP14A22 RP12A22 RP10B20 RP7B20 RP6A22 COMM 1 RP16A20 CB376 COMM 1 P J 3A CR6 3 11 13 TO P3402 9 4 22 18 20 20 J 317 10 1 12 5 15 18 18 20 6 3 1 4 5 K6 2 F402 B A 8 TO AUD1 13 AVIONICS 105115 A 21 0 GPS N 1 GPS N 1 COMM 1 TO P1061 20 TO P43011 19 TO P43011 20 TO P43021 11 TO P43021 12 Ground Clearance Figure 1 Sheet 5 ...

Page 1646: ...PAGE 6 Feb 28 07 8E22 91 23 00 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1647: ...NABLED XMP1 18 37 RS232 TX 22 ACFT GND 19 XMDR XM SATELITE RCVR 28 VDC ACFT PWR RX XMRANT 01 ANTENNA SEE GB1A N P3C 7 MFD P530 RS232 1A GND 12 RS232 1A TX 10 RS232 RX RS232 GND 4 23 CIRCUIT BREAKER PANEL INSTRUMENT PANEL W B O 20 BLK 20 RED CABLE REF 105130 B F 24 REFERENCE DRAWING 91 24 30 FIG 3 XM Receiver Figure 1 Effectivity 4636375 and up ...

Page 1648: ...PAGE 2 Feb 28 07 8E24 91 23 30 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1649: ...PAGE 1 Feb 28 07 8F1 91 23 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1650: ...R INPUT POWER GROUND POWER GROUND SPEAKER GND GMA 340 6 44 43 7 8 9 P3402 5 11 10 22BLK 22BLK 22BLK INSTRUMENT PANEL BLU WHT BLU WHT ORG ORG BLU WHT WHT BLU LB2 H SEE 1 2 P317 4 CW15 CW16 CW15J CW16J 1 2 J34019 3 1 J34020 4 3 2 3 2 1 J34016 2 3 1 4 J34018 10 12 P566 12 10 P554 22BLU PILOT MIC PILOT PHONE C PILOT MIC C PILOT PHONE P34012 P O PILOT CONTROL WHEEL GB1A C SEE GB1A E SEE GB1A D SEE SPKR...

Page 1651: ...LU J3406 WHT BLU J34011 PASSENGER 1 PASSENGER 2 PASSENGER 3 PASSENGER 4 PAX 3 MIC IN 39 PAX 3 MIC GND 40 41 42 PAX 4 MIC IN PAX 4 MIC GND 26 27 28 MUSIC 2 INPUT GND MUSIC 2 INPUT R MUSIC 2 INPUT L P34013 2 1 3 WHT BLU ORG BLU WHT ORG 2 1 3 2 1 3 2 1 3 PASSENGER 1 4 2 3 1 J3409 PASSENGER 2 ORG BLU WHT PASSENGER 4 J34010 1 3 2 4 4 2 3 1 J3405 PASSENGER 3 WHT BLU ORG ORG BLU WHT TO P3402 SHIELDS ON S...

Page 1652: ...BREAKER PANEL SUMMED AUDIO OUT 24 23 SHIELD CHASSIS GROUND POWER GROUND 28 VDC POWER 25 12 13 JB1 Y SEE JB2 K SEE 20RED 22BLK 22BLK AUD1 1 XPNDR 1 JB1 D SEE P3B 8 GB4A A SEE GB4A B SEE 2 XPNDR 1 AUDIO IN SHIELD 105130 B F 26 REFERENCE DRAWING 91 24 30 FIG 3 91 24 30 FIG 4 Summing Amp Figure 2 Effectivity 4636375 and up ...

Page 1653: ...PAGE 5 Feb 28 07 8F5 91 23 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1654: ...PAGE 6 Feb 28 07 8F6 91 23 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1655: ...Breaker 40 Amp 8 S314 Radio Master Switch 9 K310 K315 Radio Master Contactor 10 A334 A335 Voltage Regulator 11 Day Night Switch 12 J420 External Power Receptacle 13 Alternator 1 14 K403 External Power Contactor 15 2 16 2 17 Battery 18 K401 Battery Contactor 19 S315 Battery Switch 20 2 21 S316 S323 Alternator Switch 22 R304 R305 Shunt 23 2 24 CB395 Avionics Bus Tie Circuit Breaker 25 Amp 1 Alternat...

Page 1656: ...PAGE 2 Feb 28 07 8F8 91 24 30 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Power Distribution and Control Figure 1 Sheet 2 of 7 Effectivity 4636001 thru 4636020 ...

Page 1657: ...PAGE 3 Feb 28 07 8F9 91 24 30 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Power Distribution and Control Effectivity Figure 1 Sheet 3 of 7 4636021 thru 4636131 ...

Page 1658: ...PAGE 4 Feb 28 07 8F10 91 24 30 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Power Distribution and Control Figure 1 Sheet 4 of 7 Effectivity 4636132 thru 4636186 ...

Page 1659: ...X2 X1 401 GB5 H K401 P2D22 a _ P303 a _ P401 J401 2 P383 2 R383 P2B22 R305 SHUNT P17A6R BATTERY CONTACTOR P4A6 F 4 0 4 F 4 0 5 F 4 0 2 P1C18 P16A6R F 4 0 3 P16A6RN P16A18RN 1 P383 P2C22 2 3 S315 BATTERY MASTER AUX F1 ALT 2 F2 F 4 0 7 BLK P402 P17C6R RP1B8R GB2 N CR315 2 5 RP3A22R 1 5 4 2 1 4 RP4A22RN RP4A22LN RP1A8R 326 5A 5A 325 CB 395 MAIN BUS RADIO MASTER SW K315 P31A20R P30A20R GB1 R d J402 b ...

Page 1660: ...303 P16A6L f f P16A6LN P401 A334 1 J401 7 2 3 8 ORN BLU BRN BLK R304 50mV SHUNT F302 F309 P11A22 P11B22 P31A20L P30A20L TO P384 4 TO P384 3 P35A20L S316 S323 R308 VOLTAGE REGULATOR 359 J P 1 5 4 9 6 GRY LAV YEL RED GRN 383 P7B20L P7B20R 5 P 1D 4 J P32A20 P7A20L P7A20R 7 4 P ALT 1 P8B20L MASTER P32C20L P8D20L 5 J P 8 6 3 P32B20L P32B20R P8A20L P8A20R 5 6 3 2 MASTER 2 3 5 6 P402 BLK BRN BLU ORN P16A...

Page 1661: ...P2A20 CONTACTOR TO STARTER 250A F401 EH1B10 K403 A1 A2 CONTACTOR BATTERY P22A20N CR403 CONTACTOR EXT PWR CR402 35A F409 4 6 5 SWITCH RADIO MASTER 3 S365 1 2 GB5 H RP1B8L P303 A P401 A J401 383 1 2 P2E22N P2B22 J AV 2 BUS 25A CB393 AV 1 BUS S315 BATTERY MASTER P2C22 P2D22 P 3 2 RECEPTACLE EXTERNAL P1C18 P1B6N P22A20 P20A6 P21A6N POWER BTTY BUS J420 105115 A 2 1 X2 X1 A3 A4 A4 A3 P6A20 P303 S R P6B2...

Page 1662: ...PAGE 8 Feb 28 07 8F14 91 24 30 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1663: ...1 3 4 CB302 CB303 Circuit Breaker 70 Amp or 80 Amp 5 6 F408 Fuse 5 Amp 7 14 15 M311 M312 Ammeters 16 M301 Volt Meter 17 19 20 K323 Day Night Bright Dim Relay 21 22 R304 R305 Shunt 23 F301 F304 Fuse 5 Amp See Power Distribution and Control 20 22 23 15 16 4 6 Power Monitor and Meters Figure 2 Sheet 1 of 4 Effectivity 4636001 thru 4636131 ...

Page 1664: ...PAGE 10 Feb 28 07 8F16 91 24 30 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Power Monitor and Meters Figure 2 Sheet 2 of 4 Effectivity 4636001 thru 4636131 ...

Page 1665: ...P5J20 P11B20 P11E20 P11G20 P11L20 P11M20 1 2 2 1 P11C20N P11D20 P11F20 P16A6R TO ALTERNATOR NO 2 50mv SHUNT R305 P5A18R F304 5A 5A F303 P6A18R M312 J315 P315 1 1 2 2 P307 J307 F302 R304 SHUNT 5A F301 5A 50mv P16A6L NO 1 TO ALTERNATOR P10B20 P6C20N CR323 R314 BRT DIM RELAY R315 R316 P6B20 P5H20 P5A18L P6A18L P10C20N P10D20 P10L20 P10M20 P10E20 P10G20 P10F20 J380 P380 P6A20 TO DAY NIGHT SWITCH SEE 9...

Page 1666: ... SEE 91 33 10 FIGURE 5 104301 D S 2 1 L28C20 P5A18L P6A18L 2 1 P307 F301 NO 1 TO ALTERNATOR P16A6L F302 R304 SHUNT 5A 5A 50mv 80A P17A6L 1A P5G20 P5E20 4 8 2 1 5 6 9 7 3 P6C20 P5B20 P6D20 2 1 J307 P5C20 J315 1 2 TO P329 6 LOW BUS VOLTAGE ANNUNCIATOR SEE 91 31 50 FIGURE 1 P5H20N P5A18R P6A18R 1 P315 2 TIE BUS CB327 80A F303 P17A6R 50mv SHUNT R305 F304 5A 5A TO ALTERNATOR NO 2 F399 C B INSTALLED ON ...

Page 1667: ...PAGE 13 Feb 28 07 8F19 91 24 30 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1668: ...0 FIGURE 4 PFD 1 D1 91 34 20 FIGURE 4 PFD 1 A2 91 34 20 FIGURE 4 PFD 1 A4 91 34 20 FIGURE 4 PFD 1 A4 91 34 20 FIGURE 4 PFD 1 D2 91 34 20 FIGURE 4 PFD 2 D4 91 34 20 FIGURE 4 PFD 2 A4 91 34 20 FIGURE 4 PFD 2 A4 91 34 20 FIGURE 4 PFD 2 D3 91 34 20 FIGURE 4 PFD 2 A2 91 34 20 FIGURE 4 PFD 2 A2 91 34 20 FIGURE 4 MFD P530 60 61 62 91 34 20 FIGURE 5 TRIM RELAY GND P567 B 91 22 10 FIGURE 1 GNS430 1 P43011 ...

Page 1669: ... 40 FIGURE 3 KMH 820 P10 SHIELD 91 34 40 FIGURE 3 KMH 820 P10 84 91 34 40 FIGURE 3 KMH 820 P10 83 91 34 40 FIGURE 3 RH FWD AFT GNS430 2 P43012 21 91 34 50 FIGURE 1 GNS430 2 P43012 22 91 34 50 FIGURE 1 JB6 Z 91 24 30 FIGURE 4 KN 63 P631 1 A 91 34 50 FIGURE 3 WX 500 P5001 5 91 34 40 FIGURE 2 TAS SW 91 34 40 FIGURE 3 CONTROL WHEEL P554 3 91 22 10 FIGURE 1 GNS430 2 P43012 77 91 34 50 FIGURE 1 GNS430 2...

Page 1670: ... 05E REF Z N M S N R P T L W C G H J D E F K A CTJ1 22E 05E REF S L N P R M A B H C E F G D J K KMH 820 P10 4 91 34 40 FIGURE 3 SQUAT SW GND P387 18 FROM 105117 ELECTRICAL HARNESS GTX 330 1 P3301 17 OR GTX 330 1 2 P3302 17 91 34 50 FIGURE 2 KN 63 SUPPRESSION SHIELD 91 34 50 FIGURE 3 KMH 820 SUPPRESSION SHIELD 91 34 40 FIGURE 3 GTX 330 1 P3301 31 OR GTX 330 1 2 P3302 31 91 34 50 FIGURE 2 KMH 820 P1...

Page 1671: ...FIGURE 3 KMH 820 P10 54 91 34 40 FIGURE 3 MFD P530 8 91 34 20 FIGURE 5 KMH 820 P10 55 91 34 40 FIGURE 3 MFD P530 28 91 34 20 FIGURE 5 PFD 1 P7321 22 91 34 20 FIGURE 4 PFD 1 P7321 21 91 34 20 FIGURE 4 KMH 820 P10 60 91 34 50 FIGURE 2 100 ONLY KMH 820 P10 61 91 34 50 FIGURE 2 100 ONLY XP 1 2 1 91 34 50 FIGURE 2 107 ONLY XP 1 2 2 91 34 50 FIGURE 2 107 ONLY PFD 2 P7322 22 91 34 20 FIGURE 4 XP 1 2 5 91...

Page 1672: ...D P530 18 91 34 20 FIGURE 5 PFD 2 P730 15 91 34 20 FIGURE 4 L23T22 L33A20 L28D20 ADF IND TRIM MON RAD ALT AUTOPILOT KMH 820 ANNUN DME P313 F P313 F L23V22 L23P22 L23Y22 TO P317 19 L23Z22 TO P317 28 LB3 LB2 LB4 AVIONICS LIGHTS CTJ1 20E 01B REF AVIONICS LIGHTS CTJ1 20E 02C REF SWITCH LIGHTS CTJ1 20E 01B REF A M L G K H J F C B A E D G J H K C B A M L G K H J F C B E D D E Effectivity 4636375 and up ...

Page 1673: ...PAGE 1 Feb 28 07 8G1 91 25 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1674: ... 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 R307 Cigar Lighter 1 or R307 Power Point 2 2 F403 5 Amp Fuse 1 4636001 thru 46360247 only 2 4636248 and up 2 1 Effectivity Cigar Lighter Power Point 4636001 and up Figure 1 Sheet 1 of 2 ...

Page 1675: ...GHTER 5 A BATTERY BUS CL6A 18 P401 P303 J401 CL6B 18 CIGAR LIGHTER ASSEMBLY R 307 c c 1 2 F403 89801 AH 41 0 85508 L 101238 E 46 0 101301 C 5 A BATTERY BUS CL6A 18 P401 P303 J401 CL6B 18 POWER POINT RECEPTACLE R 307 c c 1 2 F403 CL6C 18N 104051 C 46 0 104301 NEW S S N S 4636001 THRU 4636247 ONLY S N S 4636248 AND UP GB 3A Effectivity 4636001 and up ...

Page 1676: ...T INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Effectivity Electric and Digital Clocks 4636001 thru 4636020 Figure 2 Sheet 1 of 2 Item Designation Description 1 F406 5 Amp Fuse 2 LC 2 Digital Quartz Clock 3 LC 6 Digital Quartz Clock 1 2 or 3 ...

Page 1677: ...TTERY BUSS P357 J357 1 3 6 5 2 P401 P303 J401 GB5 B TO 91 33 10 FIGURE 3 TAPER BLOCK 1 CL4A 20 LC 2 BATTERY BUSS P357 J357 4 1 3 6 CL3A 20N CL1A 20 5 2 CL1B 20 GB5 B CL3A 20N 1 3 6 5 2 ELEC CLOCK 4 4 h h h h h h CLOCK STANDARD DIGITAL CLOCK OPTIONAL CL1A 20 P401 P303 J401 5 A F406 1 1 1 2 3 89801 AH 39 0 39 1 TO 91 33 10 FIGURE 3 TAPER BLOCK 1 5 A F406 5 A F406 Electric and Digital Clocks Figure 2...

Page 1678: ...RCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Effectivity Digital Voice Recorder Clock 4636021 and up Figure 3 Sheet 1 of 2 Item Designation Description 1 F406 Fuse 5 Amp 2 CB394 Circuit Breaker 1 5 Amp 3 Digital Quartz Clock 1 2 3 ...

Page 1679: ...DIO OUT AUDIO LO CL4A22S 2 2 1 1 3 3 CL P1 CL J1 PWR TO ELT 110 4 SEE 25 60 00 FIGURE 2 AUDIO INTERCOM REF AUDIO INTERCOM HARNESS CLOCK DVR 300i XT PHONE JACK PILOT CB394 1A _ 7 9 1 2 14 AVI BUS PWR AUDIO LO AUDIO OUT BATT BUS PWR GROUND AUDIO IN AUDIO LO CLOCK DVR 300i XT 6 13 S N S 4636021 THRU 4636247 ONLY S N S 4636248 AND UP 85508 L 33 0 101238 E 101301 C 104051 C 104301 NEW S Digital Voice R...

Page 1680: ...PAGE 8 Feb 28 07 8G8 91 25 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Stereo Optional Figure 4 Sheet 1 of 4 Item Designation Description 1 F408 5 Amp Fuse 1 ...

Page 1681: ...2 0 F408 SEE 91 24 30 FIGURE 1 ST1B20 ST1B20N 5A F408 STIA20 h _ h _ P304 P402 J402 RED BLACK YEL RED BLACK RED BLACK 14V 28V RED BLACK RED BLACK STEREO CONSOLE BLK AM CD PLAYER FM P1 2 P2 1 1 2 85508 E L 42 0 TO BATTERY BUSS 91 24 30 FIGURE 1 S N S 4636001 THRU 4636020 ONLY S N S 4636021 THRU 4636076 ONLY Stereo Optional Figure 4 Sheet 2 of 4 Effectivity 4636001 thru 4636076 ...

Page 1682: ...TIA20 h _ h _ P304 P402 J402 RED BLACK YEL RED BLACK RED BLACK 14V 28V RED BLACK WHITE RED BLACK STEREO CONSOLE BLK AM CD PLAYER FM P1 2 P2 1 1 2 1 1 3 3 2 2 85508 L 101238 E 42 0 101301 C 104051 C 104301 NEW S 41 0 TO BATTERY BUSS 91 24 30 FIGURE 1 Stereo Optional Figure 4 Sheet 3 of 4 Effectivity 4636077 thru 4636374 ...

