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MOONEY AVIATION COMPANY, INC.

M20TN SERVICE & MAINTENANCE MANUAL

Page

Date

11

2006

Rev Date

Press Windshield De--Ice switch. Check that de--icing

fluid is discharged from spraybars. Check that no holes

are blocked.

--

Switch electrical power OFF.

--

Level III

Annual Inspections.
At Level III, it is recommended that all Level II Inspections are complied with and that the following inspections are

added/included.

Maintenance Practice

Notes

Remove tailcone panels and empennage panels.

Check security and condition of component’s supply

lines and wiring. Pay particular attention to components

close to control rods, etc.

--

Drain tanks. Remove and clean strainer in tank outlets. --
Refill tanks. Check accuracy of tank contents indicator

during refilling process.

The contents indicator does not display actual contents

over the entire range. Refer to calibration chart (Figure

30--3).

Level IV

Component Checks.
The following checks are detailed for use in conjunction with SECTION 30--12--01, TROUBLESHOOTING. In cases

where components can be checked on the aircraft as an alternative to bench testing, both methods are described.

Maintenance Practice

Procedures

Check fluid delivery rate from Airframe/Propeller Pump. 1. Fill tanks to top of filler tube. Operate pump(s) at De--

Ice or Anti--Ice, as required, for a time period. Refill

tanks; measure quantity necessary to replenish to origi-

nal level. Calculate flow rate. Permitted limits are:
De--Ice -- 280 to 300 ml/min.
Anti--Ice -- 140 to 150 ml/min. OR
2. Remove Airframe/Propeller Pump. Bench test.

Check High Pressure Warn Switch.

1. Disconnect Nylon Tube from inlet to Filter. Connect

pressure gauge (0 -- 180 lbf/in

2

) (0 to 13 bar) to tube.

Use TKS Nylon Tube fittings. Operate Airframe/Propel-

ler pump in a series of short bursts (in order to limit rate

of pressure rise) and observe pressure at which High

Pressure Warn LED illuminates. Permitted limits are:
75 to 90 lbf/in2 (5 -- 6 bar) OR
2. Remove High Pressure Switch. Bench test.

30--12--02

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Summary of Contents for M20TN

Page 1: ...NCE MANUAL MOONEY P N MAN180 Copyright 2014 All Rights Reserved MOONEY INTERNATIONAL CORPORATION 165 Al Mooney Road Kerrville Texas 78028 tel 830 896 6000 ISSUED DECEMBER 2006 MOONEY INTERNATIONAL CORPORATION REVISION B MAY 2014 ...

Page 2: ......

Page 3: ...n the Mooney Aircraft Model s addressed in this pubication This warning applies to placards manufactured at Mooney Aviation Company Inc facility WARNING Manufactured with 1 1 1 Trichlorethane substances which are determined to harm public health and environment by destroying ozone in the upper atmosphere and installed on the Mooney Aircraft Model s addressed in this pubication This warning applies...

Page 4: ...MOONEY AVIATION COMPANY INC M20TN SERVICE AND MAINTENANCE MANUAL INTENTIONALLY LEFT BLANK ...

Page 5: ... Approved Original Issue December 2006 Revision A August 2010 Revision B MAY 2014 Always destroy superceded pages when you insert the revised pages Revision Date Affected Pages Description of Revision Chapter 4 AIRWORTHINESS B 4 EFFECTIVITY Revised List of Effective Pages B 4 CONTENTS Revised Table of Contents B Page 5 Added Airworthiness Limitation Data Replacement Schedule B Page 6 Added Airwort...

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Page 7: ... are normally incorporated When a subsequent Service Bulletin is issued after the delivery date Mooney Aviation Company will post them on the www mooney com website for owner s concerning details for compliance The Service Bulletin number date title and incorporation should be noted in the log provided The Service Bulletin will be incorporated into the next sched uled revision of the maintenance m...

Page 8: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Page Date 2 Rev Date 2006 S B NUMBER DATE DESCRIPTION OF BULLETIN COMPLETED BY LOG OF REVISIONS SERVICE BULLETINS AUGUST 2010 ...

Page 9: ...our lev els Group Chapter System Section Sub system Subject Unit GROUP These are primary divisions of the manual that enable broad separation of content ie Airframe systems VS Powerplant systems These groups are identified by tabs CHAPTER System The various groups contain major systems information such as flight controls landing gear etc The systems are arranged numerically per GAMA recommended nu...

Page 10: ...OR ADDRESSES PUBLICATIONS ENGINE PUBLICATIONS Teledyne Continental Motors Aircraft Products P O Box 90 Mobile Alabama USA 36601 Attn Accounts Receivable Prepaid only Overhaul Manual for Teledyne Continental Motors Aircraft TSIO 550 G Engine Models Form M18 Illustrated Parts Catalog for Teledyne Continental Motors TSIO 550 G series aircraft engines Form X30615A Maintenance Op erators Manual for Tel...

Page 11: ...5544 DE ICING PROPELLOR B F Goodrich Avionics Systems Inc 5353 52nd Street SE P O Box 873 Grand Rapids MI 49588 0873 Telephone 800 253 9525 NAVIGATION LIGHTS STROBES Whelen Engineering Co Route 145 Winthrop Road Chester CT 06412 0684 HEADSETS Bose Corporation 145 Pennsylvania Avenue Framingham MA 01701 DRE Communications Company 1723 Little Orchard Street San Jose CA 95125 Telephone 408 993 8220 T...

Page 12: ...AREAS 00 GENERAL 7 LIFTING AND SHORING 10 JACKING 8 LEVELING AND WEIGHING 00 LEVELING 9 TOWING AND TAXIING 00 GROUND HANDLING 10 TOWING 20 WARM UP AND TAXIING 30 EMERGENCY PROCEDURES 10 PARKING AND MOORING 00 GENERAL 10 PARKING 20 MOORING 11 PLACARDS AND MARKINGS 00 GENERAL 10 MARKINGS 20 PLACARDS EXTERIOR INTERIOR 12 SERVICING 00 SERVICING 10 REPLENISHING 20 SCHEDULED SERVICING 20 STANDARD PRACTI...

Page 13: ...IPMENT FURNISHINGS 00 GENERAL 10 FLIGHT COMPARTMENT 50 CARGO COMPARTMENT 60 EMERGENCY EQUIPMENT 27 FLIGHT CONTROLS 00 GENERAL 10 AILERON SYSTEM 20 RUDDER SYSTEM 30 ELEVATOR SYSTEM 40 STABILIZER TRIM SYSTEM 50 WING FLAP SYSTEM 60 AILERON RUDDER INTERCONNECT SYSTEM 90 MISCELLANEOUS 28 FUEL 00 GENERAL 10 STORAGE 20 DISTRIBUTION 30 DUMP 40 INDICATING 90 MISCELLANEOUS 30 ICE AND RAIN PROTECTION 00 GENE...

Page 14: ...INTENANCE PRACTICES 40 EXTERIOR LIGHTS MAINTENANCE PRACTICES 34 NAVIGATION 00 GENERAL 10 PITOT STATIC AIR PRESSURE SYSTEM 30 DIRECTIONAL GYRO COMPASS 90 MISCELLANEOUS INSTRUMENTS 35 OXYGEN 00 GENERAL 37 VACUUM 00 GENERAL 39 ELECTRICAL PANELS AND COMPONENTS 00 GENERAL 10 INSTRUMENT AND CONTROL PANELS 20 ELECTRICAL AND ELECTRONICS EQUIPMENT RACKS 51 STRUCTURES 00 GENERAL 10 STRUCTURAL REPAIR GENERAL...

Page 15: ...ZER 20 ELEVATOR 30 VERTICAL STABILIZER 40 RUDDER 56 WINDOWS 00 GENERAL 10 20 WINDSHIELD CABIN WINDOWS 50 ACRYLIC DRILLING 57 WINGS 00 GENERAL 10 MAIN FRAME 20 AUXILIARY STRUCTURE 30 PLATES SKINS 40 ATTACH FITTINGS 50 FLIGHT SURFACES 61 PROPELLERS 00 GENERAL 10 PROPELLER ASSEMBLY 20 CONTROLLING 40 BALANCING PROCEDURES 71 POWERPLANT 00 GENERAL 10 COWLING 20 MOUNTS 30 FIRESEALS 60 AIR INTAKES 72 ENGI...

Page 16: ...GNITION 00 GENERAL 10 POWER CONTROL 20 ENGINE FIRING ORDER 30 SWITCHING 76 ENGINE CONTROLS 00 GENERAL 10 ENGINE CONTROLS RIGGING 20 MAINTENANCE 77 ENGINE INDICATING 00 GENERAL 10 POWER 20 TEMPERATURE 30 PRESSURE 78 EXHAUST 00 GENERAL 10 INSTALLATION 30 SERVICING 40 REPLACEMENT COMPONENTS 79 OIL 00 GENERAL 20 DISTRIBUTION 30 INDICATING 40 TRANSDUCERS TEST 50 TROUBLESHOOTING 80 STARTING 00 GENERAL 1...

Page 17: ...TER SECTION TITLE 81 TURBINES 00 GENERAL 20 TROUBLESHOOTING 30 SERVICING 40 PERIODIC REPLACEMENT COMPONENTS 91 SCHEMATICS AND HARNESSES 00 GENERAL 20 ELECTRICAL SYSTEM HARDWARE CHARTS 30 SCHEMATICS AND HARNESSES Supplement CD ROM for paper manuals 95 SPECIAL EQUIPMENT INTRODUCTION AUGUST 2010 ...

Page 18: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Page Date 10 2006 Rev Date INTENTIONALLY LEFT BLANK INTRODUCTION ...

Page 19: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 4 AIRWORTHINESS LIMITATIONS ...

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Page 21: ...MANUAL MOONEY INTERNATIONAL CORPORATION Date 2006 Rev Date CHAPTER 4 AIRWORTHINESS LIMITATIONS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 4 Effectivity 1 05 14 4 Contents 3 05 14 4 00 00 5 05 14 4 EFFECTIVITY MAY 2014 ...

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Page 23: ...INTERNATIONAL CORPORATION Date 2006 Rev Date CHAPTER 4 AIRWORTHINESS LIMITATIONS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 4 00 00 Airworthiness Limitations 5 4 10 00 Component Replacement 5 4 10 01 Replacement Schedule 5 4 CONTENTS MAY 2014 ...

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Page 25: ... or Airworthiness Directives 4 10 01 REPLACEMENT SCHEDULE ITEM REPLACE TIME LIMITS Propulsion Exhaust Tailpipe V Band Clamp Tailpipe V Band clamps shall be replaced with new clamp after it has been removed the second time The V Band clamp shall also be replaced with a new clamp at each engine overhaul or 2 000 hours maxim um whichever occurs first NOTE Components shall be inspected and serviced at...

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Page 27: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 5 TIME LIMITS MAINTENANCE CHECKS ...

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Page 29: ... Contents 3 12 06 5 00 00 5 12 06 5 10 00 6 05 14 5 10 01 7 05 14 5 10 01 8 08 10 5 10 01 9 08 10 5 20 00 10 12 06 5 20 01 11 12 06 5 20 01 12 12 06 5 20 01 13 12 06 5 20 02 14 12 06 5 20 05 15 08 10 5 20 06 16 08 10 5 20 06 17 08 10 5 20 06 18 08 10 5 20 06 19 08 10 5 20 06 20 08 10 5 20 07 21 08 10 5 20 07 22 08 10 5 20 07 23 08 10 5 20 07 24 08 10 5 20 07 25 12 06 5 20 07 26 08 10 5 EFFECTIVITY...

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Page 31: ... 5 00 06 Cabin Heating Ventilating Systems 5 5 00 07 Fuel System 5 5 10 00 Time Limit Components 6 5 10 01 Overhaul Maintenance and Replacement Schedule 7 5 20 00 Scheduled Maintenance Checks 8 5 20 01 Inspection Check Points 8 Torque Tables 9 5 20 02 Aircraft File Inspection 12 5 20 03 Engine Functional Check 12 5 20 04 First 25 Hours Inspection Non Repetitive 12 5 20 05 50Hour Inspection Repetit...

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Page 33: ...cally actuated and are controlled by a spring loaded up off down switch on the center console 5 00 04 ELECTRIC POWER SYSTEM The Master Switch and power relay control the electri cal power system comprised of a 100 AMP 28 Volt al ternator and two 10 AMP HR 24 Volt batteries The al ternator system has an overvoltage protective relay and an overvoltage annunciator light Circuit breakers or circuit br...

Page 34: ...ements over those found in the Manu facturer s Data Propeller See Special Note below Refer to Propeller Manufacturer s Continued Airwor thiness Data for specific Time Limits Mooney has no special requirements over those found in the Manu facturer s Data Propeller Governor Refer to Continental Bendix Manufacturer s Contin ued Airworthiness Data for specific Time Limits Mooney has no special require...

Page 35: ...ars A C with Solid Green Kevlar Bottle P N 026N2001 3 Hydrostatic Test Required 3 year intervals A C with Striped Green Carbon Bottle P N 026N2003 3 Hydrostatic Test Required 5 year intervals Oxygen Bottle return to Precise Flight Replace 15 Years Air Conditioning Components Optional Chapter 21 See Section 21 58 00 for specific maintenance and servicing times All Other Components Excluding Avionic...

Page 36: ...e Replace On Condition GDU 1042 MFD Remove Replace On Condition GMA 1347 Remove Replace On Condition GIA 63 IAU Qty 2 Remove Replace On Condition GEA 71 EAU Remove Replace On Condition GTX 33 Mode S Transpon der Remove Replace On Condition GTX 33 Mode S Transpon der Test according to Title 14 CFR ww 91 411 and 91 413 as well as Part 43 Appendix F 24 Months GDC 74A Remove Replace On Condition GDC 7...

Page 37: ...tion Procedure Interval TVS Unit Replacement Replace the voltage suppressor unit Refer to G1000 GFC700 Wiring Diagram The Standby Attitude Indicator Voltage Suppres sor is located behind instrument panel near the Standby Attitude Indicator harness connector Replace After Suspected Actual Lightning Event Visual Inspection Complete Visual Inspection Aircraft Annual Electrical Bonding Test Perform an...

Page 38: ...etween systems and the engine shall be torqued to 25 inch pounds Hose clamp installations on blast tubes air ducts drain and vent lines shall be torqued to 15 inch pounds 4 Pipe Threads Tightening and torque procedures Lubricate pipe threads as follows Oxygen Lines Use only MIL T 5542 thread com pound or Teflon thread seal tape on threads of valves connectors fittings parts or assemblies which mig...

Page 39: ...riate class is intended to provide an assembly capable of being tightened to the bolt proof load without thread stripping occurring The torque value to be set for a particular size of screw is dependent upon 1 Material of the screw 2 Parent material steel non ferrous metal or plastic 3 Whether the screw is untreated or plated 4 Whether the screw is dry or lubricated 5 The depth of the thread TIGHT...

Page 40: ... 70 135 99 160 118 M14 X 1 5 150 110 210 154 250 184 M16 X 1 5 225 165 315 232 380 280 M18 X 1 5 325 239 460 339 550 405 M20 X 1 5 460 339 640 472 770 567 M22 X 1 5 610 449 860 634 1050 774 M24 X 2 780 575 1100 811 1300 958 TIGHTENING TORQUES Electrically Zinc Plated Hardware Friction Coefficient 0 125 NOMINAL DIAMETER Coarse Thread PROPERTY CLASS 5 6 8 8 10 9 12 9 TORQUE Ma Nm Ft Lb Nm Ft Lb Nm F...

Page 41: ...6 X 1 5 210 154 295 217 350 258 M18 X 1 5 305 224 425 313 510 376 M20 X 1 5 425 313 600 442 720 531 M22 X 1 5 570 420 800 590 960 708 M24 X 2 720 531 1000 737 1200 885 METRIC CONVERSION FACTOR One Nm Newton Meter 7375 Foot Pound One Foot Pound 1 355818 Nm AN MS STANDARD BOLT NUTS TORQUE TABLES FINE THREAD SERIES NUT BOLT SIZE TENSION Type AN BOLTS AN365AN310 NUTS SHEAR Type AN BOLTS AN364 AN320 NU...

Page 42: ...Certificate Airworthiness Certifi cate Weight Balance Record Engine Service Infor mation Aircraft Radio Station License if applicable FAA Airworthiness Directives and Mooney service documents 5 20 03 ENGINE FUNCTIONAL CHECK Prior to a scheduled 100 hour or annual inspection and or 25 hours after installation of new or overhauled engine wash down the engine and engine compo nents Then perform an en...

Page 43: ...damage G Inspect ignition leads harness spark plug el bows and shielding nuts for damage and security H Inspect cylinders for evidence of overheating Engine Installation Inspections I Inspect baffles for secure anchorage close fit around cylinders and freedom from cracks J Inspect engine controls for full travel freedom of movement and security K Drain and clean fuel strainer Gascolator L Visually...

Page 44: ...e a differential hot engine compres sion check Ref TCM SB M84 15 or current rev clean and gap or replace spark plugs 016 021 both Champion fine wire and thick electrode also refer to manufacturer for proper specifications B Inspect engine for evidence of fuel and oil leak age Inspect oil cooler Inspect oil and fuel hoses for condition and security C Drain engine oil sump remove clean and in spect ...

Page 45: ...ng the aircraft B Inspect wheels for cracks distortion misalign ment corrosion and bolt failure Inspect condition of felt seals and bearings re pack bearings at 100 hour inter vals C Inspect brakes for disc and pad wear and disc warpage Ref Section 32 40 04 D Inspect hydraulic reservoir for proper fluid level E Inspect hydraulic brake lines and hoses for leak age dents cracks chafing kinks and sec...

Page 46: ...er adjustment See Section 33 43 00 for adjustment procedures L Inspect external Decals Placards for security M Lightening Strike Inspection exterior interior 6 INTERIOR INSPECTION A Inspect seats seat tracks and upholstery for cleanliness and mounting security Inspect seats for condition and operation of position locks Inspect seat structure for cracks deformation corrosion and mech anism lubricat...

Page 47: ...es to ensure that no corrosion chaffing cracks or other defects exist 3 Manually move the ailerons for roll servo ele vators for pitch servo elevator trim wheel for pitch trim servo and rudder pedals for yaw servo from stop to stop and observe the servo capstan and control surface rigging Ensure there is no binding in the control cabling and that the capstan pulleys rotate freely 4 Check the servo...

Page 48: ...e Ice if installed Push switch ON observe prop de ice annunciator for illumination BLUE light M Check operation of TKS Ice Protection System if installed Check operation of each pump Switch to Main Pump 1 ON set to MAXIMUM FLOW verify steady GREEN light Select NORMAL FLOW verify steady GREEN light OFF Verify High Pressure Light not illuminated if illuminated is indication of need for fil ter repla...

Page 49: ...etraction Tube Rod End Bearings Bellcranks Bungees 100 100 100 Gear Door Rod End Bearings 50 4 Main Gear Grease Fittings 100 Retraction Tube Rod End Bearings Bellcranks Bungees 100 100 100 Gear Door Rod End Bearings 50 Electric Gear Actuator Gear Box AR Electric Gear Actuator Ball Screw 1000 5 Elevator Rudder Controls Control Tube Rod End Bearings Bellcranks 100 100 Batteries Stabilizer Trim Contr...

Page 50: ...ings 100 Bellcranks 100 Guide Blocks 100 Flap Indicator Cable 100 Electric Flap Actuator Gear Box 500 Electric Flap Actuator Ball Screw 100 17 Electric Boost Pump Gascolator 50 18 Control Systems Control Tube Rod End Bearings 100 Control Yoke Lower Section 100 NLG Steering Link Rod End Brgs 100 Rudder Pedal Cross Shaft 100 Rudder Aileron Bungee 100 Hydraulic Brake Cylinder Pedal Linkage 100 19 Ail...

Page 51: ...6 Series LiMnO2 Battery Pack û û û û 100 100 AR 100 100 34 Seat Belt Restraints Standard Inflatable Restraints Optional refer to Chapter 25 for details û û 100 100 35 SpeedBrake 2000 also see Section 27 96 00 Check Cap Strip Cover screws and top attachment screws for security Check Drain tubes for debris Clean and Inspect unit for damage corrosion loosemess proper operation Worm and Worm Gear Lubr...

Page 52: ...pec MHS 24 Oil Specifications Oil Specification or Oil Grade First 25 Engine Hours Non dispersant mineral oil conforming to SAE J1966 shall be used during the first 25 hours of flight operations However if the engine is flown less than once a week a straight mineral oil with corrosion preventative MIL C 6529 for the first 25 hours is recommended Oil Specification or Oil Grade After 25 Engine Hours...