Page 1683: ...A20 h _ h _ P304 P402 J402 RED BLACK YEL SMALL RED RED BLACK 14V 28V RED BLACK WHITE RED BLACK STEREO CONSOLE POWER SWITCH CD PLAYER P1 1 1 3 3 2 2 105115 A 31 0 TO BATTERY BUSS 91 24 30 FIGURE 1 1 1 2 2 B A D C F E YEL LARGE CONTROLLER GROUND POINT Stereo Optional Figure 4 Sheet 4 of 4 Effectivity 4636375 and up ...

Page 1684: ...PAGE 12 Feb 28 07 8G12 91 25 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1685: ...scription 1 CB323 3 Amp Circuit Breaker 2 S347 Stall Test Switch 3 S103 Squat Switch Assembly 4 S349 S350 Actuator Switch 2 each 5 S348 Throttle Lever Switch Assembly 6 A305 Horn Dual Warn Unit 7 K4 Relay Assembly 8 Lift Computer 9 Lift Transducer 5 3 1 2 4 7 6 9 8 Stall Detection and Warning Figure 1 Sheet 1 of 4 ...

Page 1686: ... 3 S2N22 S2T22 4 EXECUTE S2P22 S2R22 5 6 FULL 10 20 FLAPS 6 4 5 S2L22 S2S22 J348 3 2 1 S348 NC NO C PWR ON OFF PWR THROTTLE LEVER SW 10 12 11 S103 CLOSED IN AIR L MAIN SQUAT SW C C S350 8 25 S349 P382 S2Z22 S2J22 9 12 WARN DEVICE FAIL 25 27 S2A22 TO ANNUNCIATOR P329 3 GND COMPUTER K4 FAIL LOGIC RELAY P317 J317 GB4 F A305 G4H22N GEAR HORN HORN STALL AIR FLOW P376 STALL TEST P329 31 IN S N S 4636001...

Page 1687: ...E S2P22 S2R22 5 6 FULL 10 20 FLAPS 6 4 5 S2L22 S2S22 J348 3 2 1 S348 NC NO C PWR ON OFF PWR THROTTLE LEVER SW 10 12 11 S103 CLOSED IN FLT L MAIN SQUAT SW C C S350 8 25 S349 P382 S2Z22 S2J22 9 12 WARN DEVICE FAIL 25 27 S2A22 TO ANNUNCIATOR P329 3 SEE 91 31 50 GND COMPUTER K4 FAIL LOGIC RELAY P317 J317 GB4 F A305 G4H22N GEAR HORN HORN STALL AIR FLOW L I F T T R A N S D U C E R P376 R E T U P M O C T...

Page 1688: ... 382 S2L22 J C S350 2 1 C S349 3 P S2S22 S3H20 S3E20ORG S3E20BLU h f K J101 S2M22N f h K 105 P 1E J 7 P J B F E S1A22 P101 S3G20 S3B20WHT S3B20BLU P301 S j j S b b 26 S2D22 SECONDARY TEST SWITCH THROTTLE POSITION ENABLE EXECUTE 10 20 S2T22 S2N22 S2P22 S2R22 3 4 6 5 FULL S2F22 S2E22 S2H22 S2M22 27 28 7 8 FLAPS 28 VDC POWER SELF TEST PRIMARY P376 S2B22 S2C22 S2G22 1 16 25 24 10 GND STALL HORN A305 3...

Page 1689: ... Description 1 CB330 Circuit Breaker 10 Amp 2 CB331 Circuit Breaker 3 Amp 3 K321 Current Sensor 4 MT302 Actuator Motor Assembly 5 K320 Relay 6 A337 Time Delay Module 7 S340 S341 Flap Control Switch CR330 Diode Assembly R310 Resistor Assembly Capacitor Assembly Electric Flaps Figure 1 Sheet 1 of 3 1 2 3 5 6 4 7 ...

Page 1690: ...EC 4 7 uf 2 50wv R310 470 k ohms CW1D 18 CW1G 18 CW1E 18 CW1H 18 FLAP CONTROL UP DN 5 6 2 1 BLK CW1F 18 CW1C 18 RED WC4A 22 K320 FLAP WARN 1 1 FLAP ANNUN IN S N S 4636001 THRU 4636131 ONLY 2 5 0 uf IN S N S 4636001 THRU 4636020 ONLY 3 P328 9 IN S N S 4636001 THRU 4636131 ONLY 4 CB330 IN S N S 4636299 AND 4636314 AND UP 5 CB331 IN S N S 4636299 AND 4636314 AND UP CB330 4 CB331 5 K321 CR330 A337 CR ...

Page 1691: ... 2 3 4 P393 377 GB4 B CW2D22 CW2C22N P B A J 5 6 L28B22 CW2E22N WC5B22 P328 17 50wv 4 7uf CR330 C301 WC4A22 WC3A22 B WC3B22 WC3B22N A337 A CR 329 470K R310 K320 DOWN POTENTIOMETER FLAP RXXX S340 S341 346 2 J P CW1J18 CW1D18 6 5 1 CW1E18 CW1H18 UP CONTROL FLAP CW1C18 WC1B22 CW1B18 CURRENT K321 CW1A18 WC1A22 11 P 1E 2 P 1C WC5A22 SENSOR 1 2 4 5 6 3 CW1F18 CW1G18 CW1K18N FLAP MOTOR BLK MT 302 105115 ...

Page 1692: ...PAGE 4 Feb 28 07 8G20 91 27 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1693: ...IBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 CB324 Circuit Breaker 3 Amp 2 SpeedBrake Cartridge s 3 Up Down Switch on yoke 4 Annunciator Light 5 Asymmetric Logic Switching Unit 3 1 4 2 5 2 SpeedBrakes Figure 1 Sheet 1 of 3 Effectivity 4636187 and up ...

Page 1694: ...2 3 5 6 8 RIGHT SPEEDBRAKE CARTRIDGE CARTRIDGE LEFT SPEEDBRAKE A A B B B C C C D D D E E E F F F G G G H H H J J J K K K K J H G F E D C B A A B C D E F G H J K K J H G F E D C B A 3 2 1 1 2 3 SB1 SB2 SB3 SB4 SB5 SB6 P398 J115 FEEDTHRU P115 P116 P308 FEEDTHRU J215 P115 P116 GB6 C GB6 B BRAKE 2 2 1 1 26 SB2B22 SB2D22 20 317 J P R 317 560 ohm 14 29 TO ANNUN C B REF P 317 J P O K1 PTT SB2E22 DN1V22 P...

Page 1695: ...C E E E D D D B B B A A A K K K J J J H H H P398 P115 6 6 SB J3 5 4 3 2 1 P3 2 3 4 5 1 8 7 7 8 SPEED BRAKE SB2A22 SB2C22 SB2E22 MOTOR ASYMMETRIC LOGIC CONTROL P116 CARTRIDGE RIGHT SPEEDBRAKE FEEDTHRU J215 SB4F22 SB4C22 SB4D22 SB4E22 SB4A22 SB4B22 F F F G G G C C C D E E D D E A B B A A B P115 P308 SB4H22 J K K J J K H H H SB4G22 SB J2 P2 5 6 7 8 1 2 3 4 8 7 6 5 4 3 2 1 1 2 3 3 2 1 ORANGE WHITE BLU...

Page 1696: ...PAGE 4 Feb 28 07 8G24 91 27 60 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1697: ...AINTENANCE MANUAL Item Designation Description 1 CB310 CB311 Circuit Breaker 5 Amp 2 MT101 MT201 Fuel Pump 3 A315 A316 Fuel Pressure Switch 4 CB309 Circuit Breaker 15 Amp 5 S305 Emergency Fuel Pump Switch 6 MT401 Emergency Fuel Pump 2 4 1 3 6 5 Fuel Pumps Figure 1 Sheet 1 of 4 ...

Page 1698: ...P204 P208 J208 LEFT PUMP RIGHT PUMP EMERGENCY FUEL PUMP C B ENGINE DRIVEN PUMP A B P304 P402 J402 SELECTOR VALVE TO ANNUNCIATOR Q13C 20 Q14C 20 P329 12 P329 29 EMERG BUS 15 A EMERGENCY PUMP P304 P402 J402 Q10A 16 Q10B 16 EMERG PUMP Q10D 16N Q10C 16 EMERG PUMP SW 3 2 PRESSURE SWITCHES P423 P424 A315 A316 Q13A 20N Q14A 20N Q14B 20 Q13B 20 Q17B 20 Q16B 20 Q19B 20 Q11D 20N Q11B 20 Q17A 20 Q16A 20 Q19A...

Page 1699: ...4 P204 1 2 MT201 Q12D20N MT401 Q10E16 Q10D16N PUMP EMERGENCY O F F FUEL SELECTOR VALVE CAM 20 20 Y B Y B 20 20 Q10D16 EMERGENCY FUEL PUMP A315 A316 DRIVEN PUMP ENGINE LEFT PUMP PUMP RIGHT Q10B16 4 4 P380 R380 Q10C16 EMERG PUMP SW S305 Q10A16 P380 3 3 R380 2 3 CB309 EMERGENCY PUMP 15A J402 P304 P402 VALVE SELECTOR B A P423 C B P424 PRESSURE SWITCHES Q14B20 Q14A20N Q13B20 Q13B20N Q14C20 Q13C20 J402 ...

Page 1700: ...C J P CB310A20 L BOOST PUMP 5A CB310 1D J 1 P ENGINE Q10D16N FUEL PUMP PUMP FUEL EMERG DRIVEN FUEL SELECTOR VALVE CAM BOOST BOOST Q13B20 P423 20 20 Y Y B B k k J402 20 20 Q14A20N Q14B20 Q10E16 A B P402 C C P304 MT401 C P J J d J201 d Q12B20 Q19A20 Q12D20N P101 P201 Y X J101 P301 V V Y X P302 Q11B20 Q11D20N Q17A20 Q16A20 BLU RED 3 4 P 1 208 2 O F F RT LEFT PUMP RIGHT 1 2 BLU RED J P 1 1 204 108 2 2...

Page 1701: ...2 Circuit Breaker 3 Amp or CB372 Circuit Breaker 3 Amp 2 M305 Dual Fuel Indicator 3 Inboard Fuel Quantity Senders 4 Outboard Fuel Quantity Sender Left 5 Outboard Fuel Quantity Sender Right S N s 4636001 thru 4636020 only In S N s 4636375 and up see 91 77 40 Figure 7 Sheet 3 2 4 1 5 3 Fuel Quantity Indicator Figure 1 Sheet 1 of 3 ...

Page 1702: ...T SENDER RIGHT SENDER GRND J213 P213 Q3ALR 22N Q3AL 22N Q3AR 22N Q2AR 22 A C B C 1 2 1 2 OB IB 1 2 1 2 OB IB J113 P113 Q2BL 20 Q3BL 20N Q2AL 22 Q2BR 20 Q3BR 20N 3A GB4 R NOTE INDICATES TEST POINT FUEL QUANTITY 1 2 3 5 4 3 h h j j W X X W B A P302 J201 P201 89801 AH 9 0 Fuel Quantity Indicator Figure 1 Sheet 2 of 3 Effectivity 4636001 thru 4636020 ...

Page 1703: ...J113 1 2 2 1 P301 P101 J101 SENDERS LEFT RIGHT SENDERS Q2BL20 Q2BR20 Q2AL22 Q2AR20 INBD OUTBD INBD OUTBD Q1B22 Q1A22 Q3D22N GB7 C 19 20 WHT BL WHT Q2C22 1 TO 91 77 40 QDI IN S N S 4636021 THRU 4636131 ONLY EDI IN S N S 4636132 AND UP WHT BL WHT Q2B22 13 18 12 22 TB 1 Q2L22 Q3A22 SEE EXCEEDANCE AUDIO ALERT 91 31 50 FUEL QUANTITY GAUGE LIGHTING LO PWR RETURN RT PWR RETURN LT LIGHTING HI SIGNAL HI RI...

Page 1704: ...PAGE 4 Feb 28 07 8H8 91 28 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1705: ... MAINTENANCE MANUAL Item Designation Description 1 CB322 Circuit Breaker 25 Amp 2 CB321 Circuit Breaker 3 Amp 3 S342 Gear Selector Switch 4 A332 A331 Pressure Switch Assembly 5 MT301 Hydraulic Pump 6 S103 Squat Switch Assembly 3 1 2 4 5 6 Hydraulic Pump Figure 1 Sheet 1 of 3 ...

Page 1706: ...SQUAT SWITCH G11C 20 G11B 20 TO ANNUNCIATOR P329 7 22 22 22 RED WHT RELAYS ARE INTERLOCKED TO PREVENT SIMULTANEOUS OPERATION SQUAT SWITCH SHOWN WITH WEIGHT ON WHEELS F M M F G13D 22 RELAY SHOWN GEAR DOWN LOCKED G13C 22 2 6 4 G13B 22 A B K313 CR313 TO LANDING GEAR POSITION INDICATOR 1 2 3 FUSE HOLDER S103 A1 A2 A3 A4 UP DOWN G10B 12 22 22 IN S N S 4636132 THRU 4636186 ONLY P328 6 IN S N S 4636001 T...

Page 1707: ... 91 31 50 FIGURE 1 SHEET 15 G13D22 BLK G13B22N GEAR SELECT SWITCH G11A20 P J 1D 3 G9A20 2 S342 G13A22 6 4 2 RED NC PUMP DN PRESS SW UP DN 3 1 G12A20 G11D20 P G11B20 G11C20 M M J101 F P301 F P101 BLK 6 4 5 4 6 5 L MAIN SQUAT SWITCH S103 104 P J NO A331 NO PUMP UP PRESS SW C RED NC G10B12 BLK PUMP HYDR MT 301 RED WHT CB322 HYD PUMP POWER CB322A10 25A P 1 1A J TO P328 14 TO 91 31 50 FIGURE 1 SHEET 16...

Page 1708: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 4 Feb 28 07 8H12 91 29 10 THIS PAGE INTENTIONALLY BLANK ...

Page 1709: ...AGE MAINTENANCE MANUAL Surface Deice Optional Figure 1 Sheet 1 of 4 Item Designation Description 1 A318 Timer Assembly 2 A415 A416 Pressure Control Valve 3 A417 A418 A419 De Ice Valve 4 A430 A431 A432 Pressure Switch 5 CB362 Circuit Breaker 5 Amp 6 S319 Switch 1 2 3 4 5 6 ...

Page 1710: ...PAGE 2 Feb 28 07 8H14 91 30 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Surface Deice Optional Figure 1 Sheet 2 of 4 Effectivity 4636001 thru 4636131 ...

Page 1711: ...ING DEICE VALVES 2 1 A419 2 LOWER 1 1 2 A415 D24A20N D24A20 D23A20N G F D23A20 D26E20N D22D20 J D PRESSURE SWITCHES SURFACE DE ICE SWITCH TAIL D20A20 SURFACE DE ICE 5A D29A20N D29B20N D29B20 A432 P304 G F WING UPPER LOWER WING J D D29D20 D29D20N D29C20 D29C20N A431 A430 J402 P304 P402 D29A20 ANNUNCIATOR J416 DEICE PRESSURE CONTROL VALVES A416 1 2 D26F20 D26D20 TO D29E20 A A P392 P392 P394 TO SMART...

Page 1712: ...DE ICE PRESSURE CONTROL VALVE MAIN BUS SURFACE DE ICE SWITCH PRESSURE SWITCHES UPPER WING A431 D29C20N D29C20 LOWER WING A430 D29D20N D29D20 J P CB362A20 5A 6 4 3 5 DE ICE CB362 SURFACE 2D D20A20 P402 P304 F F D22A20 D23B20 D24B20 D25B20 D20B20N J407 1 2 2 1 J408 D25A20 D25A20N D24A20 D24A20N A417 A419 BLK YEL VIOL WH BLU BLU 7 4 6 5 3 A318 TIMER D20B20 D21A20 ORG RED 2 1 311 392 J P P J D22B20 10...

Page 1713: ...PAGE 5 Feb 28 07 8H17 91 30 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1714: ... MAINTENANCE MANUAL Effectivity Ice Detection System SMARTbootsTM Optional 4636132 thru 4636313 Figure 2 Sheet 1 of 2 Item Designation Description 1 CB358 Circuit Breaker 2 Amp 2 De icers with Integral Detectors 3 OAT Sensor 4 Controller 5 A318 Surface De ice Timer 1 5 2 3 4 ...

Page 1715: ... 10 11 7 3 6 5 13 1 2 4 9 13 5 3 4 1 2 9 6 11 7 10 P4 P3 P2 A B C 15 13 10 14 12 11 9 17 8 2 1 16 2 7 6 5 4 3 8 1 P1 P2 P2 P391 1 8 7 3 4 5 6 2 D32A20 CB358 2A ICE DETECTOR RED 4 6 7 13 12 9 10 11 8 14 20 15 16 17 18 5 33 32 31 36 AFT PRESSURE BULKHEAD DN1C22 DN1E22 DN1H22 P329 18 P329 23 P329 31 7 7 4 J311 D20B20N D25B20 WHT P394 1 1 P395 SURFACE DE ICE TIMER SEE SURFACE DEICE T O A N N U N 10123...

Page 1716: ...PAGE 8 Feb 28 07 8H20 91 30 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL GRIDS 8H20 THRU 8H24 INTENTIONALLY BLANK ...

Page 1717: ...t Heat Switch 3 AN5812 Pitot Head Assembly Heated Left and Right Wings with Avidyne Entegra 4 CB360 Circuit Breaker 25 Amp Stall Warn 5 S309 Stall Warn Heat Switch 6 R103 Resistor Heated Stall Warn 7 A101 Lift Transducer 8 S101 Switch Assembly Main Gear Uplock Left 9 K101 Relay Assembly Heated Stall Warning 3 2 5 1 4 6 9 7 8 Pitot and Lift Detector Heat Figure 1 Sheet 1 of 5 ...

Page 1718: ...D1A 14 2 3 VANE P L A T E D3C 20N CASE 9 Ohm 160W 3 J381 P381 J106 P106 3 5 4 D3A 20 6 LEFT UP LOCK SWITCH LEFT WING PRESSURE BULKHEAD LIFT DETECTOR HEAT SWITCH HEAT CONTROL RELAY 16 5 4 D3B 20 D2C 14 D2D 16 FLT GND C D2F 16 A D2E 16 LIFT TRANSDUCER K101 D2A 14 D2B 14 D2G 14N e e P301 P101 J101 J103 P103 CR 309 89801 AH 26 0 S308 S309 R103 A101 S101 Pitot and Lift Detector Heat Figure 1 Sheet 2 of...

Page 1719: ...5 NOTE R103 9 ohms 160 watts 3 P106 J106 D5C18 R103 CURRENT SENSOR WHT C N O N C P390 R390 3 3 J101 2 LIFT D5B18 P301 P101 _ e e 1 R390 1 P390 1 D28A20 ANNUNCIATOR TO AN5812 PITOT MAST D5B18N 18 D2G14N P397 P397 HEAT SWITCH STALL WARN PRESS BLKHD PITOT HEAT P392 P392 SWITCH 7 6 5 4 SHOWN ON GROUND NO POWER 4 _ D1A14 D2A14 D4A18 D5A18 HEAT SWITCH LIFT DETECTOR PITOT HEAT SWITCH S309 S308 2 3 2 3 P3...

Page 1720: ...E AT A 30 SECOND RATE WHEN AIRCRAFT IS ON THE GROUND WITH SWITCH ON PITOT HEAT WILL BE ON CONSTANTLY IN THE AIR WHEN SWITCH IS ON ANNUNCIATOR RELAY WILL TURN ON R PITOT HEAT NOTE IF POWER INPUT IS LOST GB1 C CB361A18 CB361 MAIN BUS 10A HEAT R PITOT P 2G J 2 CB360A18 CB360 MAIN BUS 10A HEAT L PITOT P 2G J 1 18 18 D5B18L e D5C18L P301 P101 J101 2 e 1 D5D18L 118 P J 107 P J 1 D5B18N D5B18R F D5C18R P...

Page 1721: ...R309 D3C20N K101 D3B20 D3A20 FLT GND HEAT CONTROL RELAY 16 STALL WARN HEAT SW CB359A14 MAIN BUS CB359 STALL HEAT 25A 381 P J 2B 1 D1A14 J 1 D2A14 D2B14 P R103 D2D16 D2C14 J D2G14N A101 P J 106 A P 117 C TRANSDUCER LIFT 395 J P 105115 A 33 0 9 OHMS 160W SEE SHEET 4 FOR PITOT HEAT X2 X1 A2 A3 B2 B3 Pitot and Lift Detector Heat Figure 1 Sheet 5 of 5 Effectivity 4636375 and up ...

Page 1722: ...PAGE 6 Feb 28 07 8I6 91 30 30 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1723: ...MAINTENANCE MANUAL Item Designation Description 1 A310 Controller 2 A427 Heated Windshield 3 CB363 Circuit Breaker 5 Amp 4 CB364 Circuit Breaker 25 Amp 5 K314 Controller Relay 6 K322 Heat Relay 7 S320 Heat Switch 2 3 4 1 5 6 7 Heated Windshield Optional Figure 1 Sheet 1 of 4 ...

Page 1724: ...PAGE 2 Feb 28 07 8I8 91 30 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Heated Windshield Optional Figure 1 Sheet 2 of 4 Effectivity 4636001 thru 4636131 ...

Page 1725: ...LER 5 6 7 CB364 D17A20N D16B20 D16G20 HEATED WINDSHIELD 25A D15A12 D15D12 D15B12 D15E12 D16H20N D15C12N D16F20 X2 K322 HI LO A3 A4 A1 X1 A2 CR 322 D16A20N K314 GB5 R P329 21 TO ANNUN HI 316 A2 A1 X2 X1 CR BLK WINDSHIELD HEATED S1 S2 P3 P1 P2 A427 P392 P392 P392 P392 P392 11 12 15 13 14 LO 101238 E 31 0 101301 C 104051 C 104301 NEW S Heated Windshield Optional Figure 1 Sheet 3 of 4 Effectivity 4636...

Page 1726: ... 11 392 14 13 GB5 R D16G20 CB364A12 CB364 7 A310 1 2A J P HEATED WINDSHIELD D15A12 D15C12N LO A4 A2 D16F20 12 X1 CR A1 X2 322 D16A20N LO A3 HI D16H20N K322 S2 S1 K314 X1 X2 A1 A2 CR 316 D15E12 P1 P2 D15B12 D15D12 BLK P3 A427 P J 105115 A 27 0 C O N T R O L L E R HEATED WINDSHIELD CONTROL BLU WHT BLU HEATED WINDSHIELD WSHLD HEAT TO P328 23 91 31 50 FIGURE 1 SHEET 16 Heated Windshield Optional Figur...

Page 1727: ...50P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 A411 Brush Block 2 A428 Timer 3 CB359 Circuit Breaker 15 Amp 4 M303 Ammeter 5 R306 Shunt 6 S318 Switch 7 Prop Heater 8 Slip Ring 7 1 8 6 2 4 5 Propeller Heat Optional Figure 1 Sheet 1 of 5 3 ...

Page 1728: ...IN BUS 2 3 PROP HEAT SWITCH AMMETER D11A 16 D12A 16 P304 J402 P402 1 2 SHUNT PROP HEATER SLIP RING A B C B G TIMER D9A 16 D13A 16N D14A 16N BRUSH BLOCK D8A 16 D8B 16 D6A 16 D7A 16 PROP HEATER e e 3 6 4 5 1 2 7 8 7 89801 AH 32 0 85508 L Propeller Heat Optional Figure 1 Sheet 2 of 5 Effectivity 4636001 thru 4636131 ...

Page 1729: ...T SWITCH P397 D12B22 P401 n P303 J401 k 16 n k 16 D A428 TIMER K7 SHOWN WEIGHT SQUAT SW RELAY 4 8 12 FOR RELAY COIL WIRING SEE 91 21 30 FIGURE 1 J387 P387 1 2 ON WHEELS D14B22 D14A22N p p GB7 L D14C22 C B B A M O V A D13A12N BRUSH BLOCK B A A411 B NOTE EACH BOOT RESISTANCE 4 12 OHMS MIN 4 56 OHMS MAX 4 90 OHMS MAX NOTE EACH BOOT RESISTANCE 4 74 OHMS MIN WIRE SIZE 14 4636132 THRU 4636186 ONLY 10123...

Page 1730: ...ANNUNCIATOR PROP HEAT SWITCH P397 D12B22 P401 n P303 J401 k 16 n k 16 D A428 TIMER K7 SHOWN WEIGHT SQUAT SW RELAY NO 1 4 8 12 FOR RELAY COIL WIRING SEE 91 21 30 FIGURE 1 J387 P387 1 2 ON WHEELS D14B22 D14A22N p p GB7 L D14C22 C B B A M O V A D13A12N BRUSH BLOCK B A A411 B NOTE EACH BOOT RESISTANCE 4 12 OHMS MIN 4 56 OHMS MAX 4 90 OHMS MAX NOTE EACH BOOT RESISTANCE 4 74 OHMS MIN C B D9A12 104301 K ...

Page 1731: ...TE EACH BOOT RESISTANCE 4 56 OHMS MAX 4 12 OHMS MIN SHOWN WEIGHT ON WHEELS 12 K7 4 8 SWITCH PROP HEAT 387 392 2 1 J 18 P GB7 L A D14B22 D13A22 p p j j J401 J P CB358A12 20A 1 D6A12 6 7 PROP HEAT CB358 2C 16 D7A12 16 P401 n n k k P303 A C E B A D7B12 D TIMER A428 F D12A22 395 J P J P D13A12N 105115 A 28 0 PROP DE ICE FAIL TO P329 23 91 31 50 FIGURE 1 SHEET 16 Propeller Heat Optional Figure 1 Sheet ...

Page 1732: ...PAGE 6 Feb 28 07 8I16 91 30 60 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1733: ...IBU MIRAGE MAINTENANCE MANUAL Flight Hour Meter Figure 1 Sheet 1 of 3 Item Designation Description 1 A404 Oil Pressure Switch 2 CB332 Circuit Breaker 3 Amp 3 K7 Squat Switch Relay 4 M310 Flight Hour Meter In S N S 4636375 and up see 91 21 30 Figure 1 Sheet 4 1 2 4 3 ...

Page 1734: ...ER M5D22 CL5A22 TO DIGITAL CLOCK CB332 P E6C20N A404 M6B20 j 13 12 M5B22 HOUR METER M6A22 E6B20 OIL PRESS ANNUN SEE 91 79 30 5 1 3 1 2 M 310 j P402 P304 J402 P387 J387 SQUAT SW RELAY K7 SEE 91 21 30 89801 AF AH 8 0 OIL PRESSURE SWITCH Flight Hour Meter Figure 1 Sheet 2 of 3 Effectivity 4636001 thru 4636020 ...

Page 1735: ...36187 AND UP S N S 4636314 AND UP S N S 4636314 AND UP S N S 4636021 THRU 4636186 ONLY P304 GB3 B J402 P387 J387 K7 3 IN S N S 4636021 THRU 4636131 ONLY 85508 L 8 0 101238 E 101301 C 104051 C 104301 L S 32 32 P402 P304 J402 SQUAT SWITCH RELAY K7 SHOWN WEIGHT ON WHEELS SEE 91 21 30 5 IN S N S 4636021 THRU 4636131 ONLY IN S N S 4636375 AND UP SEE 91 21 30 FIGURE 1 SHEET 4 Flight Hour Meter Figure 1 ...

Page 1736: ...PAGE 4 Feb 28 07 8I20 91 31 30 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL GRIDS 8I20 THRU 8I24 INTENTIONALLY BLANK ...

Page 1737: ... 07 8J1 91 31 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Annunciator Panel Figure 1 Sheet 1 of 16 1 Item Designation Description 1 CB355 Circuit Breaker 3 Amp Effectivity 4636001 thru 4636020 ...

Page 1738: ...DN12M 22 D29E 20 26 20 10 16 26 20 10 16 11 12 36 32 19 24 27 21 19 24 27 21 11 12 36 32 30 31 25 18 30 31 25 18 34 35 34 35 K2 K1 P317 J317 2 31 32 23 22 24 9 6 7 20 8 29 7 20 8 6 9 22 24 31 32 29 23 2 K3 1 2 A F B C D D I M M E R 560 Ohms FOR CONTINUATION SEE NEXT PAGE 3 A ANNUNCIATOR TO TIE BUS 2 A PRESS TO TEST DN1R 22 DN15C 22 DN15D 22N DN1J 22 DN1N 22 DN1H 22 DN1G 22 RP15A 22N DN1A 22 DN1S 2...

Page 1739: ... NIGHT SWITCH 2 3 P6A 20 DN4L 22 DN3L 22 DN2L 22 DN15G 22 DN15H 22 DN15J 22 4 5 6 7 9 1 8 2 3 4 5 6 7 9 1 8 2 3 15 15 17 18 16 17 18 16 8 9 14 13 8 9 14 13 DN15K 22 DN15L 22 DN15F 22 DN6M 22 W2C 22 1 2 3 1 2 3 5 6 11 12 4 10 5 6 11 12 4 10 7 7 DN7M 22 DN1B 22 DN1B 22 DN1B 22 DN1B 22 DN1F 22 DN1C 22 6 7 5 4 3 6 7 5 4 3 P8E20L TO 329 23 P8D20L TO P359 4 P8D20R TO P360 4 P8E20R TO P329 4 K303 K302 K3...

Page 1740: ...PAGE 4 Feb 28 07 8J4 91 31 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Annunciator Panel Figure 1 Sheet 4 of 16 Effectivity 4636021 thru 4636131 ...

Page 1741: ...PAGE 5 Feb 28 07 8J5 91 31 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Annunciator Panel Figure 1 Sheet 5 of 16 Effectivity 4636021 thru 4636131 ...

Page 1742: ...PAGE 6 Feb 28 07 8J6 91 31 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Annunciator Panel Figure 1 Sheet 6 of 16 Effectivity 4636132 thru 4636186 ...

Page 1743: ...PAGE 7 Feb 28 07 8J7 91 31 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Annunciator Panel Figure 1 Sheet 7 of 16 Effectivity 4636132 thru 4636186 ...

Page 1744: ...PAGE 8 Feb 28 07 8J8 91 31 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Annunciator Panel Figure 1 Sheet 8 of 16 Effectivity 4636187 thru 4636247 ...

Page 1745: ...PAGE 9 Feb 28 07 8J9 91 31 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Annunciator Panel Figure 1 Sheet 9 of 16 Effectivity 4636187 thru 4636247 ...

Page 1746: ...A22 91 30 10 18 J329 P329 REQUIRES 28VDC TO TURN LIGHTS ON P329 PINS 7 20 21 24 25 33 FOR CONTINUATION SEE NEXT PAGE 2 1 6 5 5 DN1E22 5 P6B20 SEE 91 24 30 R384 P384 4 4 P6A20 R384 J361 P361 4 3 P384 R384 G2H22 D15G22 DN2L22 D15H22 91 32 60 DN3L22 DAY NIGHT DN1C22 3 3 P384 2 S334 1 G2E22 DN4L22 G2D22 D15J22 2 1 3 9 CR11 CR12 CR13 4 5 6 7 8 CR14 CR15 CR16 CB355 3A DN1B22 ANNUNCIATOR GEAR LANDING DN5...

Page 1747: ...FOR CONTINUATION SEE PREVIOUS PAGE NOTES 2 1 CB355 22 91 30 10 D29E20 OX1A22 D28A20 91 30 30 91 35 10 S2A22 91 27 30 DN1P22 DN1V22 E6A22 91 77 40 34 3 14 5 DN1E22 DN1C22 ANNUNCIATOR 91 30 10 91 30 10 23 31 P329 J329 8 CR32 K2 DN5A22 E7H22 28 E7E22 19 6 7 R329 91 77 20 91 77 20 SEE DME DWG PTT POWER ANNUN INOP PTT DAY NIGHT 24 20 R317 26 91 27 60 SB2A22 91 27 60 SB2B22 FOR CHT SCANNER LIGHTS DIMMIN...

Page 1748: ...40 24 20 21 DN1N22 W22A22 18 J329 P329 P329 PINS 7 20 21 24 25 33 REQUIRES 28VDC TO TURN LIGHTS ON FOR CONTINUATION SEE SHEET 13 OR SHEET 14 2 1 6 5 5 DN1E22 5 P6B20 P384 4 R384 J361 P361 4 3 P384 R384 G2H22 D15G22 DN2L22 D15H22 91 32 60 DN3L22 DAY NIGHT DN1C22 3 3 P384 2 S334 1 G2E22 DN4L22 G2D22 D15J22 2 1 3 9 CR11 CR12 CR13 4 5 6 7 8 CR14 CR15 CR16 CB355 3A DN1B22 ANNUNCIATOR GEAR LANDING DN5A2...

Page 1749: ...OT HEAT OIL PRESS 3A CB355 22 91 30 10 D29E20 OX1A22 D28A20 91 30 30 91 35 10 S2A22 91 27 30 DN1P22 DN1V22 E6A22 34 3 14 5 ANNUNCIATOR 23 31 P329 J329 8 CR32 K2 DN5A22 E7H22 28 E7E22 19 6 7 R329 91 77 20 SEE DME DWG PTT POWER ANNUN INOP 104301 N S 14 1 PTT DAY NIGHT 24 20 R317 26 SB2A22 SB2B22 14 91 27 60 SB2E22 21 ANNUNCIATOR PANEL 1 5 4 3 6 7 2 STBY ATT IND TEST STBY ATT BATT HTR FAIL WITH OPTIO...

Page 1750: ... MANUAL HAS INTERNAL SUPPRESSION FOR CONTINUATION SEE SHEET 12 2 DAY NIGHT K301 11 NOTES 1 7 10 P384 J384 R331 X2 X1 16 SEE AVIONICS COMPASS HARNESS SEE AVIONICS COMM NAV HARNESS 8 9 47K OHMS 104301 E S 14 2 Annunciator Panel Figure 1 Sheet 14 of 16 Effectivity 4636299 and 4636314 4636374 ...

Page 1751: ...PAGE 15 Feb 28 07 8J15 91 31 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1752: ...OP 24 5 P302 U G2D22 5 P301 C 5 P304 Z 4 P317 22 G2H22 G2E22 DN1J22 ANNUNCIATOR LANDING GEAR G2DA22 DN1JA22 D15G22 DN1JC22 D15H22 DN1JB22 G2HA22 D15J22 G2EA22 LEFT NOSE RIGHT 2 K313 A G13C22 18 6 6 P302 H 6 P302 G STBY ATT BTTY WARN IN STBY ATT IND TEST IN K303 K302 CR335 CR334 ALT 1 INOP ALT 2 INOP 15 DN1U22N GB6 L R351 P 384 J 20 19 L PITOT HEAT 3 SPLICE D4C22 3 SPLICE D4B22 3 1 4 B A E C D K J ...

Page 1753: ... SPLICE P303 n 2 12 23 PTT 28 VDC OUTPUT PRP DE ICE FAIL GEAR WARN D12A22 W22A22 P304 k 13 BOOST PUMP Q14C20 P304 C A314 SPLICE 4 8 15 FUEL PRESS DOOR AJAR CABIN ALT Q13C20 W17A22 W6A22 SB2B22 20 P J 317 P304 S 11 E6A22 SPLICE 6 16 OXYGEN STALL WRN FAIL OX1A22 S2A22 P328 OIL PRESS K3 ANNUN INOP CR31 B PTT CR32 B DAY NIGHT 5 4 STBY ATT IND TEST STBY ATT BTTY HTR FAIL STBY ATT BATT HTR FAIL STBY ATT...

Page 1754: ...PAGE 18 Feb 28 07 8J18 91 31 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1755: ...PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 F341 Fuse 2 Amp 5 Amp with Avidyne Entegra Amp in S N s 4636021 thru 4636247 only 2 Resistor 3 Horn 1 2 3 Exceedance Audio Alert Figure 2 Sheet 1 of 3 Effectivity 4636021 and up ...