Page 53: ...NANCE MANUAL Page Date 25 2006 Rev Date 7 27 19 27 33 25 24 27 27 17 12 32 11 12 2 10 13 14 30 29 3 23 1 21 20 22 15 16 27 27 26 TN5 1 27 19 6 14 4 18 28 5 12 13 10 7 11 12 32 31 8 9 ACCESS COVER IDENTIFICATION LUBRICATION SERVICE GUIDE FIGURE 5 1 5 20 07 ...

Page 54: ...MOONEY INTERNATIONAL CORPORATION M20TN SERVICE MAINTENANCE MANUAL Page Date 26 2006 Rev Date INTENTIONALLY LEFT BLANK 5 20 07 ...

Page 55: ...on Procedure Interval TVS Unit Replacement Replace the voltage suppressor unit Refer to G1000 GFC700 Wiring Diagram The Standby Attitude Indicator Voltage Suppres sor is located behind instrument panel near the Standby Attitude Indicator harness connector Replace After Suspected Actual Lightning Event Visual Inspection Complete Visual Inspection Aircraft Annual Electrical Bonding Test Perform an e...

Page 56: ...een systems and the engine shall be torqued to 25 inch pounds Hose clamp installations on blast tubes air ducts drain and vent lines shall be torqued to 15 inch pounds 4 Pipe Threads Tightening and torque procedures Lubricate pipe threads as follows Oxygen Lines Use only MIL T 5542 thread com pound or Teflon thread seal tape on threads of valves connectors fittings parts or assemblies which might ...

Page 57: ...ate class is intended to provide an assembly capable of being tightened to the bolt proof load without thread stripping occurring The torque value to be set for a particular size of screw is dependent upon 1 Material of the screw 2 Parent material steel non ferrous metal or plastic 3 Whether the screw is untreated or plated 4 Whether the screw is dry or lubricated 5 The depth of the thread TIGHTEN...

Page 58: ...0 135 99 160 118 M14 X 1 5 150 110 210 154 250 184 M16 X 1 5 225 165 315 232 380 280 M18 X 1 5 325 239 460 339 550 405 M20 X 1 5 460 339 640 472 770 567 M22 X 1 5 610 449 860 634 1050 774 M24 X 2 780 575 1100 811 1300 958 TIGHTENING TORQUES Electrically Zinc Plated Hardware Friction Coefficient 0 125 NOMINAL DIAMETER Coarse Thread PROPERTY CLASS 5 6 8 8 10 9 12 9 TORQUE Ma Nm Ft Lb Nm Ft Lb Nm Ft ...

Page 59: ... 1 5 210 154 295 217 350 258 M18 X 1 5 305 224 425 313 510 376 M20 X 1 5 425 313 600 442 720 531 M22 X 1 5 570 420 800 590 960 708 M24 X 2 720 531 1000 737 1200 885 METRIC CONVERSION FACTOR One Nm Newton Meter 7375 Foot Pound One Foot Pound 1 355818 Nm AN MS STANDARD BOLT NUTS TORQUE TABLES FINE THREAD SERIES NUT BOLT SIZE TENSION Type AN BOLTS AN365AN310 NUTS SHEAR Type AN BOLTS AN364 AN320 NUTS ...

Page 60: ...tificate Airworthiness Certifi cate Weight Balance Record Engine Service Infor mation Aircraft Radio Station License if applicable FAA Airworthiness Directives and Mooney service documents 5 20 03 ENGINE FUNCTIONAL CHECK Prior to a scheduled 100 hour or annual inspection and or 25 hours after installation of new or overhauled engine wash down the engine and engine compo nents Then perform an engin...

Page 61: ...age G Inspect ignition leads harness spark plug el bows and shielding nuts for damage and security H Inspect cylinders for evidence of overheating Engine Installation Inspections I Inspect baffles for secure anchorage close fit around cylinders and freedom from cracks J Inspect engine controls for full travel freedom of movement and security K Drain and clean fuel strainer Gascolator L Visually in...

Page 62: ...a differential hot engine compres sion check Ref TCM SB M84 15 or current rev clean and gap or replace spark plugs 016 021 both Champion fine wire and thick electrode also refer to manufacturer for proper specifications B Inspect engine for evidence of fuel and oil leak age Inspect oil cooler Inspect oil and fuel hoses for condition and security C Drain engine oil sump remove clean and in spect oi...

Page 63: ...the aircraft B Inspect wheels for cracks distortion misalign ment corrosion and bolt failure Inspect condition of felt seals and bearings re pack bearings at 100 hour inter vals C Inspect brakes for disc and pad wear and disc warpage Ref Section 32 40 04 D Inspect hydraulic reservoir for proper fluid level E Inspect hydraulic brake lines and hoses for leak age dents cracks chafing kinks and securi...

Page 64: ... adjustment See Section 33 43 00 for adjustment procedures L Inspect external Decals Placards for security M Lightening Strike Inspection exterior interior 6 INTERIOR INSPECTION A Inspect seats seat tracks and upholstery for cleanliness and mounting security Inspect seats for condition and operation of position locks Inspect seat structure for cracks deformation corrosion and mech anism lubricatio...

Page 65: ... to ensure that no corrosion chaffing cracks or other defects exist 3 Manually move the ailerons for roll servo ele vators for pitch servo elevator trim wheel for pitch trim servo and rudder pedals for yaw servo from stop to stop and observe the servo capstan and control surface rigging Ensure there is no binding in the control cabling and that the capstan pulleys rotate freely 4 Check the servo c...

Page 66: ...ce if installed Push switch ON observe prop de ice annunciator for illumination BLUE light M Check operation of TKS Ice Protection System if installed Check operation of each pump Switch to Main Pump 1 ON set to MAXIMUM FLOW verify steady GREEN light Select NORMAL FLOW verify steady GREEN light OFF Verify High Pressure Light not illuminated if illuminated is indication of need for fil ter replacem...

Page 67: ...d End Bearings Bellcranks Bungees ψ Σ ψ 100 100 100 Gear Door Rod End Bearings ψ 50 4 Main Gear Grease Fittings Ω 100 Retraction Tube Rod End Bearings Bellcranks Bungees ψ Σ Σ 100 100 100 Gear Door Rod End Bearings ψ 50 Electric Gear Actuator Gear Box Ω AR Electric Gear Actuator Ball Screw 1000 5 Elevator Rudder Controls Control Tube Rod End Bearings Bellcranks ψ Σ 100 100 Batteries Stabilizer Tri...

Page 68: ...llcranks Σ 100 Guide Blocks 100 Flap Indicator Cable Σ 100 Electric Flap Actuator Gear Box Ω 500 Electric Flap Actuator Ball Screw 100 17 Electric Boost Pump Gascolator Σ 50 18 Control Systems Control Tube Rod End Bearings ψ 100 Control Yoke Lower Section Σ 100 NLG Steering Link Rod End Brgs ψ 100 Rudder Pedal Cross Shaft Σ 100 Rudder Aileron Bungee Σ 100 Hydraulic Brake Cylinder Pedal Linkage Σ 1...

Page 69: ...06 Series LiMnO2 Battery Pack û û û û 100 100 AR 100 100 34 Seat Belt Restraints Standard Inflatable Restraints Optional refer to Chapter 25 for details û û 100 100 35 SpeedBrake 2000 also see Section 27 96 00 Check Cap Strip Cover screws and top attachment screws for security Check Drain tubes for debris Clean and Inspect unit for damage corrosion loosemess proper operation Worm and Worm Gear Lub...

Page 70: ...TCM Spec MHS 24 Oil Specifications Oil Specification or Oil Grade First 25 Engine Hours Non dispersant mineral oil conforming to SAE J1966 shall be used during the first 25 hours of flight operations However if the engine is flown less than once a week a straight mineral oil with corrosion preventative MIL C 6529 for the first 25 hours is recommended Oil Specification or Oil Grade After 25 Engine ...

Page 71: ...CE MANUAL Page Date 25 2006 Rev Date 7 27 19 27 33 25 24 27 27 17 12 32 11 12 2 10 13 14 30 29 3 23 1 21 20 22 15 16 27 27 26 TN5 1 27 19 6 14 4 18 28 5 12 13 10 7 11 12 32 31 8 9 ACCESS COVER IDENTIFICATION LUBRICATION SERVICE GUIDE FIGURE 5 1 5 20 07 ...

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Page 73: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 6 DIMENSIONS AND AREAS ...

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Page 75: ... 2006 Rev Date CHAPTER 6 DIMENSIONS AND AREAS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 6 Effectivity 1 12 06 6 Contents 3 12 06 6 00 00 5 08 10 6 00 01 6 08 10 6 00 02 7 08 10 6 00 03 8 08 10 6 00 03 9 12 06 6 00 03 10 12 06 6 EFFECTIVITY AUGUST 2010 ...

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Page 77: ...06 Rev Date CHAPTER 6 DIMENSIONS AND AREAS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 6 00 00 Dimensions and Areas 5 6 00 01 Specifications 5 6 00 02 Dimensions 8 6 00 03 Wing Station Ribs and Fuselage Stations 9 6 00 03 Empennage Stations 10 6 CONTENTS AUGUST 2010 ...

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Page 79: ...rs 386 1 Liters 22 7 Liters Spark Plugs Champion RHB32E Two Prong Plug Gap 016 0 41mm 021 0 53mm RHB32S Fine Wire Iridium Plug Gap 016 0 41mm 021 0 53mm Oil Grade Normal Service Below 40o F 4o C Ambient air SL Above 40o F 4o C Ambient air SL 15W50 or 20W50 SAE 30 10W30 15W50 or 20W50 SAE 50 15W50 or 20W50 Oil Capacity 8 Qts 7 57 Liters Minimum for Flight Oil Level 4 5 Qts 4 54 Liters Oil Specifica...

Page 80: ...1RF F7498 B Note B Indicates W Boots Installed Pitch Angle 30 in Sta LOW 17 0o 0 2o HIGH 38 0o 1 0o Diameter Min Max 74 76 188 0 193 0 cm Governor Hartzell Governor Hartzell AIRFRAME WEIGHTS LOADINGS Approximate Empty Weight 2319 Lbs 1051 9 Kg Gross Weight 3368 Lbs 1528 0 Kg Useful Load No Options 1049 Lbs 475 8 Kg Wing Loading 19 26 Lbs Sq Ft 94 0 Kg Sq m Power Loading 12 03 Lbs Hp 5 46 Kg Hp WIN...