Page 1756: ...1A22 EG1C22 E8D22 E4E22 Q3A22 E10D22 E15B22 P340 9 18 SEE 91 77 40 FIGURE 3 P338 9 18 SEE 91 77 40 FIGURE 6 P336 9 18 SEE 91 28 40 FIGURE 1 P337 9 18 SEE 91 77 40 FIGURES 5 6 P339 9 SEE 91 77 40 FIGURE 4 RESISTOR 3K 1 2 WATT 85508 L 5 0 101238 E 101301 C 104051 C 104301 NEW S Exceedance Audio Alert Figure 2 Sheet 2 of 3 Effectivity 4636021 thru 4636374 ...

Page 1757: ... MALIBU MIRAGE MAINTENANCE MANUAL Exceedance Audio Alert Figure 2 Sheet 3 of 3 3K 1 2 WATT R306 RESISTOR HORN M306 CB352A20 CB352 MFD 7 5A MAIN BUS 20 RED 2 J 2D P E3M20 20 105115 A 13 0 P530 14 P O AVIONICS HARNESS E3L22 EXCEDANCE HORN Effectivity 4636375 and up ...

Page 1758: ...PAGE 22 Feb 28 07 8J22 91 31 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1759: ...PAGE 23 Feb 28 07 8J23 91 31 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1760: ...PAGE 24 Feb 28 07 8J24 91 31 50 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1761: ...S401 Left Right Main and Nose Gear Up Lock Switch Assembly 3 CB319 Circuit Breaker 3 Amp 4 CB320 Circuit Breaker 3 Amp 5 S342 Gear Selector Switch 6 A305 Dual Warning Horn 7 S103 Squat Switch Assembly 8 S325 Throttle Switch Assembly S N s 4636001 thru 4636374 only 9 S330 Flap Switch 10 S405 MAP Switch S N s 4636375 and up 1 2 2 7 6 9 3 4 1 2 8 5 Landing Gear Position and Warning Figure 1 Sheet 1 o...

Page 1762: ...02 J102 3 1 S102 3 1 G1D22 P201 P302 J201 U U T T G1G20 G2A20 R MAIN P202 J202 3 1 S202 3 1 G2H22 G2E22 G2D22 3 5 7 L N R O M E S A I N N I A M G13C22 SEE 91 29 10 SEE 91 31 50 SWITCHES DOWN LOCK SWITCHES SHOWN GEAR DOWN AND LOCKED P361 INDICATION CB319 LANDING GEAR J361 89801 AH 12 0 85508 L 101238 E 101301 C 104051 C 104301 NEW S Effectivity 4636001 thru 4636374 Landing Gear Position and Warning...

Page 1763: ...G7F20 G3C20 S202 R MAIN S402 5 6 4 NOSE S102 J102 P102 J101 P101 P301 4 6 5 4 6 5 4 5 4 5 W22A22 TO ANNUN P329 33 91 31 50 5 2 3 6 8 9 10 CR 314 5 4 6 G8F22 SELECT GEAR SWITCH UP DN S342 GND CR 320 HORN GEAR A305 G4H22N GB4 F 1 2 7 THROTTLE G 8 C 2 2 G3R22 G8A22 G8D22 G3T22 8 7 1 3 G8B22 G3S22 G3U22 G8E22 J348 P348 P346 J346 P347 J347 FLAP NOTES INDICATES TERMINAL BOARD 301 S P328 18 IN S N S 4636...

Page 1764: ...CK S201 5 4 5 6 4 203 202 P 1 4 3 5 J 2 5 6 3 4 1 DN LOCK S202 R MAIN CP17D20N J402 K P304 M L H p Z G2G20 G2F20 K L Z H p M P402 G3L20 G2K20 G2J20 G4B20 G1H20 G2B20 H F Y K CP17B22 S2H22 G11A20 G11D20 M H K Y F M G11C20 G11B20 CP17C20 S3H20N S3H20 G5A20 410 403 P P 1 5 4 2 1 3 J J 3 5 6 2 3 2 4 1 1 UP LOCK DN LOCK S401 NOSE 2 2 5 4 9 7 12 10 5 6 8 9 11 12 4 7 10 6 SQUAT S103 C U D P E G G E D P C...

Page 1765: ...PAGE 5 Feb 28 07 8K5 91 32 60 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1766: ...PAGE 6 Feb 28 07 8K6 91 32 60 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL GRIDS 8K6 THRU 8L24 INTENTIONALLY BLANK ...

Page 1767: ...PART NUMBER 761 876 February 28 2007 9A1 AIRPLANE MAINTENANCE MANUAL CARD 9 OF 9 PA 46 350P S N s 4636001 AND UP PIPER AIRCRAFT INC ...

Page 1768: ...9A2 Published by Technical Publications Piper Aircraft Inc 2926 Piper Drive Vero Beach Florida 32960 U S A Member General Aviation Manufacturers Association ...

Page 1769: ...2 3 4 5 and 6 CR981223 December 23 1998 1 2 3 4 5 and 6 PR000201 February 1 2000 1 2 3 4 5 and 6 PR010515 May 15 2001 1 CR050730 July 30 2005 1 2 3 4 5 6 7 and 8 PR060207 February 7 2006 1 2 3 4 5 6 7 and 8 CR070228 February 28 2007 1 2 3 4 5 6 7 8 and 9 COMPLETE REVISION OF MAINTENANCE MANUAL 761 876 Revisions appear in all Aerofiche Cards Accordingly discard your entire existing Aerofiche Card S...

Page 1770: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 1 Feb 28 07 AEROFICHE EFFECTIVITY 9A4 THIS PAGE INTENTIONALLY BLANK ...

Page 1771: ...Feb 28 07 Intro Table of Contents 1 Feb 28 07 2 Feb 28 07 Introduction 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11 Feb 28 07 12 Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 Index 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 CHA...

Page 1772: ...PAGE 2 Feb 28 07 INTRO LIST OF EFFECTIVE PAGES 9A6 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1773: ...A9 Effectivity 2 9A10 Serial Number Explanation 2 9A10 Assignment of Subject Material 2 9A10 Pagination 3 9A11 Aerofiche Effectivity 3 9A11 Identifying Revised Material 3 9A11 Indexing 3 9A11 List of Effective Pages 3 9A11 Warnings Cautions and Notes 3 9A11 Accident Incident Reporting 4 9A12 Supplementary Publications 4 9A12 Piper Publications 4 9A12 Vendor Publications 4 9A12 Chapter Section Inde...

Page 1774: ...PAGE 2 Feb 28 07 9A8 INTRO CONTENTS PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1775: ...GENUINE PIPER AIRCRAFT PARTS OR PIPER AIRCRAFT APPROVED PARTS OBTAINED FROM PIPER APPROVED SOURCES IN CONNECTION WITH THE MAINTENANCE AND REPAIR OF PIPER AIRPLANES Genuine PIPER parts are produced and inspected under rigorous procedures to ensure airworthiness and suitability for use in PIPER airplane applications Parts purchased from sources other than PIPER even though identical in appearance ma...

Page 1776: ...ane are broken down into subsystems These sub systems are identified by the second element of the standard numbering system The element 40 of the number 28 40 01 concerns itself with the indicating section of the fuel system C Unit Subject The individual units within a sub system section may be identified by the third element of the standard numbering system The element 01 of the number 28 40 01 i...

Page 1777: ...his set 8 Identifying Revised Material A revision to a page is defined as any change to the printed matter that existed previously Revisions additions and deletions are identified by a vertical line i e change bar along the left hand margin of the page opposite only that portion of the printed matter that was changed A change bar in the left hand margin opposite the footer i e chapter section subj...

Page 1778: ...s Catalog P N 761 878 2 Periodic Inspection Report Form P N 767 011 3 Progressive Inspection Manual 50 hour P N 767 013 B Vendor Publications WARNING FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION S WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT MAY RENDER THE AIRCRAFT UNAIRWORTHY 1 AIR CONDITIONING COMPRESSOR Vendor Address Sanden International USA Inc PH 972 442 8400...

Page 1779: ...cialty Systems PH 330 374 3040 Goodrich Corporation FAX 330 374 2290 1555 Corporate Woods Parkway Uniontown Ohio 44685 8799 Technical Assistance PH 800 334 2377 330 374 3743 FAX 330 374 2290 Email dssd support goodrich com http www deicingsystems goodrich com Black Standard Pneumatic De Icer Installation Maintenance and Repair Manual ATA 30 10 31 SmartBoot System ATA 30 10 65 8 ELECTRONIC FLIGHT I...

Page 1780: ...ntext See www avantext com or PH 800 998 8857 11 FIRE EXTINGUISHER PORTABLE Vendor Address H3R Inc PH 800 249 4289 43 Magnolia Ave 4 San Francisco California 94123 2911 http www h3r com index htm 12 FORCE APPLICATOR KIT Vendor Address Safe Flight Instrument Corp PH 914 946 9500 20 New King Street White Plains New York 10602 13 FUEL BOOST PUMP Vendor Address Parker Hannifin Corp PH 800 272 7537 Nic...

Page 1781: ...ww unisonindustries com index4 html Installation Operation F1100 MASTER SERVICE MANUAL and Maintenance 4300 6300 SERIES MAGNETO MAINTENANCE AND Instructions OVERHAUL MANUAL L 1363 19 NAVIGATION COMMUNICATIONS AND GPS NAV COM GPS Vendor Address Garmin International PH 913 397 8200 1200 East 151ST Street Olathe KS 66062 http www garmin com 20 OXYGEN SYSTEM Vendor Address Scott Aviation PH 716 683 51...

Page 1782: ...DAR WEATHER RDR 2000 Vendor Address Honeywell Bendix King See Autoflight above Maintenance Manual Bendix King ART 2000 P N 006 05332 0001 25 RADIO COOLING BLOWER Vendor Address Globe Motors PH 937 228 3171 2275 Stanley Ave FAX 937 229 8531 Dayton Ohio 45404 http www globe motors com home html 26 STARTER Vendor Address Kelly Aerospace See Alternator above or Sky Tec Partners Ltd PH 800 476 7896 350...

Page 1783: ...MALIBU MIRAGE MAINTENANCE MANUAL 28 VACUUM PUMP Vendor Address Aero Accessories Inc PH 800 822 3200 1240 Springwood Avenue Gibsonville NC 27249 http www aeroaccessories com index html 29 VACUUM REGULATORS Vendor Address Parker Hannifin Corp see Fuel Boost Pump above ...

Page 1784: ...PAGE 10 Feb 28 07 INTRODUCTION 9A18 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1785: ...chapter CHAPTER SECTION TITLE GRID NO 4 AIRWORTHINESS LIMITATIONS 1C1 00 Airworthiness Limitations 5 TIME LIMITS MAINTENANCE CHECKS 1C9 00 General 10 Time Limits 20 Scheduled Maintenance Checks 30 Special Inspections 50 Unscheduled Maintenance Checks 6 DIMENSIONS AND AREAS 1E13 00 General 7 LIFTING AND SHORING 1F1 10 Jacking 8 LEVELING AND WEIGHING 1F9 10 Weighing and Balancing 20 Leveling 9 TOWIN...

Page 1786: ...emperature Control 22 AUTOFLIGHT 2F11 10 Autopilot 23 COMMUNICATIONS 2G19 00 General 50 Audio Integrating 60 Static Discharging 24 ELECTRICAL POWER 2H11 00 General 30 DC Generation 40 External Power 60 Electrical Load Distribution 25 EQUIPMENT FURNISHINGS 2J11 10 Flight Compartment 20 Passenger Compartment 50 Cargo Compartments 60 Emergency 26 FIRE PROTECTION 2K15 20 Extinguishing 27 FLIGHT CONTRO...

Page 1787: ...rs 60 Propellers Rotors 31 INDICATING RECORDING SYSTEMS 4C1 50 Central Warning Systems 32 LANDING GEAR 4C13 00 General 10 Main Gear and Doors 20 Nose Gear and Doors 30 Extension and Retraction 40 Wheels and Brakes 50 Steering 60 Position and Warning 33 LIGHTS 4G5 10 Flight Compartment 20 Passenger Compartment 30 Cargo and Service Compartments 40 Exterior 34 NAVIGATION 5C1 00 General 10 Flight Envi...

Page 1788: ...00 General 10 Investigation Cleanup and Aerodynamic Smoothness 70 Repairs 80 Electrical Bonding 52 DOORS 6G13 10 Passenger Crew 20 Emergency Exit 30 Cargo 70 Monitoring and Operation 55 STABILIZERS 6H13 00 General 10 Horizontal Stabilizers 20 Elevator 30 Vertical Stabilizer 40 Rudder 56 WINDOWS 6I19 00 General 10 Flight Compartment 20 Cabin 30 Door 57 WINGS 6K5 40 Attach Fittings 50 Flight Surface...

Page 1789: ... Power Supply 20 Distribution 76 ENGINE CONTROLS 7G17 10 Power Control 77 ENGINE INDICATING 7H3 10 Power 20 Temperature 40 Integrated Engine Instrument Systems 79 OIL 7J3 20 Distribution 30 Indicating 80 STARTING 7J15 10 Cranking 81 TURBINES 7K9 20 Turbo Supercharger 91 CHARTS WIRING DIAGRAMS 8C1 10 Charts 21 and up Electrical Schematics 91 CONT CHARTS WIRING DIAGRAMS CONT 9C1 Electrical Schematic...

Page 1790: ...PAGE 16 Feb 28 07 INTRODUCTION 9A24 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1791: ...sion Control Wing 6L3 Attitude Indicator 5D5 Autopilot 2F17 Component Locator 2G2 Installation 2F18 2F20 Maintenance 2F23 Operational Checkout 2F24 Pitch Servo 2G12 Pressure Transducer 2G6 Roll Servo 2G4 Servo Clutch Torque Adjustment 2G15 Trim Monitor 2G3 Trim Servo 2G6 Yaw Amplifier 2G14 Yaw Servo 2G10 Avionics Cooling 2C14 Avionics Master Switch 2H1 B Ball Diameters for Testing Hose Restriction...

Page 1792: ...rrection 2I10 Troubleshooting 2I7 2I13 Valve Regulated Lead Acid 2I13 Bonding 6G9 Resistance Index 6G10 Buses Avionics 2H19 Main 2H19 Circuit Breaker Panel 6D22 Electrical Shelf 6E7 External Power 2I19 Load Distribution 2J1 Relay Installation Co Pilot s Side 6E10 K1 thru K8 6E10 Pilot s Side 6E9 Schematics Air Conditioning 8E7 Airspeed Standby 9E19 Altimeter Radar 9F14 Altimeter Standby 9E19 Annun...

Page 1793: ...n Light 9E5 WX 500 9F11 XM Receiver 8E23 Switch Panels 6E1 Symbols 8D14 System 2H17 Troubleshooting 2H20 Tie Bus Panel Connections 6E3 Volt Ammeter 2J4 Voltage Regulation and Control 2H19 Wire Coding 8D13 Elevator Balancing 6I3 Control System Installation 3D23 Rigging and Adjustment 3D24 Troubleshooting 3D19 Torque Tube Bearing Changes 3D20 Trim Controls Actuator Assembly 3E3 Corrosion Control 3E4...

Page 1794: ...Drain Valve 3G8 Draining 1I19 Draining Moisture 1I18 Fuel Filter 3G7 Fuel Pumps Specifications 3G5 Fuel Quantity Gauge Accuracy Test 3G14 Full Range Check 3G20 Senders 3G13 Leak Test Setup 3G1 Selector Switch and Valve 3G6 Cable Adjustment 3G7 Troubleshooting 3F16 Leak Evaluation 3F22 G GMA 340 Audio Panel Adjustments 2H6 Installation 2H3 System Functional Test 2H4 GNS 430 5F5 GNS 530 5F5 Ground C...

Page 1795: ... 4D11 Position and Warning 4F19 Landing Gear Up Power Reduced Warning Switch Adjustment 4G2 Troubleshooting 4F20 Leading Particulars and Principal Dimensions 1E20 Leveling 1F17 Life Limited Parts 1C7 Lifting 1F7 See also 57 40 00 Lights Exterior 4H3 Landing 4H7 Position 4H4 Pulse 4H7 Strobe 4H3 Taxi 4H6 Wing Inspection Light 4H7 Interior 4G11 Annunciator Panel 4G12 Baggage Area 4G21 Forward 4H1 Re...

Page 1796: ...g 3K6 Troubleshooting 3J20 Propeller Assembly 7C9 Publications Piper A12 Vendor A12 Q Quad Digital Indicator QDI See Engine Instruments Transicoil EMIS R Radar 5F1 Repairs Fiberglass 6F19 Metal Wire Stitching 6G5 Thermoplastic 6F21 List of Materials 6F24 Window Windshield Acrylic 6J10 Restraint System 2J23 Inertial Reel Adjustment 2J23 Inspection 2J23 Revised Material A11 Robinair 34700 Charging S...

Page 1797: ... Bellcrank Centering 4C22 Horn Arm Gap 4C22 Nose Wheel Centering 3C15 4C22 Rudder Pedal Neutral Alignment 3C15 4C22 Rudder Travel Tool 3C15 Torque Conversion 8C20 Torque Wrench Formula 1K2 Towing 1G5 Transponder 5F9 GTX 327 5F9 GTX 330 5F9 Post Installation Setup Procedure 5F10 ARINC 429 Configuration Page 5F11 Display Mode and Key Lighting 5F11 Hexadecimal Conversion 5F13 Operation Configuration ...

Page 1798: ...in 6I11 Vertical Speed Indicator 5C18 Volt Ammeter See Electrical W Warnings Cautions and Notes A11 Weather Radar 5F1 Weighing 1F15 Wheel Brake Assembly 4F4 Wheels Bearing Cup 4F4 Main Wheel Assembly 4F2 Nose Wheel Assembly 4F1 Repairs 4F3 Windows and Windshields Door Window 6K3 Heated Windshield Testing 3J15 Troubleshooting 3J15 Inspection and Repair Definitions 6J1 Limitations 6J1 Crack Limitati...