Page 81: ...n Electrical Wheel Track 9 2 279 4 cm Wheel Base 6 7 1 2 201 9 cm Tire Size Nose 6 Ply Rating 5 00x5 Tire Size Main 6 Ply Rating 6 00x6 Tire Pressure Nose 49 Lbs Sq In Tire Pressure Main 42 Lbs Sq In 6 00 02 AIRCRAFT DIMENSIONS SUBJECT STANDARD METRIC OPT MISC DIMENSIONS Wing Span 36 6 1112 5 cm Fuselage Length 26 8 812 8 cm Tail Height 8 6 259 1 cm Stabilizer Span 11 9 358 1 cm AREAS Wing 174 8 S...

Page 82: ... 03 AIRCRAFT STATIONS NOTE The datum line station 0 0 is 13 inches aft of the nose gear trunnion pivot point Reference Figure 8 2 1112 5 cm 279 4 cm 76 193 0 cm 201 9 cm 6 7 1 2 9 2 358 1 cm 11 9 259 1 cm 8 6 36 6 812 8 cm 26 8 R6 1 PRINCIPAL AIRCRAFT DIMENSIONS FIGURE 6 1 6 00 03 AUGUST 2010 ...

Page 83: ... 9 2006 Rev Date STA FUSELAGE STATIONS 211 50 STA 176 00 STA 142 00 STA 100 00 STA 21 80 STA 53 00 STA R6 2 5 00 STA 5 375 3 68 STA WING STATION RIBS 103 50 210 97 STA 193 50 STA 147 75 STA STA 24 50 59 25 STA STA WING STATION RIBS AND FUSELAGE STATIONS FIGURE 6 2 6 00 03 ...

Page 84: ...ONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Page Date 10 2006 Rev Date STA 25 75 STA 5 25 R6 3 STA 52 50 STA 70 0 STA 42 25 STA 4 43 STA 42 25 STA 70 0 EMPENNAGE STATIONS FIGURE 6 3 6 00 03 ...

Page 85: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 7 LIFTING AND SHORING ...

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Page 87: ...N SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 7 LIFTING AND SHORING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 7 Effectivity 1 12 06 7 Contents 3 12 06 7 10 00 5 08 10 7 10 00 6 08 10 7 EFFECTIVITY AUGUST 2010 ...

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Page 89: ...AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 7 LIFTING AND SHORING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 7 10 00 Jacking 5 7 10 00 Jacking 6 7 CONTENTS AUGUST 2010 ...

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Page 91: ...oint 3 To raise engine remove top cowling and support the engine using an A Frame with chain hoist or hy draulic Cherry Picker and hook into the engine lifting hook LYCOMING engine mounted on top of engine or front and rear engine lift hooks CONTINENTAL en gine Refer to Figure 7 1 4 Raise aircraft keeping wings as nearly level as possible 5 Secure safety locks on each jack WARNING Do not use prope...

Page 92: ...N RING WARNING DO NOT USE AS A JACK POINT ADJUSTABLE JACKSTANDS ENGINE LIFT POINT A FRAME WITH CHAIN HOIST LYCOMING ENGINE WARNING DO NOT USE PROPELLER JACKS OR PROPELLER STANDS ENGINE LIFT POINTS CONTINENTAL ENGINE DO NOT LEAVE ON AIRCRAFT DURING FLIGHT JACK AND LIFT POINT LOCATION FIGURE 7 1 AUGUST 2010 ...

Page 93: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 8 LEVELING AND WEIGHING ...

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Page 95: ...ANCE MANUAL Date 2006 Rev Date CHAPTER 8 LEVELING AND WEIGHING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 8 Effectivity 1 12 06 8 Contents 3 12 06 8 00 00 5 08 10 8 00 01 6 12 06 8 00 01 7 12 06 8 00 01 8 12 06 8 EFFECTIVITY AUGUST 2010 ...

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Page 97: ...VIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 8 LEVELING AND WEIGHING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 8 00 00 Leveling 5 8 00 01 Weight and Balance 5 8 CONTENTS ...

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Page 99: ...l to each tank see Pilot s Oper ating Handbook for proper quantity of unusable fuel 5 Fill oil to capacity 8 quarts 6 Position a 2000 pound capacity scale under each of the three wheels 7 Level aircraft as described in Section 8 00 00 and center nose wheel 8 Weigh the aircraft 9 Find reference point by dropping a plumb bob from center of nose gear trunnion retracting pivot axis to floor Mark point...

Page 100: ... 2100 1000 1050 2200 2300 1100 Kg 2400 2500 LBs 1150 1050 CENTER OF GRAVITY F S Inches 2363 2344 19 42 42 15 209 5 x x 43 98810 102791 3981 44 45 503 CENTER of GRAVITY F S mm ON or ABOVE LINE 1070 1090 1110 505 1130 1150 501 R8 1 REQUIRED NO BALLAST WEIGHT 505 Charlie Weight Installation For license calculate new weight C G Moment Licensed Empty Weight Licensed Empty Weight C G Location 43 5 CHARL...

Page 101: ...TENANCE MANUAL Page Date 7 2006 Rev Date REF POINT NOSE GEAR TRUNNION STA 13 Lm n Lm r Lc g Wn Lm Wr Wl L M N M R L MEASUREMENTS DATUM STA 0 REFERENCE LEVELING SCREWS LEVEL REF INCHES CM INCHES CM R8 2 WEIGHT AND BALANCE DIAGRAM FIGURE 8 2 8 00 01 ...

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Page 103: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 9 TOWING AND TAXIING ...

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Page 105: ...C M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 9 TOWING AND TAXIING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 9 Effectivity 1 12 06 9 Contents 3 12 06 9 00 00 5 12 06 9 30 00 6 12 06 9 EFFECTIVITY ...

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Page 107: ...N SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 9 TOWING AND TAXIING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 9 00 00 Ground Handling 5 9 10 00 Towing 5 9 20 00 Warm up Taxiing 5 9 30 00 Emergency Procedures 5 9 CONTENTS ...

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Page 109: ...ledgement of maneuvers refer to Garmin G1000 Cockpit Reference Guide for detailed description of flight display features 5 Check Garmin G1000 Multi Function Display MFD for any sluggish response to engine control movements refer to Garmin G1000 Cockpit Reference Guide for detailed description of flight display features Repair any discrepancies found prior to flight 9 30 00 EMERGENCY PROCEDURES 1 E...

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Page 111: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 10 PARKING AND MOORING ...

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Page 113: ...ERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 10 PARKING AND MOORING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 10 Effectivity 1 12 06 10 Contents 3 12 06 10 00 00 5 08 10 10 20 00 6 12 06 10 EFFECTIVITY AUGUST 2010 ...

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Page 115: ...ANUAL Date 2006 Rev Date CHAPTER 10 PARKING AND MOORING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 10 00 00 General 5 10 10 00 Parking 5 10 10 01 Storage Flyable 5 10 10 02 Storage Prolonged 5 10 10 03 Return to Service 5 10 20 00 Mooring 5 10 CONTENTS ...

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Page 117: ...for protec tion 1 Refer to paragraph 10 20 00 for mooring instruc tions 2 Tape or cover all openings 3 Remove batteries charge fully and store in a cool place 4 Raise aircraft to remove weight from tires and block up wheels CAUTION If weight is not removed from tires rotate wheels tires to a new position at least once each 30 days to prevent flat spotting tires 5 See appropriate TCM Service Inform...

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Page 119: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 11 PLACARDS AND MARKINGS ...

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Page 121: ...0TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 11 PLACARDS AND MARKINGS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 11 Effectivity 1 12 06 11 Contents 3 12 06 11 00 00 5 12 06 11 30 00 6 12 06 11 EFFECTIVITY ...

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Page 123: ...N SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 11 PLACARDS AND MARKINGS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 11 00 00 General 5 11 10 00 Markings Exterior Paint 5 11 20 30 00 Placards Exterior Interior 5 11 CONTENTS ...

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Page 125: ...nance actions When an airplane has been painted in spect all placards to assure that they are not ob scured by paint 11 10 00 MARKINGS EXTERIOR PAINT Exterior paint schemes are depicted in M20TN Illus trated Parts Catalog 11 20 30 00 PLACARDS EXTERIOR INTERIOR All required placards and their locations both interior and exterior are listed in Section II of the FAA Ap proved Flight Manual and Pilot ...

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Page 127: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 12 SERVICING ...

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Page 129: ... 2006 Rev Date CHAPTER 12 SERVICING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 12 Effectivity 1 12 06 12 Contents 3 12 06 12 00 00 5 12 06 12 10 04 6 08 10 12 20 02 7 12 06 12 20 03 8 12 06 12 20 06 9 12 06 12 20 06 10 12 06 12 EFFECTIVITY AUGUST 2010 ...

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Page 131: ...g Intervals 5 12 10 00 Replenishing 5 12 10 01 Fuel Tanks 5 12 10 02 Fuel Drains 5 12 10 03 Engine Oil 5 12 10 04 Oxygen System Avox Scott 6 12 10 05 Oxygen System Precise Flight 6 12 20 00 Scheduled Servicing 6 12 20 01 Induction Air Filter 6 12 20 02 Batteries 7 12 20 03 Tires Wheels 8 12 20 04 Brake Reservoir 8 12 20 05 Hydraulic Brakes 8 12 20 06 Cleaning 9 12 CONTENTS AUGUST 2010 ...

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Page 133: ...Drain The fuel gascolator is at the lowest point in the fuel system and has a drain valve op erated by a control on the floor in the cabin To drain the fuel gascolator A Switch fuel selector valve handle to L and pull fuel drain valve control ring for 10 seconds B Switch fuel selector valve handle to R and pull fuel drain valve control ring for 10 seconds C After draining be sure fuel drain valve ...

Page 134: ...fully charged contain approximately 77 cubic feet or 115 7 cubic feet of avia tors breathing oxygen Specifications No MIL O 27210 Recharging of this oxygen cylinder should be accomplished by using the appropriate Scott recharging fittings to the pressure shown on Figure 12 1 Pressure vs Temperature Table WARNING Oil grease or other lubricants in contact with oxygen create a serious fire hazard suc...

Page 135: ...bris Remove any debris found 8 Re install air filter Make sure the air filter assem bly is properly seated and is mounted securely to the filter air box assembly Make sure of proper sealing and security 9 Re install engine cowling NOTE Do not use gasoline jet fuel or caustic cleaning solutions or shop solvents Use only FAA ap proved Challenger cleaning solution in Challeng er Re charger Kit P N CP...

Page 136: ...ke is released prior to beginning hydraulic system servicing For best results use a hydraulic pressure service unit pressure pot to back bleed the system through wheel cylinder bleeder valves NOTE Brake pedal may need to be pulled back in order for fluid to bleed back into reservoir DUAL BRAKE SYSTEM Ref Figure 12 3 1 Remove hydraulic fluid reservoir filler plug and install a suitable fitting for ...