Page 1799: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 9 Feb 28 07 INDEX 9B9 THIS PAGE INTENTIONALLY BLANK ...

Page 1800: ...PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL PAGE 10 Feb 28 07 INDEX 9B10 GRIDS 9B10 THRU 9B24 INTENTIONALLY BLANK ...

Page 1801: ...9C1 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL CHAPTER 91 CHARTS WIRING DIAGRAMS Continued ...

Page 1802: ...9C2 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1803: ...Feb 28 07 13 Feb 28 07 14 Feb 28 07 15 Feb 28 07 16 Feb 28 07 17 Feb 28 07 18 Feb 28 07 CHAPTER SECTION PAGE DATE 91 Cont List of 1 Feb 28 07 Effective Pages 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 91 Cont 1 Feb 28 07 Table of Contents 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 91 33 10 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 9 Feb 28 07 10 Feb 28 07 11...

Page 1804: ...b 28 07 19 Feb 28 07 20 Feb 28 07 21 Feb 28 07 22 Feb 28 07 23 Feb 28 07 24 Feb 28 07 25 Feb 28 07 26 Feb 28 07 91 79 30 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 CHAPTER 91 Continued LIST OF EFFECTIVE PAGES CHAPTER SECTION PAGE DATE 91 34 40 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 07 5 Feb 28 07 6 Feb 28 07 7 Feb 28 07 8 Feb 28 07 91 34 50 1 Feb 28 07 2 Feb 28 07 3 Feb 28 07 4 Feb 28 0...

Page 1805: ...PAGE 3 Feb 28 07 9C5 91 CONT LOE PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1806: ...PAGE 4 Feb 28 07 91 CONT LOE 9C6 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1807: ...7330 9G18 ATA Code Grid No 7420 9G20 7710 9H2 7720 9H4 7740 9H14 7930 9I18 Subject Grid No Air Conditioning 8E7 Airspeed Standby 9E19 Altimeter Radar 9F14 Altimeter Standby 9E19 Annunciator 8J1 Attitude Indicator Standby 9E19 Autopilot 9E23 9F2 Autopilot 55X 8E14 Avionics Cooling 8D19 Avionics Dimming 9D7 Avionics Lighting 9D7 Baggage Compartment Lights 9D15 C B Panel Lights 9C15 Cabin Heater 8E3 ...

Page 1808: ... GMA 340 8F2 GNS 430 9F2 9F17 Ground Blocks 8F20 Ground Clearance 8E17 GTX 330 9F3 9F22 Hour Meter 8I17 Hydraulic Pump 8H9 Subject Grid No Ice Detection System 8H18 Ice Light 9E5 IHAS Integrated Hazard Alert System 9F12 Instrument Panel Switch Lights 9C23 Junction Blocks 8F22 KMC 850 9F12 KMH 820 9F12 KN 63 9F24 KPA 900 9F10 KR 87 9G1 KRA 10A 9F14 Landing Gear Position and Warning 8K1 Landing Ligh...

Page 1809: ...ope 9F11 Strobe Lights 9D19 Summing Amp 8F4 9F12 9F14 Tachometer 9H2 9H19 9I13 Tail Light Optional 9D22 9E1 Taxi Lights 9E9 TIT Indicator 9H4 9I1 9I13 Turn Coordinator s 9E16 Vacuum Indicator 9I5 9I13 Vacuum Low Indicator 9G14 Vent Blowers 8E7 Vent Defogger 8E3 Weather Radar 9F9 Wing Inspection Light 9E5 WX 500 9F11 XM Receiver 8E23 NOTE Card 8 grid numbers above may be erroneous if Card 8 has bee...

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Page 1811: ...91 33 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL 1 2 Map Lights Figure 1 Sheet 1 of 3 Item Designation Description 1 CB329 Circuit Breaker 3 Amp CB331 in S N s 4636314 and up 2 XDS308 XDS309 Map Light ...

Page 1812: ...NUAL WHITE BLACK WHITE L50E 22 L50C 22 L50F 22 L50G 22N L50A 22 MAP LIGHT 3 A 75 Ohm 25 Watt P326 J326 P324 J324 MAIN BUS L50D 22 2 1 2 1 BLACK 2 1 L50H 22 L50K 22 L50J 22 P325 J325 XDS 309 XDS 308 GB4 L 1 R327 89801 AH 23 0 Map Lights Figure 1 Sheet 2 of 3 Effectivity 4636001 thru 4636020 ...

Page 1813: ...LK WHT J324 P324 1 2 XDS309 XDS308 85508 L 23 0 101238 E 101301 C 104051 C 104301 NEW S 105115 A 18 0 MAP LIGHT NON ESS BUS 3A CB331 CB331A22 1E 12 P J S N S 4636375 AND UP WITH AVIDYNE ENTEGRA CB331 IN S N S 4636314 AND UP 324 1 L50G22N GB4 L J 2 1 BLK WHT P XDS308 L50A22 2 325 P J 326 2 1 J BLK WHT P XDS309 Map Lights Figure 1 Sheet 3 of 3 Effectivity 4636021 and up ...

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Page 1815: ...E 5 Feb 28 07 9C15 91 33 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 A338 Inverter 1 Electroluminescent Panel Lighting C B Panels Figure 2 Sheet 1 of 3 ...

Page 1816: ... L41B22 L41C22 L41E22 L41D22 L42F22 2 P375 1 2 L42H22 L42G22 P372 P373 P374 1 1 2 1 2 L42D22 L42E22 L42C22 L42B22 L42A22 L42J22 L42H22N L41J22 L41H22N L40H22N L40J22 J363 2 1 BLK E L PANELS INVERTER A338 BLK L40K22 P363 GB2 H GB4 B LEFT AFT PANELS LEFT FWD PANELS RIGHT PANELS RED IN S N S 4636001 THRU 4636131 ONLY 89801 AH 44 0 85508 L 101238 E 43 0 101301 C 104051 C 104301 NEW S Electroluminescen...

Page 1817: ... FWD C0 PILOT SIDE WHT BLK BLK WHT WHT BLK BLK WHT WHT BLK BLK WHT BLK WHT WHT BLK BLK WHT L42B22N L42A22 L41B22N L41A22 J L40A22 L40B22N 8 7 P 1F J 6 5 P 1F GB4 C L41K22 L41L22N GB2 H L42L22N L42K22 TO LB1 G 363 2 L43J22 L43K22 1 P BLK 115AC TO 28VDC BLK A338 INVERTER E L PANELS J 105115 A 14 2 Electroluminescent Panel Lighting C B Panels Figure 2 Sheet 3 of 3 Effectivity 4636375 and up ...

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Page 1819: ...ER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 A302 Dimmer Control 2 R301 Panel Light Dimmer Rheostat 3 CB354 Circuit Breaker 5 Amp Post Light Assembly 1 2 3 Post Lights Figure 3 Sheet 1 of 4 ...

Page 1820: ...G REOSTAT GB2 E L23C 20 L23D 20 L40K 22 CL4A 20 TO DIGITAL CLOCK 91 25 10 FIGURE 2 TO EL PANELS FIGURE 2 P385 J385 PILOT S INSTRUMENT PANEL L H SIDE CENTER INSTRUMENT PANEL PILOT S INSTRUMENT PANEL R H SIDE CO PILOT S INSTRUMENT PANEL TO DIGITAL T I T 91 77 20 FIGURE 1 TAPER BLOCK TB1 O A T L23N 22 TO ENGINE COMBUSTION ANALIZER 2 1 2 1 WHITE BLACK L30A 20 TO SWITCH LIGHT DIMMER OPTIONAL OXYGEN GAU...

Page 1821: ...4 E3H22 SEE 91 77 40 FIGURES 1 2 L40K22 TO EL PANELS L23D20 L23C20 L23G20 L23F20 TAPER BLOCK P315 GB2 E A302 DIMMER TB1 L23M22 L23M22 COMPASS LIGHT GB2 P PILOT INSTR PNL R H SIDE CENTER INSTR PNL CO PILOT INSTR PNL PILOT INSTR PNL L H SIDE BEZEL LIGHTING L23N20 L23N20N SEE FIGURE 2 INSTR PANEL LIGHTS 5A CB354 L30A20 LIGHTS DIMMER TO SWITCH SEE FIGURE 4 S N S 4636132 UP ONLY 85508 L 20 0 101238 E 1...

Page 1822: ...0 L20A20 L24A22N B C P306 V R301 V L21A22 2 V 1 V V 5K L43K22 RP116A22 TO K10 2 3 TO P393 5 1 L28B22 C L23D20 L23E20 K A L D E F G J H B PILOT POST LIGHTS COPILOT POST LIGHTS M 105115 A 14 1 3 TO 91 34 20 FIGURE 2 SHEET 2 1 TO 91 27 50 FIGURE 1 SHEET 3 2 TO 91 33 10 FIGURE 2 SHEET 3 NOTES 4 TO 91 33 10 FIGURE 4 SHEET 7 Post Lights Figure 3 Sheet 4 of 4 Effectivity 4636375 and up ...

Page 1823: ...PER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 A329 Dimmer Control 2 R309 Panel Light Dimmer Rheostat 3 CB354 Circuit Breaker 5 Amp 1 2 3 Instrument Panel Switch Lights Figure 4 Sheet 1 of 7 ...

Page 1824: ...D HEAT PROP HEAT SURF DEICE L33A 20 GB2 F GB6 H RADIO MASTER AVIONICS L28D 22N L33A 20 L28C 22 AVIONICS ELT GND CL REFER TO GROUND CLEARANCE SWITCH SCHEMATIC RP7E 22 L23L 22 GB6 A GB6 B GB6 C CABIN HEAT AIR COND FAN VENT DEFOG LDG LT TAXI LT STROBE LT NAV LT DAY DIM MAG L MAG R BATT MAST ALT 1 ALT 2 EMERG FUEL PUMP CABIN PRESSURE STARTER L23H 22N L23J 22N L23K 22N L23J 22 L23K 22 L23H 22 TO PANEL ...

Page 1825: ...PAGE 15 Feb 28 07 9D1 91 33 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Instrument Panel Switch Lights Figure 4 Sheet 3 of 7 Effectivity 4636021 thru 4636131 ...

Page 1826: ...PAGE 16 Feb 28 07 9D2 91 33 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Instrument Panel Switch Lights Figure 4 Sheet 4 of 7 Effectivity 4636132 thru 4636247 ...

Page 1827: ...AG R STARTER MASTER BATTERY ALT 2 ALT 1 FUEL PUMP MAG L L23P22 WHT 1 1 2 P387 P387 TAXI LT LDG LT STROBE LT NAV LT DAY NIGHT 1 2 GB2 F 5k 2 1 BLK 2 TO POST LIGHTS DIMMER SEE FIGURE 3 D I M M E R L35A20 P392 20 L23S20 21 P392 TO SW PANEL 19 D4K20N GB5 E R387 R387 INSTR PANEL LIGHTS IND DITIGAL RESET 388 P J 104051 C 19 0 Instrument Panel Switch Lights Figure 4 Sheet 5 of 7 Effectivity 4636248 thru ...

Page 1828: ...L L23P22 WHT 1 1 2 P387 P387 TAXI LT LDG LT STROBE LT NAV LT DAY NIGHT 1 2 GB2 F 5k 2 1 BLK 2 TO POST LIGHTS DIMMER SEE FIGURE 3 D I M M E R L35A20 P392 20 L23S20 21 P392 TO SW PANEL 19 D4K20N GB5 E R387 R387 INSTR PANEL LIGHTS 388 P J RESET IND DIGITAL L23T22 P365 8 9 P365 RADIO MASTER GND CLEARANCE 8 P366 9 P366 L23U22N GB7 R INSTALLED WITH EFIS OPTION ONLY TO SWITCH PANEL ON INSTR PANEL Effecti...

Page 1829: ...8 A C 5K CW V R309 V V 2 VV 1 ALT 2 LANDG LT TAXI LT BLK WHT J 379 2 1 P WHT BLK GB7 R STROBE LT NAV LT CABIN PRESS NIGHT DAY L23U22N L23T22 MAIN BUS TO P306 A 1 INSTR PNL CB354A20 CB354 5A LIGHTS P 2D J 4 L20A20 SWITCH PANEL L35A20 D4K20N GB2 C 19 20 21 ASSY P392 L23Y22 TO P317 19 2 L23V22 L23W22N MFD PFD 2 PFD 1 LB4 J K A E D B C H G 105115 A 14 0 20 L23Z22 TO P317 28 2 1 TO 91 33 10 FIGURE 3 SH...

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Page 1831: ... 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 A301 Dimmer Control 2 R302 Panel Light Dimmer Rheostat 3 CB356 Circuit Breaker 3 Amp 1 2 3 Avionics Lighting Figure 5 Sheet 1 of 3 ...

Page 1832: ...22 L26A22 B F D A C AVIONICS CB356 DIMMING 3A DIMMER A301 GB2 D R302 5K 2 1 CW BLOCK TAPER TB2 89801 AH 36 0 85508 L 101238 E 101301 C 104051 C 104301 NEW S L28B20 L28C20 TO FLAP INDICATOR TO VOLT AMP METER 91 24 30 FIGURE 2 S N S 4636299 AND 4636314 UP Avionics Lighting Figure 5 Sheet 2 of 3 Effectivity 4636001 thru 4636374 ...

Page 1833: ...02 1 V VV VV CW 5K B F C A D L27A22 L28A20 L25A20 L26A22 L29A22N DIMMER A301 TRANSPONDER 1 TRANSPONDER 2 ADF RECEIVER DME GNS 430 1 GNS 430 2 GMA 340 AUDIO RAD ALT GI 106A AUTOPILOT IHAS ANNUN TRIM MONITOR AVIONICS LIGHTS DIMMER H J G F L M K B A E D C H J G F L K E D C B A M 105115 A 17 0 105130 A 30 0 L28D20 Avionics Lighting Figure 5 Sheet 3 of 3 Effectivity 4636375 and up ...

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Page 1835: ...PAGE 1 Feb 28 07 9D11 91 33 20 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL 1 Cabin Lights Figure 1 Sheet 1 of 3 Item Designation Description 1 CB337 Circuit Breaker 5 Amp ...

Page 1836: ...40 1 2 2 1 P356 1 2 2 1 L16N 22 L16P 22N P341 1 2 2 1 L15F 22 L15D 22 P352 P339 P353 1 2 2 1 1 2 2 1 1 1 2 2 P338 P350 L16D 22N L15E 22 L16F 22 L16H 22N 1 2 2 1 L16E 22 L16G 22N 2 2 1 1 L16B 22 L16L 22N 2 2 5A CB337 L15B 22 89801 AH 22 0 85508 L 101238 E 101301 C 104051 C 104301 NEW S Cabin Lights Figure 1 Sheet 2 of 3 Effectivity 4636001 thru 4636374 ...

Page 1837: ...ESS BUS L15F22 L16L22N L16J22 337 1 P354 2 P 1E 13 CB337A22 J J L15A22 L15C22 1 2 P340 L15B22 P L16F22 L16H22N L16N22 L16P22N 1 P341 2 P356 1 2 P353 1 2 CABIN L15E22 L16D22N L16B22 2 1 P350 L15D22 1 2 P338 L16G22N L16E22 1 P339 2 1 2 P352 105115 A 16 0 1 Cabin Lights Figure 1 Sheet 3 of 3 Effectivity 4636375 and up ...

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Page 1839: ...MANUAL Item Designation Description 1 A323 Timer 2 Baggage Compartment Light Assembly 3 Courtesy Light Assembly 4 S352 Timer Reset Switch 5 Cabin Door Lock Switch 6 S403 Baggage Door Switch 7 F407 Fuse 5A 2 3 6 1 5 4 7 Courtesy Lights Baggage Compartments Door Cabin Figure 2 Sheet 1 of 3 ...

Page 1840: ...GAGE DOOR SWITCH SHOWN WITH DOORS OPEN NOTE 2 1 2 1 L60K 20 L60A 20 L60C 20 22 22 22 22 RED WHITE BLACK P345 J345 W17D 20N L16P 22 L16R 22 L16S 22 L16V 22N L16U 22N L16T 22N L60B 20 L60F 20 W17C 20 28 V GND LOAD F407 D D ENTRANCE DOOR AFT BAGGAGE COMPARTMENT FORWARD CABIN 1 2 2 1 2 2 1 1 2 2 1 1 TO 91 52 70 89801 AH 21 0 85508 L 101238 E 101301 C 104051 C 104301 NEW S 2 1 Courtesy Lights Baggage C...

Page 1841: ...COMPARTMENT L60K20 LIGHTS BAGGAGE LIGHT P F407 BTTY BUS J401 S403 DOOR SWITCH FWD BAGGAGE SHOWN DOOR OPEN L60F20 J 413 2 1 P J 1 2 417 W17C20 L60B20 b D L60A20 P401 W17D20N 2 1 L60C20 W17B22 P303 b D J W17D22 SWITCH S352 TO P329 4 DOOR S326 S327 22 22 P W17A22 J P 332 22 WHT BLK RED A323 TIMER 344 J 22 P TIMER RESET LOCK SWITCH CABIN DOOR W17F22 W17E22 J 316 P 105115 A 15 0 1 TO 91 31 50 FIGURE 1 ...

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Page 1843: ...MANUAL Item Designation Description 1 CB344 CB345 Circuit Breaker 5 Amp 2 S303 S304 Nav Strobe Lights Switch 3 XDS 202 XDS 203 Nav Strobe Light Right 4 XDS 102 XDS 103 Nav Strobe Light Left 5 A103 A201 Strobe Light Power Supply 1 2 5 3 5 4 Position and Strobe Lights Figure 1 Sheet 1 of 6 ...

Page 1844: ...3 1 1 WHITE WH ORG P302 P201 J201 WH BLU J209 P209 4 4 L9C 18N L2D 18 RIGHT POSITION LIGHT 3 2 2 3 1 1 WHITE WH ORG P301 P101 J101 WH BLU J109 P109 4 4 L9B 18N L5D 18 3 2 2 3 1 1 WHITE WH ORG PWR SUP 1 2 3 1 2 3 P110 P111 RIGHT STROBE LIGHT P302 P201 J201 WH BLU J209 P209 4 4 L9C 18N L5D 18 3 2 2 3 1 1 WHITE WH ORG PWR SUP 1 2 3 1 2 3 P210 P211 2 3 2 Z c a a Z c c c Z Z a a c c Z Z a a Z c a a Z c...

Page 1845: ...1 P101 J109 P109 P302 J201 P201 J209 P209 1 SWITCH S304 R386 P386 CB344 5A L1A18 1 R386 2 L1B18 1 P386 3 L2A18 1 S303 J201 P201 2 2 L2B18 Z c P302 a L2E18 L9C18N Z c WH ORG WH BLU a WHITE 2 3 J209 P209 1 4 L2D18 RIGHT POS N XDS 203 XDS 202 LIGHTS POSITION NAV LTS SWITCH c a J101 P101 Z c a L2C18 P301 L9B18N Z WH BLU WH ORG WHITE 1 2 3 L2D18 J109 P109 4 POS N LEFT XDS 102 _ _ _ _ _ _ _ _ _ _ _ _ _ ...

Page 1846: ...P209 J209 L5D18 4 3 2 1 L9B18N WHITE WH ORG WH BLU Z P109 J109 L5D18 4 3 2 1 STROBE RIGHT A201 P211 P210 SUPPLY POWER 3 2 1 3 2 1 203 XDS LEFT STROBE A103 P111 P110 SUPPLY POWER 3 2 1 3 2 1 XDS 102 L5H20 2 3 1 FIN FLASHING LIGHT FIN 104301 NEW S 17 0 1 1 L5F18 L5G18 L5J20N OVERHEAD SW PANEL AUTOPILOT CONN IN AFT PRESSURE BULKHD LIGHT ASSY t t 1 1 2 2 3 3 L5K20N L5L20 430 P J P431 Effectivity 46362...

Page 1847: ...8 P101 J101 a c P201 J201 P302 L2E18 a c Z L2B18 2 2 R386 P301 L2C18 a c Z J209 L9C18N WHITE a WH BLU WH ORG c Z 4 1 3 2 L9B18N WHITE WH ORG WH BLU Z 4 P109 J109 L2D18 3 2 1 P209 RIGHT XDS 203 LEFT 102 XDS AUTOPILOT CONNECTOR IN AFT PRESSURE BULKHEAD _ _ g L2F18 g L2G18 TAIL LIGHT L2D18 2 3 OPTIONAL Position and Strobe Lights Figure 1 Sheet 5 of 6 Effectivity 4636299 and 4636314 thru 4636374 ...

Page 1848: ...S WHT ORG WHT BLU WHT ORG WHT BLU 5A S303 5A MAIN BUS 7 5A J P L2B18 L1A18 CB347 L2A18 L1B18 CB347A18 3 L4A18 1 2 J 2F P 4 L8A18 STROBE LIGHTS CB344A18 CB345A18 CB345 TAXI LIGHTS 1 J 2F P 2 L5C18 L2C18 L9D18 L9C18 L2E18 P201 P302 Z Z c c J101 Z a c P301 P101 Z a c WHT POSITION LIGHTS CB344 2F LEFT STROBE POSITION LIGHTS WHT POS WHT POS 1 XDS101 RIGHT TAXI LIGHT L9B18N 3 2 P 212 1 2 J 2 3 4 1 109 J...

Page 1849: ...RAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 CB344 Circuit Breaker 5 Amp 2 S303 Nav Lights Switch In S N s 4636299 and 4636314 up see Figure 1 Sheets 5 and 6 1 2 Tail Light Optional Figure 2 Sheet 1 of 3 ...

Page 1850: ...TS NAV LT SW 3 2 MAIN BUS L1A 18 g g L2F 18 L2G 18 AUTOPILOT CONNECTOR IN AFT PRESSURE BULKHEAD TAIL LIGHT 5A CB344 S303 89801 AH 17 1 When this option is installed Wire L2A18 see Figure 1 is disconnected from NAV LIGHT Switch Post 3 Tail Light Optional Figure 2 Sheet 2 of 3 Effectivity 4636001 thru 4636020 ...

Page 1851: ...2G18 LIGHT TAIL AUTOPILOT CONNECTOR IN AFT PRESSURE BULKHEAD _ _ POSITION 5A CB344 LIGHTS L1A18 L1B18 P386 1 R386 1 S 303 SWITCH NAV LTS 3 2 R386 2 L2A18 2 P386 L2B18 L2E18 L2C18 85508 L 17 1 101238 E 101301 C 104051 C Tail Light Optional Figure 2 Sheet 3 of 3 Effectivity 4636021 thru 4636313 less 4636299 ...

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Page 1853: ...40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 XDS307 Ice Light 2 S324 Ice Light Switch 3 CB348 Circuit Breaker 3 Amp 3 2 1 Wing Inspection Ice Light Optional Figure 3 Sheet 1 of 3 ...

Page 1854: ...PAGE 12 Feb 28 07 9E6 91 33 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Wing Inspection Ice Light Optional Figure 3 Sheet 2 of 3 Effectivity 4636001 thru 4636131 ...

Page 1855: ... P349 J349 L66B22N XDS307 ICE LIGHT IN LEFT SIDE OF FUSELAGE GB6 P P392 P392 16 17 101238 E 24 0 101301 C 104051 C 104301 NEW S ICE LIGHT MAIN BUS 3A 1E CB348 CB348A22 15 P J 105115 A 18 0 S N S 4636375 AND UP WITH AVIDYNE ENTEGRA SWITCH ICE LIGHT 17 16 L65A22 392 J P Wing Inspection Ice Light Optional Figure 3 Sheet 3 of 3 Effectivity 4636132 and up ...

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Page 1857: ...ing Light 2 K5 Landing Light Relay 3 S401 Nose Gear Up Lock Switch 4 S302 Landing Light Switch 5 CB346 Circuit Breaker 10 Amp 6 XDS101 XDS201 Taxi Lights 7 S301 Taxi Lights Switch 8 CB 347 Circuit Breaker 7 5 Amp In S N s 4636375 and up see Figure 1 Sheet 6 for Taxi Lights 1 2 3 6 6 4 7 Landing and Taxi Lights Figure 4 Sheet 1 of 5 5 8 ...

Page 1858: ...J209 XDS101 LEFT XDS201 RIGHT c c c a a a Z Z Z WHITE WHITE WH BLU WH ORG 2 3 G2G22 G2K20 G2J20 P402 J402 NOSE UP LOCK SWITCH 6 5 4 6 4 5 P304 L12A18N XDS401 P402 J402 P304 L10B18 L10C18 5 3 B LANDING LIGHT RELAY K5 3 4 5 6 P387 J387 L10A18 G2F22 L11B22 L10B22N GB4 P LANDING LIGHT SWITCH LANDING LIGHT 10A NOSE GEAR ASSY LANDING LIGHT CB346 S302 S401 PILOT S AFT CB PANEL M a p a M p A CR 5 1 J403 P...

Page 1859: ...PAGE 17 Feb 28 07 9E11 91 33 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Landing and Taxi Lights Figure 4 Sheet 3 of 5 Effectivity 4636021 thru 4636131 ...

Page 1860: ...209 P209 P304 P402 J402 TAXI LEFT P112 J112 J212 P212 2 1 RIGHT XDS201 6 5 3 4 G2F22 L11B22 L10B22N L10B18 L11C22 2 3 P384 2 2 R384 R384 1 1 P384 L12A22 a a L10C18 XDS201 L12A18N GEAR ASSY NOSE LANDING LIGHT G2G22 LANDING LIGHT SWITCH G2J20 G2K20 5 J403 P403 4 GB4 P LIGHT RELAY LANDING 5 A B CR5 K5 3 P304 P402 J402 1 5 4 6 S401 SWITCH NOSE UP LOCK P387 1 2 R343 RED GRN L8C18 L8F18 ASSY FLASHER 1 2...

Page 1861: ...T SW 3 CB346A18 CB346 LIGHT 2F J P L10A18 L11C22 G2F20 S384 LANDING 2 3 375 2 J L11B20 P P304 M p a G2K20 G2J20 P402 M p a 5 6 GEAR UP GEAR DOWN P 1 2 403 J 4 S401 L10C18 LANDING LIGHT RELAY 18 4 20 20 L10B18 3 6 5 18 3 J402 387 P J 1 5 NOSE GEAR ASSY L12A18N XDS201 105115 A 18 0 SEE FIGURE 1 SHEET 6 FOR TAXI LIGHTS 18 18 Landing and Taxi Lights Figure 4 Sheet 5 of 5 Effectivity 4636375 and up ...

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Page 1863: ...PAGE 1 Feb 28 07 9E15 91 34 20 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1864: ...6 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 Pilot s Turn Coordinator Standard Copilot s Turn Coordinator Optional 2 CB318 CB336 Circuit Breaker 3 Amp CB317 in 4636001 thru 4636131 only 1 2 Turn Coordinator s Figure 1 Sheet 1 of 2 ...

Page 1865: ...COORDINATOR PILOT S FWD CB PANEL GB4 E F2A 22N A B C CO PILOT S TURN COORD F3A 22 CO PILOT S TURN COORDINATOR PILOT S FWD CB PANEL GB2 B F4A 22N A B C P307 P306 OPTIONAL 89801 AH 38 0 85508 L 101238 E 101301 C 104051 C 104301 NEW S 3A CB317 3A CB336 CB318 IN S N S 4636001 THRU 4636131 ONLY IN S N 4636248 AND UP SEE AUTOPILOT C I P FOR PILOT S TURN COORDINATOR WIRING ...

Page 1866: ...RAGE MAINTENANCE MANUAL Standby Instruments Figure 2 Sheet 1 of 2 Item Designation Description 1 CB341 Circuit Breaker 3 Amp 2 CB342 Circuit Breaker 7 5 Amp 3 K 1 Lighting Relay 4 S356 Standby Gyro Switch 5 PS 834A Power Supply Effectivity 4636375 and up 1 2 3 3 5 4 1 2 4 ...

Page 1867: ...4A20N RP103A20 RP105B20 RP106B22 RP107B22 RP108B22 RP109B22 RP118A20N RP111B22N RP111D22N RP111C22N RP112A20N RP113A20N RP110D22 RP110C22 RP110A22 RP110B22 RP117A20 2 1 LIGHTING LIGHTING MAG COMPASS RP119A22N 1 2 RP115A20N RP101A22 RP116A22 GB5 P GB5 M GB5 N GB5 K GB6 D GB5 F GB4 H RP114A22 RP105C20 RP102A20 28VDC POWER 24 28VDC OUT ON OFF CONTROL REMOTE TEST IN REMOTE TEST LAMP REMOTE WARN LAMP G...

Page 1868: ...CE MANUAL Item Designation Description 1 S TEC 6446 Flux Sensor 2 ADAHRS Select Relay 3 Meggitt 37002 01 02 ADAHRS Unit 4 ADAHRS Select Switch 5 Meggitt 84 133 5 PFD Unit 6 Meggitt 84 134 5 ND Unit Electronic Flight Instrument System EFIS Meggitt Figure 3 Sheet 1 of 5 1 2 3 4 5 6 4 5 6 ...

Page 1869: ...00 INSTR PANEL EFIS SWITCH SW 1 15 1 12 6 2 9 5 17 16 13 14 3 8 7 10 11 4 PRESSURE BULKHEAD DISC FLUX VALVE 6 1 4 5 14 2 3 13 12 9 16 22 WH TYP 2 1 8 10 7 6 3 7 15 17 8 11 HARNESS ASSY DETAIL A EFIS LIGHT DIM 2 1 5K N C SEE DETAIL A L7A20 L7B20N L7C20 L7D20 L7E20 1 2 A D B C F 104291 M Electronic Flight Instrument System EFIS Meggitt Figure 3 Sheet 2 of 5 ...

Page 1870: ...9 OUT1 SHIELD GROUND 429 IN4A SHIELD GROUND 429 IN4B BUS B 429 IN4B BUS A CONFIGURE RETURN 429 IN2 BUS A 429 IN2 BUS B 429 IN2 SHIELD GROUND 429 OUT1 BUS A 429 OUT1 B BUS 429 IN4B SHIELD GROUND 429 IN4A B BUS 429 IN4A A BUS CONFIGURE 7 1 2 29 11 28 27 10 12 31 30 21 25 9 10 11 29 28 27 9 6 6 24 20 22 23 35 17 20 1 5 17 5 2 21 3 22 4 23 35 3 4 422 BUS A CONFIGURE 4 CONFIGURE RETURN CONFIGURE 1 CONF...

Page 1871: ...K 22BLK 22BLK 22BLK 20BLK 20BLK 20BLK 20R EADI SKYWATCH ADAHRS 1 A P SWITCH REV DISC F D 3 ADF1 DME ADF1 DME METRIC FIGURE 1 CONFIGURATION WITH VARIOUS OPTIONS SELECTED 22 23 24 21 25 9 9 20 15 16 17 18 19 10 11 13 14 3 4 5 6 7 8 1 2 28 9 27 26 3 5 4 6 8 7 1 2 8 7 2 1 3 6 4 5 5 1 2 3 2 3 1 23 7 10 31 11 12 30 29 28 9 27 10 31 11 30 12 29 9 28 27 10 31 11 12 30 29 28 9 27 10 31 29 30 12 11 27 9 28 ...

Page 1872: ...32 33 35 4 7 15 6 13 5 9 11 3 2 1 9 31 20 19 3 4 8 9 14 15 16 13 AIRSPEED WARN CONN GND CHASSIS GND W1B22 W1E22 W1A22 ALT B4 PARITY CONFIG RETURN 28VDC RETURN SIG Z SIG Y SIG X EXC HI EXD LO 28VDC POWER 28VDC RETURN SHIELD GROUND ALT RETURN ALT D4 SHIELD GROUND ALT C4 ALT C2 ALT C1 SHIELD GROUND 28VDC POWER A D B E F C DME SEL SW2 ALT A2 ALT A1 CONN GND ALT B2 ALT B1 SHIELD GROUND ALT A4 DME SEL S...

Page 1873: ...PAGE 11 Feb 28 07 9F1 91 34 20 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1874: ...DN G S UP W B INSTRUMENT PANEL P7322 PFD 2 CO PILOT GNS 430 2 P43012 CH 0 TX A CH 0 TX B 22 21 CH 0 TX A CH 0 TX B 22 21 GPS ARINC 429 IN 1B GPS ARINC 429 IN 1A GPS ARINC 429 IN 2A GPS ARINC 429 IN 2B 50 51 GPS ARINC 429 IN 2A GPS ARINC 429 IN 2B 51 GNS 430 1 GPS ARINC 429 IN 1B GPS ARINC 429 IN 1A 50 P43011 DISCRET INPUT 12 14 JB5 C SEE JB5 D SEE JB5 A SEE JB5 B SEE ARINC 429 CH 4 RX A ARINC 429 ...

Page 1875: ... 16 AWG RED 28VDC INPUT GND MAG OAT 422 RX B CH_ID1 CH_ID2 CH_ID0 GND SEE SEE SEE SEE GB2A H SEE GB2A D L H INST PNL SEE 16 AWG RED P2E 1 P3D 1 R H INST PNL 16 AWG RED TAIL DISCONNECT PFD 1 PILOT MAG OAT 422 TX MAG OAT PWR GND MAG OAT 24VDC OUT MAG OAT 422 TX W B W B W B W B JB RACK CENTER ARINC 429 CH 7 TX A ARINC 429 CH 7 TX B INSTRUMENT PANEL CIRCUIT BREAKER PANEL GTX 330 TRANSPONDER ARINC 429 ...

Page 1876: ...8 D8 D7 SHIELD GROUND PITCH STR ROLL STR GROUND SIG REF 35 28 29 30 15 55X AUTOPILOT GROUND SIG REF 42 12 7 ROLL STR P552 13 PITCH STR 55X AUTOPILOT P552 72 DISCRETE INPUT 11 9 1 8 GND BYTEFLIGHT BYTEFLIGHT DISCRETE INPUT 14 DISCRETE INPUT 13 53 34 ADAHRS 2 SELECT ADAHRS 1 SELECT INSTRUMENT PANEL 55X AUTOPILOT P552 4 FD LOGIC 55X AUTOPILOT 24 ANNUN LOAD P552 25 26 ANNUN CLK ANNUN DATA 50 30 11 50 ...

Page 1877: ...B W CH_ID1 PFD 2 CO PILOT MAG OAT 24VDC OUT MAG OAT PWR GND MAG OAT 422 TX B W B W TAIL DISCONNECT GB3A M SEE LB4 K SEE SH28 GB3A J 16 AWG RED 28VDC INPUT 16 AWG BLACK 16 AWG RED 28VDC INPUT GND BEZEL DIMMING 16 AWG BLACK A4 GND SEE SEE P2E 2 P3D 3 SEE SEE 16 AWG RED R H INST PNL 16 AWG RED L H INST PNL CIRCUIT BREAKER PANEL DETAIL C MTA106D SWITCH COPILOT PFD CONTROL INHIBIT 13 CONTROL INHIBIT SW...

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Page 1879: ...C 429 CH 3 RX A 8 28 JB6 N SEE JB6 J SEE 20 AWG RED 28 VDC 40 GND GND 28 VDC 60 61 42 28 VDC 41 GND LIGHTING 62 18 20 AWG BLK MFD P530 INSTRUMENT PANEL DISC OUT 1 14 JB RACK CENTER EXCEEDANCE REF ALERT HORN RC 1 2G302JT 3K 1 2 WATT P2D 2 INSTRUMENT PANEL CIRCUIT BREAKER PANEL 20 GA JUMPER 20 GA RED JUMPER 36 GB3 N SEE E3L22 EXCEEDANCE HORN 22BLK 22BLK 22RED 22RED LB4 J SEE 22BLK 22RED 2 REQ D E3M2...