Page 137: ...r use pre wax cleaners during initial paint curing period Use only mild aircraft detergent and cool water when washing exterior during the first 90 days after repainting D To remove heavy oxidation film use a pre wax cleaner E Apply an exterior finish wax recommended for protection of urethane enamel Apply a heavy coating of wax to leading edges of wings empennage and nose section to reduce drag a...

Page 138: ... out by using Plexiglass re surfacing kits i e Micro Mesh available from aircraft accessory suppliers D Check door seals for damage that could cause leakage E Check cabin and baggage door mechanism for proper working order 3 ENGINE COMPARTMENT Accumulation of dirt and oil within the engine compart ment creates a fire hazard and hampers inspection pro cedures A Wash engine cowling and engine compar...

Page 139: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 20 STANDARD PRACTICES AIRFRAME ...

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Page 141: ...06 Rev Date CHAPTER 20 STANDARD PRACTICES AIRFRAME LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 20 Effectivity 1 12 06 20 Contents 3 12 06 20 00 00 5 12 06 20 00 01 6 12 06 20 00 02 7 12 06 20 00 02 8 12 06 20 00 03 9 12 06 20 00 04 10 12 06 20 EFFECTIVITY ...

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Page 143: ...2006 Rev Date CHAPTER 20 STANDARD PRACTICES AIRFRAME TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 20 00 00 General 5 20 00 01 Skin Specifications 5 20 00 02 Corrosion Detection Prevention 7 20 00 03 Painting 9 20 00 04 Low Pressure System Lines Hoses 10 20 CONTENTS ...

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Page 145: ... 11 10 14 9 16 8 7 15 1 18 2 3 4 5 6 24 50 STA 59 25 STA 103 50 STA 147 75 STA 193 50 STA 210 97 STA TN20 1 INDEX SKIN MATERIAL INDEX SKIN MATERIAL NO THICKNESS NO THICKNESS 1 0 063 2024 T 3 CLAD 12 0 025 c 2024 T 3 CLAD 2 0 050 2024 T 3 CLAD 13 0 020 a 2024 T 3 CLAD 3 0 040 2024 T 3 CLAD 14 0 032 2024 T 3 CLAD 4 0 040 2024 T 3 CLAD 15 0 040 b 2024 T 3 CLAD 5 0 025 2024 T 3 CLAD 16 0 040 d 2024 T ...

Page 146: ...KNESS 1 0 025 2024 T 3 CLAD 10 0 032 2024 T 3 CLAD 2 0 040 d 2024 0 CLAD 11 0 032 2024 T 3 CLAD 3 0 025 c b 2024 T 4 CLAD 12 0 032 2024 T 3 CLAD 4 0 025 2024 T 3 CLAD 13 0 025 a 2024 T 3 CLAD 5 0 025 b 2024 T 3 CLAD 14 Polyester Glass Fiber Reinforced 6 0 020 2024 T 3 CLAD a Left side only 7 0 025 2024 T 3 CLAD b Right side only 8 0 032 d e 2024 0 CLAD c 0 032 can be used 9 0 025 2024 T 3 CLAD d H...

Page 147: ...used Paint removing sub stances left in metal crevices will cause further corro sion Turco 6898 Turco Products Inc 6135 South Central Ave Los Angeles California will remove cor rosion from aluminum and treat the metal surface in one application This Section discusses corrosion types and their prevention along with suggested proce dures for corrosion protection of internal airframe sur faces 1 Type...

Page 148: ...erior surface dry after washing down E Hangar aircraft when not in use F If battery acid is spilled on any part of the aircraft immediately wash the area with a solution of sodium bi carbonate in water Rinse with clear water and dry with clean towels NOTE ACF 50 or equivalent can be fogged into fuse lage empennage or wing skin areas It is recom mended that electrical connections and electrical com...

Page 149: ...ith one of the wipe solvents listed above After the old paint grime etc has been loosened and removed the scoured area should be wiped with a tack rag and again cleaned with fresh wipe solvent The part should now be ready for priming and painting b On steel Remove all grease grime loose paint etc by wiping with a wipe solvent and rags Do not allow the wipe solvent to evaporate Wipe it dry Steel pa...

Page 150: ...control surfaces It is required that repainted control surfaces be removed and reba lanced prior to flight per paragraph 27 91 00 NOTE Never use abrasive polish compounds or harsh soaps and detergents on urethane finishes Once the surface gloss is damaged it cannot be re stored by polishing 20 00 04 LOW PRESSURE SYSTEM HOSES LINES Any low pressure line Static Drain etc may be spliced to replace a ...

Page 151: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 21 ENVIRONMENTAL SYSTEMS ...

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Page 153: ... 21 Effectivity 1 12 06 21 Contents 3 12 06 21 00 00 5 08 10 21 50 00 6 08 10 21 51 00 7 08 10 21 51 01 8 08 10 21 52 00 9 08 10 21 52 02 10 08 10 21 53 00 11 08 10 21 53 03 12 08 10 21 54 03 13 08 10 21 54 04 14 08 10 21 55 03 15 08 10 21 55 05 16 08 10 21 56 05 17 08 10 21 57 00 18 08 10 21 57 00 19 08 10 21 58 00 20 08 10 21 59 00 21 08 10 21 EFFECTIVITY AUGUST 2010 ...

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Page 155: ...rive Belt Inspection Maint 12 21 54 01 Belt Removal 12 21 54 02 Drive Belt Replacement Procedure 12 21 54 03 Drive Belt Alignment Procedure 13 21 54 04 Drive Belt Tensioning Procedure 14 21 55 00 Compressor Assembly Inspection Maint 14 21 55 01 Special Tools 14 21 55 02 Compressor Inspection Procedure 14 21 55 03 Compressor Removal 15 21 55 04 Compressor Replacement 15 21 55 05 Compressor Oil Leve...

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Page 157: ...de at regular intervals to en sure proper operation 21 40 00 HEATING Heat is extracted from the high pressure temperature flow between the compressor and intercooler through flexible hoses connecting the turbocharger air induc tion pipes Fig 21 1 and the cabin heater box assem bly The air from the high pressure temperature flow is regulated by fixed orifice sonic nozzles It is recom mended that th...

Page 158: ...ected to the evaporator module expansion valve where the high pressure liquid is expanded to a low pressure The expansion process creates a super cool gas which passes through the evaporator coil and absorbs heat from the warm cabin air passing over the coils The warm low pressure refrigerant then enters the R 134a compressor where the process starts all over again In addition to cooling cabin air...

Page 159: ...RONT EVAP BLOW 4 2 3 1 AIR11A14 AIR08A14 AIR17A14 AIR04A14 PL02A 2 1 TAILCONE CL37A AIR02A14 8 AIR COND TAILCONE AIR01A14 SUPPLIED VENDOR AIR01A14 AIR BR20 CONDR 20 CL04A PL04A RC04A CL04A CL37A AIR101A AIR COND SWITCH 7 CIRCUIT BREAKER PANEL 1 1 1 1 0 9 2 1 8 PL21A AIR02A14 AIR03A14 JUMPER JUMPER AIR14A14 AIR07A14 AIR12A14 CIRCUIT BREAKER PANEL B AIR COND SWITCH RC37A CONSOLE A N C T E F V L 9 PL...

Page 160: ...1 4 21 51 01 SPECIAL TOOLS AND OR EQUIP MENT REQUIRED The following tools and or equipment are required to leak check a refrigerant plumbing system 1 Gaseous dry nitrogen regulated source 0 500 PSIG 2 R 134a refrigerant charging manifold with gauges and hoses 3 Electronic leak detector 4 R 134a refrigerant 30 lb cylinder 5 R 134a Refrigerant oil Ester RL 500S 6 Leak check fluid soapy solution 7 As...

Page 161: ... on all male fitting threads sparingly staying off the first two 2 threads near sealing surface A light coating of R 134a refrigerant oil must be applied to flare and or o ring to prevent metal galling o ring damage NOTE Do not apply oil to fitting threads CAUTION Do not over tighten plumbing connections Stripped threads or cracked flares may result 14 Tighten joints as necessary to stop leaks CAU...

Page 162: ...ion manual for recov ery unit handling and operation NOTE Two people are required for the following proce dure 1 Verify that all electrical power to the system is OFF 2 If required repeat leak check and evacuation pro cedures CAUTION Eye and hand protection must be worn during this procedure 3 Connect manifold charging hose YELLOW to R 134a cylinder shutoff valve and open valve 4 Crack hose fittin...

Page 163: ... will begin to equalize Pressures should be equal in 60 90 seconds 15 Close refrigerant container shutoff valve turn C W Record the refrigerant container final weight and calculate system refrigerant charge as follows CHARGE lb W initial lb W final lb 16 Turn knob on suction and discharge charging hose quick coupler to closed position and disconnect hoses from service ports 17 Remove YELLOW chargi...

Page 164: ...rence of evaporator inlet and outlet air is 25 5o F 11 If suction pressure is above the values outlined in Section 21 52 03 13 the adjustment screw of the evaporator expansion valve which has lowest outlet temperature must be turned OUT in 1 2 revolution in crements 12 Adjust other expansion valve of evaporator that has higher temperature by turning adjustment screw IN in 1 4 revolution increments...

Page 165: ...t gauge Borrough s Tool No 8082A or equivalent around starter accessory drive sheave pulley assembly The extended end of align ment gauge should overlay the upper portion of the compressor sheave outer pulley assembly B The alignment gauge alignment bar must fall within 0 020 inches of the center of the compressor sheave outer pulley groove C If alignment bar is off center of groove by more than 0...

Page 166: ... beneath belt 5 Tighten adjusting bolt two full turns 6 Secure adjusting bolt jam nut 275 325 in lbs and idler pulley slide nut 300 350 in lbs 7 Confirm belt tension is 50 70 lbs by one of the fol lowing methods A Use a direct reading belt tension gauge such as Borrough s Tool No BT 33 73F OR B Measure belt deflection under a five 5 lb load at the center of the longest belt span Correct deflection...

Page 167: ...ther contaminates from en tering system 11 Remove compressor mounting hardware and lift compressor from mounting bracket 21 55 04 COMPRESSOR REPLACEMENT If a new or rebuilt compressor is supplied without suc tion and discharge swivel fittings or pulley these parts must be removed from the failed compressor and installed on the new compressor It is recommended that a complete new compressor assembl...