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Page 1881: ... AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 IN 182A or MFD Radar Indicator 2 ART 2000 Radar Antenna Transceiver Radar Antenna Array Configuration Module 1 2 Weather Radar Figure 1 Sheet 1 of 2 ...

Page 1882: ... 2 CHIP SELECT 1 CONFIG DATA RX MODULE GND 45 48 44 47 46 49 50 28V DC AIRCRAFT POWER 28V DC AIRCRAFT POWER DC AIRCRAFT PWR CHAS GND WEATHER RADAR RDR 2000 P5001 B W 024 0064 00 CABLE RADAR POD W B 1 R T ON OFF 67 78 75 453 CH 0 RX A 453 CH 0 RX B 453 GND P530 TO P7321 67 91 34 20 FIG 4 B W TO P7321 68 91 34 20 FIG 4 64 63 43 MFD LS ARINC 429 TX1 B LS ARINC 429 TX1 A 429 GND CONFIGURATION MODULE P...

Page 1883: ...TEST Y LOOP ANT COM ANT_REF 12 V STORMSCOPE ANTENNA X LOOP SENSE 12 V F J G A H DRAIN BLUE GREEN YELLOW BLACK C P5004 B D ORANGE BROWN RED 20 RS 232 TX P5003 WX 500 STORMSCOPE GND 14 28 VDC P5001 1 6 5 9 20BLK AFT EQUIPMENT SHELF 20RED 51 49 P530 50 MFD RS232 C TX RS232 C RX RS232 C GND P3C 4 20RED CIRCUIT BREAKER PANEL INSTRUMENT PANEL WHT BLU ORG 20BLK 20BLK 20RED 2 GB5A B SEE 105130 B F 21 BFG ...

Page 1884: ... TERM RDY DIAG RS232 RX DIAG RS232 TX DIAG RS232 READY 41 40 39 38 SERIAL DATA OUT 10 1 EGPWS DIAG PORT 2 P8203 RD 5 SG 3 TD SERIAL DATA IN SERIAL DATA OUT KCM 850 7 CONFIGURATION MODULE CLK CS 8 9 2 1 3 VCC 5VDC CHIP SELECT CLOCK GND 5 4 SERIAL DATA IN 6 DTR TD RD 4 2 3 SG 5 CTS 8 28V DC AIRCRAFT PWR 28V DC AIRCRAFT PWR TRAFFIC TERRAIN DC AIRCRAFT PWR CHAS GND DC AIRCRAFT PWR CHAS GND P10 KMH 820...

Page 1885: ...N CTL UNIT TERR AWRN ANNUN TERR CAUTION ANNUN TERR N A ANNUN P411 11 5 10 JB6 P SEE JB6 K SEE B W JB3 C SEE AV1E22 INSTRUMENT PANEL CIRCUIT BREAKER PANEL 23 2 FUNCTIONAL TEST TAS STANDBY 4 3 1 2 5 6 W B B W W B 27 SHIELD 24 26 59 56 P530 6 SHIELD MFD LS ARINC 429 CH 2 TX B LS ARINC 429 CH 2 TX A ARINC 453 CH 1 RX B ARINC 453 CH 1 RX A 95 96 GPWS CTL 429 RX A GPWS CTL 429 RX B GPWS DATA 453 TX A GP...

Page 1886: ...DE SELF TEST RAD ALT LO 20VDC 2 9 7 12 5 P1001 6 28VDC FILTERED 4 22 BLU 1 LIGHT COMMEN 20 VDC 2 10 ANALOG ALTITUDE 5 RAD ALT LO SELF TEST 9 KI 250 RADAR ALT INDICATOR P3C 3 20 RED 20 RED P2501 CIRCUIT BREAKER PANEL 7 DH AUDIO HI RAD ALT IN 20 BLK SUMMING AMP 7 AUD1 SHIELD 8 RAD ALT SW 105130 B F 24 REFERENCE DRAWING 91 24 30 FIG 3 91 24 30 FIG 4 91 24 30 FIG 5 KRA 10A Radar Altimeter Figure 4 Eff...

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Page 1888: ...PAGE 8 Feb 28 07 9F16 91 34 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1889: ... Description 1 Garmin GNS 430 Global Navigation System 2 Garmin GI 106 Course Deviation NAV Indicator 3 NAV Antenna Coupler 4 GPS 1 Antenna i e left side GPS 2 Antenna i e right side 5 COM 1 Antenna 6 COM 2 Antenna 7 NAV Antenna 1 2 4 6 7 3 5 GNS 430 COM NAV GPS Figure 1 Sheet 1 of 4 Effectivity 4636375 and up ...

Page 1890: ...46 P317 12 P317 1 CROSSFILL CROSSFILL 42 41 CROSSFILL CROSSFILL GNS430 2 P43012 GB2A J SEE GB2A K SEE INSTRUMENT PANEL 22 GA RED JUMPER 18 GA RED JUMPER W B B W B W P43022 P3301 ARINC 429 CH 1 RX B ARINC 429 CH 1 RX A GTX 330 TRANSPONDER 1 P7321 LS ARINC 429 CH 1 RX B LS ARINC 429 CH 1 RX A MFD P530 DC COUPLER XMTR PTT P501 5 25 35 32 12 COMM 1 MIC KEY COMM 2 MIC KEY 30 5 VOR ILS ARINC 429 OUT A 2...

Page 1891: ...GH 15 14 13 NAV 2 AUDIO HIGH NAV 2 AUDIO LOW 19 20 COM 2 CIRCUIT BREAKER PANEL 18RED P3A 2 P3B 4 NAV COMM GPS 2 GNS 430 P43012 GB4A D SEE GB4A C SEE INSTRUMENT PANEL B W 22 RED 18 RED P7322 PFD 1 43 42 CH 3 RX A CH 3 RX B LS ARINC 429 CH 2 RX A LS ARINC 429 CH 2 RX B 65 45 P530 MFD W B 7 6 CH 4 RX A CH 4 RX B PFD 2 CH 3 RX B CH 3 RX A 42 43 VOR ILS ARINC 429 OUT A VOR ILS ARINC 429 OUT B 24 23 W B...

Page 1892: ...AL FLAG LATERAL FLAG RIGHT 8 12 7 SEE GB1A B BLU WHT WHT BLU GRN ORG WHT WHT BLU WHT BLU BLU SEE LB2 G SEE GB1A A 22BLK 20RED 22BLK 22BLU 18 UP DOWN OBS RES G OBS RES F VERTICAL FLAG LEFT VERTICAL FLAG 13 14 6 4 16 15 OBS RES C OBS RES H TO FROM OBS RES E OBS RES D 1 9 10 3 5 2 28 VDC ANNUN POWER VLOC ANNUNCIATOR 28 VDC PANEL LAMPS PANEL LAMPS GROUND 20 21 22 P1061 NAV INDICATOR GI 106A GPS N 1 TO...

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Page 1894: ... 61 60 JB5 F SEE JB5 E SEE KMH 820 P10 CIRCUIT BREAKER PANEL B W W B GB2A P SEE 15 16 46 14 31 17 27 43 21 12 42 1 P O P554 28 30 ANTENNA AUDIO OUT HI TIS SELECT DIM SUPPRESSION SQUAT SWITCH PWR GROUND PWR GROUND CW8H22 22BLK 22BLK 28VDC PWR EXT IDENT 28VDC PWR AVIONICS MASTER ON CW7H22 22RED 22RED 22RED 20RED ARINC 429 TX ARINC 429 TX AUDIO OUT LO 105130 B F 19 REFERENCE DRAWING 91 24 30 FIG 3 91...

Page 1895: ...5 B W JB6 A SEE JB6 E SEE 16 15 13 14 31 17 43 27 12 42 21 1 P O P554 31 17 43 27 12 42 21 1 14 13 46 15 16 30 28 35 32 46 60 61 XP 1 2 JB5 N SEE JB5 K SEE JB5 G SEE JB5 H SEE 30 28 33 ARINC 429 CH7 RX A AUDIO OUT HI ANTENNA 2 STANDBY ALERT 36 DIM SQUAT SWITCH CW8H22 CW7H22 PWR GROUND PWR GROUND EXT IDENT 22 BLK 22 BLK 28VDC PWR 28VDC PWR AVIONICS MASTER ON 22 RED 22 RED 22 RED 22 RED 22 RED 22 RE...

Page 1896: ... 33 21 14 20 P43061 39 42 40 43 22 P43062 2 GNS 430 SUPPRESSION 192 V AUDIO LO AUDIO HI DATA BUS GROUND HOLD 9 25 V ON CLOCK BUS K 10 N C F 12 6 E 9 11 A IN A IN GROUND GROUND KN 63 3 2 A 1 P631 15 2 x 5 0 1 MHZ A 2 x 5 0 1 MHZ E 2 x 5 0 1 MHZ D 2 x 5 0 1 MHZ C 2 x 5 1 MHZ D 2 x 5 1 MHZ E 2 x 5 1 MHZ C 2 x 5 1 MHZ A BLK BRO RED ORG YEL GRE BLU GRY VIO WHT 39 38 35 20 41 43 42 48 44 37 NAV 1 COMMON...

Page 1897: ... MOUNT ANT GROUND AUDIO OUT LOOP ENABLE ANT PWR WHITE RED WHITE GREEN WHITE 12 8 6 32HZ 90 R 10 D H M E P 20 BLK B A 9 22BLU 28VDC PWR PWR GND 13 S 20RED 20BLK P871 32HZ 0 WHITE ORANGE RF OUTPUT INNER SHIELD OUTER SHIELD 3 TRIAXAL CABLE 8 WHITE BLUE 7 5 GROUND 9 LOOP ENABLE 32HZ 90 WHITE GREEN WHITE RED WHITE P441 1 2 ANT PWR 4 200 02586 0003 E C B H A P2271 4 5V COMMON A C GND DC SIN OUT 28V LIGH...

Page 1898: ...P MALIBU MIRAGE MAINTENANCE MANUAL DC 50 ANT COUPLER 28 VDC ACFT PWR 1 ACFT GND 8 SEE GB1A P P501 CIRCUIT BREAKER PANEL 20RED 20BLK P3A 3 105130 B F 26 REFERENCE DRAWING 91 24 30 FIG 3 91 24 30 FIG 4 91 24 30 FIG 5 DC Coupler Figure 5 Effectivity 4636375 and up ...

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Page 1900: ...PAGE 1 Feb 28 07 9G10 91 35 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Oxygen System Optional Figure 1 Sheet 1 of 2 Item Designation Description 1 S335 S336 S337 Switch 3 each 1 ...

Page 1901: ...XYGEN BOTTLE 1 J322 P322 P321 OX3A22 OX2A22 OX1C22 OX3D22N OX2D22N OX1F22N OX1A22 OX1B22 TO ANNUNCIATOR P329 34 GB6 K GB6 J GB6 H SWITCHES SHOWN IN ARMED POSITION OXYGEN BOTTLE 2 OXYGEN BOTTLE 3 P329 18 IN S N S 4636001 THRU 4636131 ONLY P329 6 WITH AVIDYNE ENTEGRA 89801 AH 40 0 85508 L 101238 E 101301 C 104051 C 104301 NEW S 105115 A 30 0 OX2B22 OX2C22 OX1D22 OX1E22 IN S N S 4636075 AND UP WITH A...

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Page 1903: ...PAGE 1 Feb 28 07 9G13 91 37 20 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1904: ...AGE 2 Feb 28 07 9G14 91 37 20 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description Information Pending See Parts Catalog Vacuum Low Indicator Figure 1 Sheet 1 of 2 ...

Page 1905: ...0C20 D30B20 D30G20 D30H20 P L P L M M N N P401 P401 P303 P303 D30J20N D30F20 D30A20 D30D20N TO ANNUNCIATOR P329 15 TO ANNUNCIATOR P329 16 GB5 C GB5 J P329 6 IN S N S 4636021 THRU 4636131 ONLY P328 16 WITH AVIDYNE ENTEGRA SEE 91 31 50 FIGURE 1 P329 8 IN S N S 4636021 THRU 4636131 ONLY P328 21 WITH AVIDYNE ENTEGRA SEE 91 31 50 FIGURE 1 85508 L 27 0 101238 E 101301 C 104051 C 104301 NEW S 105115 A 24...

Page 1906: ...16 91 52 70 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Door Ajar Warning Figure 1 Sheet 1 of 2 Item Designation Description 1 S403 Nose Baggage Door Switch 2 S326 S327 Door Ajar Switch Lower Upper 2 1 ...

Page 1907: ...TS b b P401 J401 P303 W17B22 W17A22 TO ANNUNCIATOR P329 32 W17E22 W17F22 2 1 J316 P316 S326 DOOR LOWER SWITCH AJAR AJAR DOOR UPPER SWITCH S327 SWITCHES SHOWN NORMALLY CLOSED WITH DOORS OPEN W17D22 P329 21 IN S N S 4636001 THRU 4636131 ONLY P329 4 IN S N S 4636375 AND UP 89801 AH 16 0 85508 L 101238 E 101301 C 104051 C 104301 NEW S 105115 A 15 0 b b S N S 4636132 THRU 4636374 IN S N S 4636375 AND U...

Page 1908: ...LIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 A413 Flow Transducer 2 M308 Manifold Pressure and Fuel Flow Gauge 3 CB313 Circuit Breaker 3 Amp 4 M306 Fuel Flow Totalizer 5 CB324 Circuit Breaker 5 Amp 3 5 1 2 4 Fuel Flow Gauge s Figure 1 Sheet 1 of 2 ...

Page 1909: ...6 2 4 A F H D L B GR5 D E16A 22N MANIFOLD PRESSURE AND FUEL FLOW GAUGE 2 P310 9 1 GR5 C GND 28V dc FUEL MGT 5A PILOT S FWD CB PANEL 5 DN8B 22 26 26 J317 P317 E15A 22 VENDOR SUPPLIED HARNESS INTERFACE TO ENGINE MANIFOLD U V W P P W V U FUEL FLOW POWER L TXD SIG L TXD GND L TXD SIG L TXD GND SDA SDB BRIGHTNESS R328 39K 1 4 W 2 10 K2 DAY NIGHT RELAY SEE ALSO 91 31 50 K2 89801 AH 6 0 CA301 CA401 Fuel ...

Page 1910: ...U MIRAGE MAINTENANCE MANUAL Item Designation Description 1 CB334 Circuit Breaker 5 Amp 2 F410 Fuse 2 Amp 3 K404 Starter Contactor 4 Start Relay 5 S311 L S312 R Magneto Switch 6 Start Switch 7 A336 Vibrator 5 6 1 2 3 4 7 Engine Start and Ignition Figure 1 Sheet 1 of 4 ...

Page 1911: ... 18 K2B 20 K2A 18 J1C 20 J3D 18N J2A 18N J3E 18N J1D 18N STARTER CONTACTOR K404 R LR L GB3 R IN A336 BO VIBRATOR 2 2 1 MAG SWITCHES GB5 N GB5 P J1A 18 W2B 20 FUSE 2A BUS BAR TO BATTERY CONTACTOR TO ANNUNCIATOR P329 12 MAIN BUS START 5A START SWITCH J3C 18 1 16 17 18 19 11 6 12 7 13 8 14 9 T C T C X X i i c f c f Y Y g g ON ON OFF OFF J4A 18N 2 3 7 6 1 5 5 89801 AH 3 0 LEFT RIGHT Engine Start and I...

Page 1912: ...VIBRATOR BO IN R389 6 P389 6 7 7 J1D20 J1C20 2 3 4 J1C18 J1B18 L MAG SWITCH C C P303 P401 J401 T T W2B20 START RELAY K3A20 CR403 BUS BAR TO BATTERY CONTACTOR W2A20 K4A4 CONTACTOR STARTER B401 STARTER K4B4N K404 F410 2A J3D18 P389 R389 f c _ _ J402 P304 P402 J6A18 J1A18 1 J6B18N R L J402 X P304 _ i P402 J401 Y P402 P304 g _ 4 382 2 3 J3B18 J3C18 J3G18 J4A18 J3A18 SWITCH 2 R MAG 1 J5A18 1 P382 J5B18...

Page 1913: ...2 X f c J1D18N LR J3E18N 4 TO EXT PWR CONTACTOR SEE 91 24 30 FIGURE 1 SHEET 7 J402 J401 4 3 2 J1C18 J1D18 361 P J6A18 1 J1B18 J J6B18N g Y C T P303 i W2C22 K3B20 J4B18 380 P 2 1 J GB7 J 6 CB334A20 K5A20 J3D18 K5D20 J3F18N J1D20 VIBRATOR J3A18 W2A20 CONTACTOR STARTER K4A4 K404 J4A18 P401 g Y C T i K3A20 W2B20 CR404 F410 STARTER RIGHT MAG R B401 K4B4N 8 P329 10 SEE 91 31 50 FIGURE 1 SHEET 16 7 3 5 J...

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Page 1915: ...PAGE 1 Feb 28 07 9H1 91 77 10 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1916: ...RAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 M304 Tachometer Indicator 2 Magneto Sensor 3 CB314 Circuit Breaker 3 Amp 2 1 3 RPM Indicator Tachometer Figure 1 Sheet 1 of 2 Effectivity 4636001 thru 4636020 ...

Page 1917: ...BLK RED BLU LEFT MAGNETO SENSOR WHITE WHT BLU WHT ORG WHITE WHT BLU WHT ORG TACHOMETER INDICATOR A D B C E TACHOMETER 3A GB4N E8A 22 PILOT S FWD CB PANEL P401 P303 J401 1 2 3 P308 2 4 1 CA 402 CA 302 G H J K K J H G 89801 AH 5 0 RPM Indicator Tachometer Figure 1 Sheet 2 of 2 Effectivity 4636001 thru 4636020 ...