Page 168: ...ir loss is experienced due to loose connections cracked or kinked hose Repair as necessary 21 56 04 EVAPORATOR MODULE BLOWER MOTOR REMOVAL The evaporator module blower motor is a low cost item that does not contain replaceable brushes Therefore it is recommended that the motor be replaced rather than repaired 1 MOTOR REMOVAL A Verify all power to unit is OFF and all shrouds enclosures etc are remo...

Page 169: ...d and access to the expansion valves must be achieved B Remove valve inlet tubing and remove valve from coil header tube C Inspect valve inlet for contamination and clean as required If no contamination is noted valve should be replaced if operation was erratic prior to removal CAUTION Do not adjust internal spring setting or valve will not operate correctly D Inspect valve internal works to verif...

Page 170: ...lace 5 Failed pressure switch 5 Replace 6 Failed power contactor 6 Replace 7 Failed motor drive 7 Replace 8 Vented system 8 Pressure check evacuate charge 9 Low ambient temperature 9 Normal cutout function 10 Drive motor fuse blown 10 Replace 11 Drive motor temp SW failed 11 Replace switch 12 Contactor control line fuse blown 12 Replace fuse C System operates but does not cool 1 Low refrigerant ch...

Page 171: ...iled switch 1 Replace 2 Failed resistor 2 Replace 3 Failed relay 3 Replace G Compressor Condenser will not operate 1 C B failed or OFF 1 Turn ON or replace 2 Relay s failed 2 Replace 3 Pressure switch failed 3 Replace 4 Power contactor failed 4 Replace 5 Low ambient temperature 5 Normal 6 Low refrigerant charge 6 Re charge system 7 Motor temperature SW failed 7 Replace switch H No evaporator modul...

Page 172: ...ND OR MAINTENANCE SCHEDULES 1 SCHEDULED MAINTENANCE TABLE CHAPTER 5 normally lists the maintenance and replacement time frames for components However since specific air conditioning components have sub component listings these components are listed as follows TYPE MAINTENANCE SERVICE HOURS COMPRESSOR ASSEMBLY R 134A Leak check seal shaft 500 800 Bearing inspection 1000 1500 Bearing replacement On ...

Page 173: ...ays wear eye and hand protection when servicing an air conditioning system Liquid refrigerant can cause frostbite and or blindness 2 Recovery of refrigerant Do not discharge R 134a refrigerant into the atmo sphere Although its ozone depletion potential is zero it can have an effect on global warming In the United States recovery and recycling are mandated by the Clean Air Act Refrigerant recovery ...

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Page 175: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 22 AUTOPILOT SYSTEMS ...

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Page 177: ...EMS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 22 Effectivity 1 08 10 22 Contents 3 08 10 22 00 00 5 08 10 22 00 00 6 08 10 22 10 00 7 08 10 22 10 02 8 08 10 22 10 02 9 08 10 22 10 03 10 08 10 22 10 04 11 08 10 22 10 04 12 08 10 22 10 05 13 08 10 22 40 00 14 08 10 22 EFFECTIVITY AUGUST 2010 ...

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Page 179: ...vo Mounts 7 22 10 01 Roll Servos and Servo Mount 7 22 10 02 Pitch Trim Servos and Servo Mount 8 22 10 03 Pitch Servos and Servo Mount 10 22 10 04 Servo Clutch Adjustment 11 22 10 05 Flap Discrete Input Check 13 22 20 00 Troubleshooting 13 22 20 01 LRU Replacement Procedure 13 22 20 02 LRU Software Installation Testing 13 22 30 00 Autopilot Disconnect Switch 13 22 40 00 System Monitoring 13 22 CONT...

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Page 181: ...arbox GTP 59 Temperature Probe The GFC 700 Autopilot is a two axis fail safe digital flight control system that is integrated into the G1000 It consists of the following components which are added to the existing G1000 components GSA 8 X Servo Actuators Roll Pitch Pitch Trim GSM 85 A Servo Mounts Roll Pitch Pitch Trim The following functions are provided by the GFC 700 in this installation Flight ...

Page 182: ...T HARNESS ASSY INBOARD MAGNETOMETER GMU 44 OAT PROBE HARNESS ASSY GTP 59 OAT ROLL SERVO CABIN AREA GDC 74 AIR DATA FORWARD HARNESS ASSY FORWARD AFT DISCONNECT AFT HARNESS PITCH TRIM SERVO PITCH SERVO GDL 69A GTX 33 GIA 63 1 GIA 63 2 GDU 10 XX PFD FORWARD HARNESS ROLL SERVO ON GFC700 ON GFC700 ROLL SERVO ON STEC EQUIPPED ON GFC700 GARMIN 1000 AUTOPILOT SYSTEM COMPONENTS FIGURE 22 1 22 00 00 AUGUST ...

Page 183: ...PUT GEAR 2 Removal of Roll Servo Mount A Remove the center cotter pin and retaining nut holding the roll servo mount arm B Remove the safety wire MS20995 C and 6 mounting screws and washers holding the roll servo mount arm Roll servo mount arm should be free to remove C Remove the 4 mounting bolts holding the roll servo mount to the bracket Remove servo mount 3 Roll Servo Mount Clutch Adjustment A...

Page 184: ...sole panels and belly fairing 22 10 02 PITCH TRIM SERVO AND SERVO MOUNT 1 Removal of Pitch Trim Servo A Ensure aircraft power is off Unplug any auxil iary power supplies B Set the elevators in neutral position C Remove LH and RH Tailcone access panels and locate GFC700 Pitch Servo Mount D Disconnect servo pigtail connector E Remove the 2 mounting bolts from Pitch Trim Servo to Servo Mount F Remove...

Page 185: ... 35 5 in lbs B Use a brush or applicator apply a thin coat of grease to the servo output gear Use Aeroshell 33MS or Aeroshell 17 Clean and apply grease to output gear every 1000 hours or 3 years C Install Pitch Trim servo to servo mount with original 2 bolts Torque to 35 5 in lbs D Install sprocket dust cap assembly and se cure with original 6 attaching screws Check for alignment top and bottom sp...

Page 186: ...UARD COVER DOWEL SCREWS AND BRIDLE CABLE PITCH SERVO BRIDLE CABLE CENTER FIGURE 22 7 C Remove Servo Mount 4 attaching bolts and remove from Aircraft 3 Pitch Servo Mount Clutch Adjustment A Prior to installation adjust and verify the slip clutch torque on the Pitch Servo is set to 42 6 in lbs Conduct a visual inspection and check slip clutches once every 12 months Refer to Section 22 10 04 Servo Cl...

Page 187: ...ct a 24 Volt DC power supply to the test stand G Place the solenoid switch to ON run motor CW Adjust the capstan nut until torque value indi cates the required setting for appropriate servo mount Switch direction to CCW and adjust capstan nut until the torque value is within required range for appropriate servo mount H Switch motor back and forth adjusting cap stan nut as needed until required tor...

Page 188: ...R SERVO MOUNT CLAMP SERVO MOUNT TO TEST FIXTURE 4 PLACES INSTALL TEST SPROCKET ADJUST TENSION ON CHAIN WITH APPROXIMATELY 1 8 DEFLECTION AND CHAIN TO VALUE SPECIFIED FOR EACH SERVO MOUNT TIGHTEN THUMBSCREWS COTTER CABLE RETENTION DOWEL PIN SERVO SERVO SCREW AND WASHER DUST CAP CABLE GUARD MOUNT PIN CABLE STYLE CAPSTAN SHOWN SERVO MOUNT CLUTCH ADJUSTMENT Typical FIGURE 22 7 AUGUST 2010 22 10 04 ...

Page 189: ...rete input check is complete 22 20 00 TROUBLESHOOTING Troubleshooting the GFC 700 system per the G1000 GFC 700 System Maintenance Manual 190 00638 01 Rev A or later FAA approved revi sion The Garmin G1000 Maintenance Manual should also be referred to for additional calibration instruc tions related to the S TEC Autopilot system 22 20 01 LRU REPLACEMENT PROCEDURES Installing the LRUper proceduresin...

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Page 191: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 24 ELECTRICAL POWER ...

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Page 193: ... CHAPTER SECTION SUBJECT PAGE DATE 24 Effectivity 1 12 06 24 Contents 3 12 06 24 00 00 5 08 10 24 31 02 6 08 10 24 31 02 7 08 10 24 31 02 8 08 10 24 31 02 9 08 10 24 31 03 10 08 10 24 31 03 11 08 10 24 31 04 12 08 10 24 34 00 13 08 10 24 36 00 14 08 10 24 39 03 15 12 06 24 39 04 16 12 06 24 39 05 17 08 10 24 EFFECTIVITY AUGUST 2010 ...

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Page 195: ...Charging System Maintenance Standby Alternator 10 Post Installation Test Procedure Standby Alt 10 Troubleshooting Voltage Regulator Standby Alt 10 Troubleshooting Noise Standby Alt 11 24 31 04 Auxiliary Power System 12 24 32 00 Battery Maintenance 12 24 33 00 Warning Circuits 12 24 34 00 Power Plant Circuits 13 Low Battery Starting Procedures 13 24 35 00 Lighting Circuits 13 24 36 00 Landing Gear ...

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Page 197: ...ammeter Garmin G1000 MFD display shows a discharge at higher RPM a charging system component alternator voltage regulator circuit break er or wiring is malfunctioning On the plane testing should identify which component s may be faulty and needs to be removed from the aircraft for bench test and subsequent repair or replacement The alternator charging system requires no special attention however i...

Page 198: ...T switch is OFF OPEN while battery switch is ON The field to ground short protection GFP func tion or open field OV protection turns off the alternator due to OV fault or RS loss Loss or opening of the Alternator Off Sense wire or voltage Whenever the TSL on the unit is Red the AOI is on Field to Ground Short Protection GFP If the alter nator s field becomes shorted to ground the reason most ACU V...

Page 199: ...he alternator APAC system A Red TSL with the Bat Alt switches on means there is an internal or external ground short in the alter nator field circuit Some alternator s field short to ground under a flying short condition which usually occurs when engine is rotating at higher RPM and not when the engine is off or rotating at a lower RPM A Green TSL with the engine running means there is power comin...

Page 200: ...INSTALLATION TEST PROCEDURE 1 Turn On the Alt Bat switches observe that the AOI light is on 2 On the APAC the TSL should be Green If the TSL is Red the Field is shorted to ground 3 If the TSL is Off measure the voltage on pins 5 and 7 Read Battery voltage on pin 5 and 1 2 volts less on pin 7 4 If the steps 3 4 are successful perform step 5 If not repeat Installation Maintenance Instructions pro vi...

Page 201: ...sing Buss load Poor connection between the load shunt and the ammeter may also give false load indication Buss voltage drops with load increase See Alternator carries only about half its rated output Alternator drops off line during run up If the alternator drops off line during run up check the color of the TSL Red means that the field is grounded or the Remote Voltage Sensor wire pin 8 is open b...

Page 202: ...RPM TROUBLESHOOTING VOLTAGE REGULATOR STANDBY ALTERNATOR 1 Turn all switches off Use the lowest resistance scale Ω on a DVM Digital Volt Meter Check resist ance between the battery negative terminal and both Terminal 7 of the regulator and the engine case Measurements over 0 5 Ohm to either would be cause for investigation In this case check the engine ground strap battery ground strap and regulat...

Page 203: ...ured is not close to 5 0 Volts suspect the current sensor in the standby alternator output lead 10 If the measurements in Steps 8 and 9 are satis factory prepare to monitor the voltage between termi nals 3 and 7 of the regulator with the engine running Move the aircraft to a safe location for a 2000 RPM run up Start the engine Minimize the bus loads and bring the engine RPM up to approximately 200...

Page 204: ...sion Removal A Mix one pound of baking soda bicarbonate of soda in one gallon of water B Wash battery mounting area and flush battery with mixture Do not allow soda water to enter battery cells permanent damage will result if soda mixes with electrolyte C Rinse thoroughly with clear water dry the area D Clean battery terminals with emery cloth rein stall and tighten cables Coat terminals and conne...

Page 205: ...ttery WARNING If more then 10 amps are required to trickle charge the battery the fuse will blow There is no indication of blown fuses to the pilot if this oc curs Therefore if only one battery is discharged to the point that it will not start the engine the other battery may be selected and the flight continued 2 Oil and Cylinder Head Temperature Gauge Cir cuits Both the oil and cylinder head tem...

Page 206: ...antity indicating system is comprised of two transmitters in each fuel tank inboard and outboard and is displayed on the G1000 screen 1 Fuel Pump Circuit A single auxiliary electric boost fuel pump is controlled by two switches and a relay lo cated behind PFD mtg on Air Data Computer bracket The LOW BOOST switch is utilized for engine starting procedures and to purge fuel vapors from system dur in...

Page 207: ... high Reduce charging rate by adjusting voltage regulator Electrolyte runs out of vent plugs Too much water added to battery and charging rate too high Drain battery and keep at proper level adjust voltage regulator Excessive corrosion on mounting surface Spillage from overfilling Flush area with baking soda solu tion Leaking or clogged vent line Repair or clean vent line Charging rate too high Ad...

Page 208: ...to operate Contd After seating thoroughly clean brushes and commutator to pre vent excessive wear Keep motor bearing free from sand or metal particles Dirty commutator If commutator is rough or dirty smooth and polish with No 0000 sandpaper If too rough and pitted remove commutator and turn down Blow out all foreign material Shorted grounded or open arma ture Remove and replace with an arma ture k...

Page 209: ... the location of a particular component and the exact manner in which the components are interconnected from International Avionics Incorporated IAI 3782 Arapaho Road Addison TX 75001 Telephone Number 972 247 7498 24 50 00 ELECTRICAL LOAD DISTRIBUTION 24 51 00 POWER DISTRIBUTION SYSTEM The power Buss distributes direct current power to the electrical system from the alternator and from the se lect...

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Page 211: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 25 EQUIPMENT AND FURNISHINGS ...

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Page 213: ...ANUAL Date 2006 Rev Date CHAPTER 25 EQUIPMENT AND FURNISHINGS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 25 Effectivity 1 12 06 25 Contents 3 12 06 25 00 00 5 12 06 25 10 00 6 12 06 25 10 03 7 08 10 25 10 04 8 08 10 25 EFFECTIVITY AUGUST 2010 ...

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Page 215: ... OF CONTENTS CHAPTER SECTION SUBJECT PAGE 25 00 00 General 5 25 00 01 Interior Surfaces 5 25 10 00 Flight Compartment 6 25 10 01 Seats 6 25 10 02 Seat Belts Restraints 6 25 10 03 Seat Belts Restraints Removal Installation 7 25 10 04 Cabin Lighting 8 25 50 00 Baggage Compartment 8 25 60 00 Emergency Equipment 8 25 CONTENTS ...

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Page 217: ...th com mercially available leather cleaning products Follow the instructions on the product label or A Leather Care Instructions 1 Gently dust surface area regularly with a dry soft cloth Due to the natural characteristics of leather scratches and marks may appear on the surface over time This appearance is the character of natural leather 2 Use a clean slightly damp cloth with clear lukewarm wate...

Page 218: ...ight of aircraft centerline on forward spar This al lows adjustment from approximately 10o to 40o recline position The pilot and co pilot seats may be removed by remov ing seat track pins or bolts forward and aft push seat forward to lift up front of seat structure then aft to lift up rear rollers of seat structure Installation is the reverse of removal 25 10 02 SEAT BELTS RESTRAINTS 1 General A S...

Page 219: ...ght or use a direct heat source B Inflatable Airbag Restraint System Cleaning Optional Restraint System CAUTION INFLATABLE AIRBAG RESTRAINT SYSTEMS Do not immerse the airbag belt assembly into water Moisture may damage internal compo nents and cause component failure CAUTION Restraint Systems incorporating inflatable airbag technology may NOT be dry cleaned under any circumstances 1 Refer to the R...

Page 220: ...consists of these core compo nents S Seatbelt Airbag Assembly SAA S Inflator Assembly S Electronics Module Assembly EMA S Cable Interface Assembly The SAA 1A 1B 1C 1D consists of two primary sub assemblies the Three Point Airbag Belt Assy 10A 10B 10C 10D with Safety Cable Tie and the End Re lease Buckle Assy 20A 20B 20C 20D see Figure 25 1 The SAA mounts to seat and aircraft structure using existi...

Page 221: ...wer source which is user replaceable To perform properly the SDT needs to be re calibrated yearly by the OEM Refer to program specific Am Safe s Supplemental Maintenance Manual for return information This test tool does not contain any self annunciated testing hardware and is repairable only by the OEM or the OEM s designated repair facility The AAIR System is a self contained modular re straint s...

Page 222: ...THOR OUGHLY FAMILIAR WITH ALL WARNINGS CAU TIONARY STATEMENTS AND DIRECTIVES CON CERNING THE AAIR SYSTEM AS FOUND IN AMSAFE S SUPPLEMENTAL MAINTENANCE MANUAL OR AIRCRAFT OEM MAINTENANCE MANUAL FAILURE TO DO THIS MAY RESULT IN INADVERTENT AIRBAG DEPLOYMENT WHICH CAN RESULT IN SEVERE PERSONAL INJURY AND EQUIPMENT DAMAGE 1 The AAIR Diagnostic Check provides a system functional analysis of the AAIR ci...

Page 223: ...luminates 4 Unbuckle seatbelt 5 Repeat Step 3 for next seat position 6 Unbuckle seatbelt Turn SDT ON OFF switch to OFF If finished testing all seat positions in aircraft replace the diagnostic protective cap or cover Otherwise start at Step 2 for next seat test AAIR System testing complete NOTE It is required after completion of functional test ing to document this task as an entry in the aircraft...

Page 224: ...ount of fray exceeds 10 of the width of the webbing and exceeds 8 inches in length S Webbing with more than 15 broken yarns in loca tions other than the edge Webbing that is frayed or distorted sufficiently to cause improper operation of any portion of the re straint system Check seat belt hardware end fittings buckle con nector for S Cracks S Dents S Corrosion If any cracks are visible on the sea...

Page 225: ...ith a damp wrung out washing cloth Do not leave residue on cleaned areas Rinse if neces sary with clear water on a damp wrung out washing cloth Hand wash the webbing and gas hose Gentle scrubbing with a soft brush and cold soapy solution is permissible Air dry the belt assembly Do not dry the belt assembly in sunlight or near any source of heat For airbag cover cleaning please refer to Garrett Lea...

Page 226: ...ator by squeezing both sides of the connector and gently pull ing away from the Inflator Figure 25 3 SQUIB CONNECTOR INFLATOR HOSE FITTING ELECTRICAL AND HOSE CONNECTOR OF IN FLATOR ASSEMBLY FIGURE 25 3 CAUTION If replacement of Three Point Airbag Belt is not immediately possible cover Inflator hose connector to protect from debris 2 Disconnect the gas hose s from the Inflator Assy s The gas hose ...

Page 227: ... for airbag connector tongue at this time CAUTION Check orientation of Three Point Seatbelt Airbag Belt s before inserting gas hose into Inflator Gas hose should be protruding on top of seatbelt attachment hardware Airbag cover must present away from occupant label orientation is on in side towards occupant for Aftermarket installa tions refer to AmSafe Installation drawings 509760 pilot co pilot ...

Page 228: ...vidual overhead cabin lights are controlled by rocker switches located on each passenger s arm rest excluding front seat passenger The rockers switches control light ON OFF and DIM Front seat passenger s light switch is located forward of the cabin door hinge on the interior side panel A 24 volt baggage compartment light is located in the baggage compartment left hand headliner and is con trolled ...

Page 229: ...ubjected to maintenance not more than one year apart or when specifically indicated by an inspection Maintenance is a thorough examina tion of the extinguisher covering mechanical parts ex tinguishing agent and expelling means It is intended to give maximum assurance that an extinguisher will op erate effectively and safely and should be done profes sionally Most authorities require special tags b...

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Page 231: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 27 FLIGHT CONTROLS ...

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Page 233: ...E DATE 27 Effectivity 1 12 06 27 Contents 3 12 06 27 00 00 5 08 10 27 20 00 6 08 10 27 20 00 7 12 06 27 20 00 8 12 06 27 30 00 9 12 06 27 30 03 10 12 06 27 40 01 11 12 06 27 40 02 12 12 06 27 40 02 13 12 06 27 41 00 14 12 06 27 50 00 15 12 06 27 60 00 16 12 06 27 92 00 17 12 06 27 95 01 18 08 10 27 96 03 19 08 10 27 97 01 20 12 06 27 EFFECTIVITY AUGUST 2010 ...

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Page 235: ...im System Opt 13 27 50 00 Wing Flap System Rigging 14 27 60 00 Aileron Rudder Interconnect System 15 27 90 00 Miscellaneous 15 27 91 00 Control Surface Static Balancing 15 27 92 00 Equipment Materials Static Balancing 16 27 93 00 General Procedures Static Balancing 16 27 93 01 Detail Procedures Static Balancing 16 27 94 00 Control Surface Trailing Edge 16 27 95 00 Stall Warning Maintenance Practic...