Page 1918: ...MIRAGE MAINTENANCE MANUAL Item Designation Description 1 M307 Turbine Inlet Temperature Indicator 2 A403 Turbine Inlet Temperature Probe 3 CB315 Circuit Breaker 3 Amp 4 1 2 3 Effectivity 4636001 thru 4636020 Turbine Inlet Temperature TIT Indicator Figure 1 Sheet 1 of 2 ...

Page 1919: ...URBINE INLET TEMPERATURE INDICATOR 8 OHMS 2 F S ANALOG DIGITAL TURBINE INLET TEMPERATURE INDICATOR 8 OHMS 2 F S PROBE YELLOW CHROMEL A 403 FEED THROUGH PRESSURE BULKHEAD RED ALUMEL YELLOW CHROMEL 2 YELLOW CHROMEL A 403 FEED THROUGH PRESSURE BULKHEAD RED ALUMEL YELLOW CHROMEL 2 TO ENGINE GAUGES SEE 91 79 30 E1A 22 RED ALUMEL PROBE 89801 AH 7 0 STANDARD OPTIONAL Turbine Inlet Temperature TIT Indicat...

Page 1920: ...PER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL 1 Item Designation Description 1 CB316 Circuit Breaker 1 5 Amp 2 M309 Combustion Analyzer Combustion Analyzer Optional Figure 2 Sheet 1 of 2 Effectivity 4636001 thru 4636020 ...

Page 1921: ...0 23 6 19 13 18 12 17 BLK YEL BLK YEL BLK YEL BLK YEL BLK YEL BLK BLK WHT 2 1 1 5A ENGINE MONITOR MAIN BUS PRESSURE BULKHEAD CHT 1 CHT 2 CHT 3 CHT 4 CHT 5 CHT 6 YELLOW BLACK GB3 L J385 P364 TO POST LIGHTS P385 REFER TO 91 33 10 WHT BLK 2 1 89801 AH 43 0 Combustion Analyzer Optional Figure 2 Sheet 2 of 2 Effectivity 4636001 thru 4636020 ...

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Page 1923: ... 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 CB312 Circuit Breaker 1 5 Amp 2 K2 Day Night Relay 3 R329 Resistor 4 S353 Cycle Control Switch 5 Scanner 5 1 4 CHT Scanner Figure 3 Sheet 1 of 3 2 Effectivity 4636001 thru 4636374 ...

Page 1924: ...B20 E7E22 3 5 17 E7N22 20 21 24 E7L22 E7K22 E7M22 19 25 10 E7C22 E7P22 E7D22N 1 E7H22 J 19 28 P 317 E7F22 E7G22 6 8 E7R22N 9 CYCLE CONTROL GB4 D S353 6 1 5 4 3 2 1 5 3 2 4 220ohm 1 2 W K2 RELAY DAY NIGHT 309 7 P J 3 11 7 R329 TO P337 24 CHT GAUGE S N S 4636021 THRU 4636131 ONLY 89801 AH 43 1 85508 L 43 0 GB3 K TO P319 D 3 UNIT ENGINE GAUGE IN S N S 4636001 THRU 4636020 ONLY CB316 IN S N S 4636001 ...

Page 1925: ... 21 8 2 11 E9F20 E9B20 E7E22 3 5 27 E7N22 28 30 29 E7L22 E7K22 E7M22 36 26 34 E7C22 E7P22 E7D22 1 E7H22 J 19 28 P 317 E7F22 E7G22 6 8 17 E7R22N 9 CYCLE CONTROL GB4 D S353 6 1 5 4 3 2 1 5 3 2 4 220ohm 1 2 W K2 RELAY DAY NIGHT 309 7 P J 3 11 7 R329 TO P337 23 91 77 40 FIGURE 5 TO P337 13 91 77 40 FIGURE 5 TO P337 22 91 77 40 FIGURE 5 TO P337 24 91 77 40 FIGURE 5 E7U22 IN S N S 4636132 THRU 4636247 O...

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Page 1927: ...PAGE 1 Feb 28 07 9H13 91 77 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1928: ...IRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL 1 3 2 Item Designation Description 1 CB365 Circuit Breaker 3 Amp 2 OAT Sensor 3 Quad Digital Indicator Quad Digital Indicator QDI Figure 1 Sheet 1 of 2 Effectivity 4636021 thru 4636131 ...

Page 1929: ...3 4 5 6 AND 91 28 40 CB365 3A DIGITAL q J301 P201 P302 s t C A D P214 LIGHTING LO 8 SIG LO EXC LO EXC HI B SIG HI OAT SENSOR r _ _ _ _ q _ r _ s _ t _ LIGHTING HI 20 E3B20N GB7 H E3K22 DISPLAY E3R20 E3P20 E3S20 E3T20 E3L22 E3M22 E3N22 E3C22 E3D22 E3R22 EXCEEDANCE RESET SW 1 SELECT 2 CAL MAP 1 3 2 P392 21 FUEL IMBALANCE 19 Q21A22 P329 22 TO ANNUNCIATOR E8G22 E8E22 E3AD20 4 4 3 3 R385 P385 E3AC20 E3...

Page 1930: ...91 77 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description Information Pending See Parts Catalog Enhanced Digital Indicator EDI Figure 2 Sheet 1 of 2 Effectivity 4636132 thru 4636374 ...

Page 1931: ...E3AC20 SWITCH DIGITAL RESET 2 3 E3A20 R385 P385 E3AD20 3 4 3 4 DATA BUS TO GAUGES SEE FIGURES 3 4 5 6 AND 91 28 40 FIGURE 2 WH BL WHT WHT WH BL TO ANNUNCIATOR 91 31 50 Q21A22 P329 2 ENHANCED DIGITAL INDICATOR CASE GROUND PWR RETURN OAT EXC LO OAT EXC HI OAT SIG HI OAT SIG LO LIGHTING HI LIGHTING LO 28VDC PWR 11 4 E3S20 RS232 IN FROM GPS 4 1 3 FMGT E3U22 5 14 16 P387 E3V22N GB7 K SQUAT SW RELAY SHO...

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Page 1933: ...IRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 Magneto Sensor 2 CB366 CB367 Circuit Breaker 3 Amp 3 Transducer 1 3 2 MAP RPM Indicator Tachometer Figure 3 Sheet 1 of 3 Effectivity 4636021 thru 4636374 ...

Page 1934: ...TOR P341 SEE FIGURE 1 CB366 3A CB367 3A RPM MAP 21 24 q J402 P402 P304 s t WHT WHT BL A B D P414 LITES LO 5 EXCEEDANCE SUPPRESSION SEE FIGURES 5 6 E8C22 EXCITATION SIG LO SIG HI C SPARE MANIFOLD PRESSURE TRANSDUCER r E8N20 MP1B20 _ _ _ _ q _ r _ s _ t _ LIGHTING HI 15 WHT WHT BL E8K22 SIG HI SIG LO EXC WHT BL MP1A20 WHT WHT E8L20 G K H CA402 WHT BL P303 P401 J401 J LEFT SENSOR 2 MAGNETO 1 P421 4 E...

Page 1935: ...22 SIG HI SIG LO EXC WHT BL MP1A20 WHT WHT E8L20 G K H CA402 WHT BL P303 P401 J401 J LEFT SENSOR 2 MAGNETO 1 P421 4 E8E22N 20 BLK BLU RED CA302 K G H J GB4 N E8M22 TO ENHANCED DIGITAL INDICATOR P341 SEE FIGURE 2 18 E8F22 E8G22 WHT WHT BL WHT 22 12 WHT BL 13 RPM LIGHTING LO E8H22 14 TB 1 LIGHTING HI E8C22 SEE FIGURES 5 6 E8D22 SEE 91 31 50 FIGURE 2 MAP RPM GAUGE 28VDC MAP 28VDC RPM SIGNAL HI SIGNAL...

Page 1936: ...PAGE 10 Feb 28 07 9H22 91 77 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL GRIDS 9H22 THRU 9H24 INTENTIONALLY BLANK ...

Page 1937: ...CRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL TIT and Fuel Flow Indicator Figure 4 Sheet 1 of 3 2 3 1 Item Designation Description 1 CB368 CB369 Circuit Breaker 3 Amp 2 A413 Flow Transducer 3 TIT Probe Effectivity 4636021 thru 4636374 ...

Page 1938: ...IT LO DATA BUS C XMIT HI TB 1 13 18 22 12 TO QUAD DIGITAL INDICATOR P341 SEE FIGURE 1 CB368 3A CB369 3A FUEL FLOW TIT LIGHTING HI 15 WHT E15H22 WHT BL WHT WHT BL W P V CA401 E15J20 P304 P402 J402 U FLOW 2 TRANSDUCER 3 J411 1 E16A22N 20 RED WHT BLK CA301 P W V U GB5 D 25 E15F22N GB7 D LIGHTING LO 21 24 RED YEL FEED THRU PRESS BLKHD RED YEL CHROMEL ALUMEL A413 E15D22 E15C22 PROBE TIT 85508 C L 7 0 T...

Page 1939: ...2N 20 RED WHT BLK CA301 P W V U GB5 D 25 E15F22N GB7 D 21 24 RED YEL FEED THRU PRESS BLKHD RED CHROMEL ALUMEL A413 PROBE TIT E15C22 WHT BL TO ENHANCED DIGITAL INDICATOR P341 SEE FIGURE 2 22 12 E15D22 WHT WHT BL WHT 13 18 E15E22 TB 1 YEL LIGHTING HI LIGHTING LO SEE 91 31 50 FIGURE 2 E15B22 28VDC TIT 28VDC F F ALARM OUT TIT SIGNAL RETURN SIGNAL HI EXC HIGH TURBINE INLET TEMP FUEL FLOW GAUGE CASE GRO...

Page 1940: ...PAGE 14 Feb 28 07 9I4 91 77 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1941: ...I5 91 77 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL Item Designation Description 1 CB313 CB371 Circuit Breaker 3 Amp 1 CHT and Vacuum Indicator Figure 5 Sheet 1 of 3 Effectivity 4636021 thru 4636374 ...

Page 1942: ...T HI TO P340 5 SEE FIGURE 3 EXCEEDANCE SUPPRESSION A307 D C B VAC XDUCER A SIG HI SIG LO SPARE TB 1 E10H22 14 LIGHTING HI KEYWAY ALARM CHT 9 8 6 12 V2A22 ALARM VAC 4 18 E10D22 E10F22 E7B22 E10L20 24 5 2 21 11 TO 91 77 20 FIGURE 3 13 P386 DATA BUS A REC HI DATA BUS B REC LO DATA BUS D XMIT LO GB7 F E10G22 WHT BL WHT BL 10 11 17 E10C22N 7 WHT 13 18 12 22 TO QUAD DIGITAL INDICATOR P341 SEE FIGURE 1 8...

Page 1943: ...2 KEYWAY 14 18 4 ALARM VAC V2A22 2 5 23 10 16 21 22 13 17 11 GB7 F E10C22N 7 E10H22 TB 1 E10D22 TO GAUGE ALERT HORN SEE 91 31 50 FIGURE 2 P386 23 12 35 22 SEE 91 77 20 FIGURE 3 33 E7T22 E7R22 E7B22 E10L20 E7S22 22 12 WHT BL E10F22 E10G22 13 18 WHT BL TO ENHANCED DIGITAL INDICATOR P341 SEE FIGURE 2 WHT WHT CHT VAC GAUGE CASE GROUND SIG HI VAC SIG LO VAC EXCEED SUPSN VAC LIGHTING HI LIGHTING LO PWR ...

Page 1944: ...PAGE 18 Feb 28 07 9I8 91 77 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1945: ...RAGE MAINTENANCE MANUAL Item Designation Description 1 A404 Oil Pressure Switch 2 A405 Oil Pressure Transducer 3 A407 Oil Temperature Sensor 4 CB370 Circuit Breaker 3 Amp 4 1 2 3 Oil Pressure and Temperature Indicator Figure 6 Sheet 1 of 3 Effectivity 4636021 thru 4636374 ...

Page 1946: ...EYWAY 13 WHT BL WHT BL LIGHTING HI SIGNAL LO SIGNAL HI SEE P304 PIN T XDUCER PRESS OIL A405 B D A P409 TO PIN P340 5 SEE FIGURE 3 EXCEEDANCE 4 SUPPRESSION 20 19 P304 P402 E E R R N N T T J402 E4L22 SEE PIN 6 E4B20 WH BL E4B20 WHT E4M20 E2A22 WHT W V V W P303 X X P401 J401 E2B20 WH BL E2B20 WHT TEMP A407 SENSOR A B P411 OIL SWITCH P NC PRESSURE OIL E6C20N P304 P402 J402 S J S J E6B20 W6B20 E6A22 TO...

Page 1947: ...ITCH P NC PRESSURE OIL E6C20N P304 P402 J402 S J S J E6B20 W6B20 E6A22 TO ANNUNCIATOR P329 14 OIL PRESSURE 91 31 50 FIGURE 1 TO HOURMETER 91 31 30 A404 SIG HI SIGNAL RET EXCITATOR E4G22 E4F22 WHT BL WHT WHT TO ENHANCED DIGITAL INDICATOR P341 91 77 40 FIGURE 2 WHT BL 13 18 12 22 TO PIN P340 5 FIGURE 3 SUPPRESSION EXCEEDANCE SEE P304 PIN T E1A22 OT OP CB370 5A TO GAUGE ALERT HORN 91 31 50 FIGURE 2 E...

Page 1948: ...PAGE 22 Feb 28 07 9I12 91 77 40 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1949: ...Data Acquisition Unit DAU 2 RPM Sensor on Left Magneto 3 A405 Oil Pressure Transducer 4 A407 Oil Temp Sensor 5 OAT Sensor 6 Fuel Senders Left Right Inboard Outboard 7 MAP Transducer 8 A413 Fuel Flow Transducer 9 A441 thru A446 CHT Sensors 10 TIT Sensor 11 A307 Vacuum Transducer 12 CB343 CB353 Circuit Breaker 2 Amp 13 CB313 Circuit Breaker 3 Amp 12 13 6 6 5 11 1 7 3 2 4 8 10 11 9 10 2 3 4 8 7 1 12 ...

Page 1950: ... ALT 1 mV LO ALT 1 mV HI OIL TEMP SIG SHIELD SENSOR TEMP SIGNAL LO SIGNAL HI P412 A B A407 OIL E8L20 CA402WHT CA402BLU 1 P421 RED 4 BLK BLU 2 J401 G G V V J J K K H H P401 P303 SENSOR SIGNAL HI SIGNAL LO EXCITATION RPM P903 23 5 E8K22 CA302WHT CA302BLU 2 RPM SIG RPM SIG EXC OUT 12 VDC 3 OAT EXC HI 14 OAT EXC LO 11 OAT SIG HI 29 OAT SIG LO t s r q J402 P201 P302 P902 q t r s SENSOR OAT SIGNAL LO C ...

Page 1951: ...UEL QTY SIG LO L FUEL QTY SIG HI V V CA401A20WHT J315 2 J315 1 E8N20 CA401A20BLU MP1B20WHT MP1B20BLU r r t t q q P P W W s s RED 1 J411 E15J20 BLK 3 WHT 2 EXCITATION SIGNAL LO SIGNAL HI U U P304 J402 P402 F F SIG HI 5 CA301WHT 36 7 25 1 E8M22 P5C20WHT P5C20BLU 23 8 26 MP1A22WHT MP1A22BLU CA301BLU SHIELD ALT 2 mV HI ALT 2 mV LO 28 VDC POWER F F SIG LO MAP SIG HI MAP SIG LO 10 1 11 E3U22 E15H22 P903...

Page 1952: ...CITATION SIGNAL LO TRANSDUCER E9N20YEL E9P20RED A307 B SENSOR TIT A307 SIGNAL HI 29 RED 11 2 21 V3A22BLU V3A22WHT YEL DE ICE SIG HI DE ICE SIG LO JUMP TO P902 36 SHIELD GROUND SEE SHEET 3 P902 MAIN BUS CB312A22 CB312 3A VAC 1 J 1E P V3B22 WHT GRN RED YEL YEL RED WHT GRN GRN RED WHT YEL GRN RED WHT YEL YEL RED WHT GRN YEL WHT RED GRN P6E20WHT P6E20BLU 24 BAT AMP LO 6 BAT AMP HI P303 S P303 R P6A22 ...

Page 1953: ...PAGE 1 Feb 28 07 9I17 91 79 30 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL THIS PAGE INTENTIONALLY BLANK ...

Page 1954: ...L Item Designation Description 1 CB315 Circuit Breaker 3 Amp 2 M30 3 Unit Engine Gauge 3 A404 Oil Pressure Switch 4 A405 Oil Pressure Transducer 5 A407 Oil Temperature Sensor 6 Oil Pressure Sensor 1 Oil Pressure and Temperature Indicators Figure 1 Sheet 1 of 2 Effectivity 4636001 thru 4636020 ...

Page 1955: ... TO ANNUNCIATOR OIL PRESS SEE 91 31 50 FIGURE 1 E6A 22 E4B 20 E4B 20 E4B 20N WHT WHT BLU WHT ORG P411 P409 P318 OIL PRESS TEMP OPTIONAL A D C F B E G H E 2 E 2 2 E 4 D 2 2 E 4 E 2 2 3 A ENGINE GAUGE MAIN BUS E1A 22 E7B 22 TO CYL HEAD TEMP SCANNER P386 13 E4C 20 A D C F E OIL PRESSURE SENSOR 3 UNIT ENG GAUGE CHT 28V OIL TEMP 0IL PRES GND G B H X W E N T R J S S J R T N E W X OPTIONAL INSTALLATION S...

Page 1956: ...PAGE 3 Feb 28 07 9I20 91 79 30 PIPER AIRCRAFT INC PA 46 350P MALIBU MIRAGE MAINTENANCE MANUAL GRIDS 9I20 THRU 9L24 INTENTIONALLY BLANK ...

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