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Page 237: ...unter weights static balance the ai lerons 1 Aileron Removal and Installation A Remove control tube attaching bolt nut and washer at aileron horn B Remove bolts nuts and washers from the three attaching hinges C Remove aileron by pulling it straight aft until hinges are clear rotate inboard portion down and for ward to allow aileron balance weights to clear wing tip D Reinstall aileron in reverse ...

Page 238: ...E BOB WEIGHT YOKE CONTROL SHAFT CONTROL TUBE CONTROL YOKE H YOKE CONTROL SHAFT JACKSHAFT ASSY CONTROL TUBE BELLCRANK ASSY E BELLCRANK ASSY YOKE CONTROL SHAFT H C JACKSHAFT ASSY B CONTROL TUBE B CONTROL TUBE AILERON CONTROL LINK ELEVATOR CONTROL TUBE RIG PIN 3 16 RIG PIN HOLE PIN INSERTED FOR CLARITY BELLCRANK ASSY REF AILERON RIG PIN AILERON ELEVATOR CONTROL WHEEL RIGGING FIGURE 27 1 27 20 00 AUGU...

Page 239: ...L ADJUSTMENT FIGURE 27 4 2 Rudder Rigging and Adjustment A Raise aircraft nose wheel off ground See Sec tion 7 10 00 B Set stabilizer trim control in neutral position sta bilizer parallel with aircraft center line C Clamp pilot s rudder pedals A Fig 27 4 in neutral position D Adjust AFT rod end bearing indicated at position B Figure 27 4 approx 11 turns out to start AFT R27 5 L 1 C RUDDER ELEVATOR...

Page 240: ...LEVATOR STOP ADJUSTMENT FIGURE 27 7 K After setting stops re tighten all jam nuts bolts and secure recheck all travel limits L Center nose wheel by removing nut washer and bolt 1 Fig 27 8 and adjusting steering idler linkage at 2 Bolts nuts and washers 5 and 6 must be installed as shown from rear to front Refer to Section 32 50 00 for Nose Gear Steering and Tracking adjust ments NOTE Measure rudde...

Page 241: ...al stabi lizer Adjust rod end bearings 9 Fig 27 9 at elevator horns 2 Elevator Rigging and Adjustment R27 10 B ELEVATOR TRIM ADJUSTMENT FIGURE 27 10 NOTE Measure elevator travel from 0 degrees stabilizer thrust line with travel board positioned at stabi lizer station 16 00 as indicated on travel board P N GSE 030004 503 and with stabilizer at 0 de grees See Fig 27 3 and Fig 27 10 for travel board ...

Page 242: ...ng the Stabilizer Trim Torque Tube surface during Horizontal Sta bilizer trimming movement Scoring of the Stabi lizer Trim Torque Tube could result if attaching hardware is installed incorrectly The threaded end of the bolt Fig 27 11 Detail A should be inserted from aircraft left side to aircraft right side threaded end pointing in the outboard direction away from the Stabilizer Trim Torque Tube a...

Page 243: ...gging The indicator is connected to the trim control wheel as sembly to indicate stabilizer position relative to the air craft thrust line A Adjust stabilizer trim to FULL DOWN position B Adjust potentiometer on trim wheel assembly per rigging instructions provided in the Garmin G1000 Maintenance Manual 3 Stabilizer Free Play Limits A Fore and aft movement at stabilizer tip 12 inches B Vertical mo...

Page 244: ... trim G Wrap cable around capstan five full turns with forward eye of cable ending up 12 inches from forward circumference edge of capstan See Fig 27 14 Aft end of cable will be in proper location for rigging proce dure Temporarily secure cable capstan position using several wraps of suitable adhesive tape around cable and capstan H Extend and secure both springs to 9 8 inches in side measurement ...

Page 245: ...vice or complete remaining maintenance action 27 41 00 Stabilizer Trim System Troubleshoot ing BINDING Check control tubes at bulk head grommets for rub marks Check Trim Actuator threads for galling or not lubricated Lubricate per Sect 5 ELECTRIC CLUTCH SLIP PING Check BINDING symptoms above Check for proper clutch set tings per vendor instruc tions Confirm full bus voltage is available at trim mo...

Page 246: ...ricants prescribed in CHAPTER 5 The flap system incorporates a preselect feature which allows flaps to be activated as desired UP TAKEOFF or DOWN The flap switch is located on center console Flap posi tion is indicated on the Garmin G1000 Engine Airframe Indicator display screen The flaps can be retracted completely by placing the switch in the UP position or to any preselect setting Refer to the ...

Page 247: ...Rudder Interconnect System Rigging Fig 27 17 A With controls in neutral position locate bracket on center aileron control tube so that the end of bell crank assembly will be 7 25 inch AFT of fuselage bulk head B Holding both rudder and aileron controls in neu tral position install springs on bellcrank and stops Position stops on rudder control tube so that installed length of each spring is 4 90 i...

Page 248: ...nced with the Con trol Horn pointing upward 4 All control surfaces are balanced with the hinge center line and the tip rib chord line level Two tooling holes are located in the tip ribs and are on the rib chord line rib center line Chordwise level can be obtained by using a spirit level and pins inserted into these tool ing holes Fig 27 18 5 Install a 1 4 inch bolt or pin through the inboard and o...

Page 249: ...ted when the airplane is test flown at the factory Should it require readjusting proceed as follows A Locate switch installation on under surface of left wing leading edge and loosen the two phillips head screws one on either side of the vane B If stall warning has been activating too early pull vane BACK and DOWN NOTE NEVER TRY TO ADJUST SWITCH BY BENDING VANE This part has been heat treated and ...

Page 250: ...ARTRIDGE RE MOVAL AND REPLACEMENT MOUNTING SCREWS CARTRIDGE ASSEMBLY LOWER SUPPORT BRACKET R27 25 SPEEDBRAKE PRECISE FLIGHT SERIES 2000 FIGURE 27 22 1 REMOVAL A Remove fourteen screws from cartridge cover plate on top of wing B Lift cartridge assembly out of wing cavity C Disconnect electrical connector from cartridge D Slide drain tube out of wing bottom surface 2 INSTALLATION A Reverse removal p...

Page 251: ...neath the avionics rack The cable tension is factory set at 15 In Lbs 2 During normal aircraft operation the tension of the cable may diminish do to temperature variations and cable stretch Verify cable tension and adjust to high side 17 In Lbs if neces sary In addition verify all S TEC electrical connections are secure Partially connected harnesses may damage connector pins and provide erroneous ...

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Page 253: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 28 FUEL ...

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Page 255: ...AGES CHAPTER SECTION SUBJECT PAGE DATE 28 Effectivity 1 12 06 28 Contents 3 12 06 28 00 00 5 12 06 28 00 01 6 08 10 28 00 01 7 08 10 28 10 00 8 08 10 28 11 00 9 08 10 28 11 00 10 08 10 28 12 00 11 08 10 28 13 00 12 08 10 28 22 00 13 08 10 28 42 00 14 08 10 28 91 00 15 08 10 28 92 00 16 08 10 28 EFFECTIVITY AUGUST 2010 ...

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Page 257: ...s Bubble Fluid Formula Preparation for Leak Check 12 28 14 00 Fuel Additives 12 28 20 00 Distribution 12 28 21 00 Fuel Boost Pump Removal Install 12 28 22 00 Gascolator Screen Cleaning 13 28 23 00 Fuel Injection System 13 28 24 00 Engine Priming 13 28 25 00 Fuel Selector Valve Removal Install 13 28 30 00 Fuel Dump 13 28 31 00 Fuel System Drains 13 28 32 00 Fuel Vents 13 28 40 00 Indicating 13 28 4...

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Page 259: ... back through the fuel selector valve and returned to the source fuel tank FUEL CHECK VENT OUTBOARD OUTLET SCREEN DRAIN LEFT FUEL TANK SELECTOR VALVE FIREWALL INDICATOR FUEL FLOW FUEL FLOW TRANSDUCER FUEL METERING UNIT FUEL PUMP ENGINE DRIVEN GASCOLATOR DRAIN ELECTRIC FUEL PUMP FILLER CAP VENT R FUEL QTY L FUEL QTY INBOARD OUTLET RIGHT FUEL TANK DRAIN VALVE FILLER SCREEN ASSY INDICATOR INDICATOR A...

Page 260: ...he O ring 4 that seals this shaft WARNING Water can enter the fuel tank through a loose fit ting or damaged cap This should be corrected as soon as possible 3 The sealing capability of each cap assembly should be checked periodically and at each annual in spection This can be accomplished per the following procedures A Remove cap assembly from wing filler port and inspect O ring 1 for damage crack...

Page 261: ... Cotter Pin Puller which Shaw Aero purchases locally from MAT CO Tools 1 Place one end of the lanyard onto the tip of the tool 2 Slide end of the lanyard down the neck of the tool to stretch open the hole 3 Place stretched hole of the lanyard onto one side of the T clip 4 Place tool through hole alongside of the T clip 5 Rotating tool stretch lanyard over other end of T clip 6 Installation complet...

Page 262: ... Glendale CA 91209 or Chem Seal Corp 11120 Sherman Way Sun Valley CA 91352 2 Handling and Mixing Sealants A Sealant Material Characteristics 1 Application life is the time that the mixed com pound remains suitable for application Application life ratings are always based on standard atmospheric conditions of 75o F and 50 relative humidity For ev ery 10o F rise in temperature application life and c...

Page 263: ...2 10 45 1 2 PR1422 B 2 36 72 2 CS3204 B 1 2 8 30 1 2 CS3204 B 2 24 72 2 CS3204 B 4 36 76 4 Follow procedures with sealant kits to properly seal tanks c Access Door Sealant except on wing walk access panel CLASS B Tack Free Time HOURS Cure Rate HOURS Application Life HOURS CS 3330 B 8 16 2 PR1403 G B2 10 48 2 PR1428 B 8 16 2 d Brushable Top Coat Protective Sealant Tack Free Time HOURS Cure Rate HOU...

Page 264: ...extruded sealant will pack tightly 2 Use a spatula to pack sealant firmly in place while working out air pockets Shape each fillet evenly C Brush Sealing 1 Brush sealant PR 1422 A 1 2 A 2 or CS3204 A 1 2 A 2 over all seams rivets nuts and bolts A one inch stiff bristle brush is recommended for sealant application Force sealant into all gaps with brush strokes parallel to seams Use a circular brush...

Page 265: ...ir stream should be repaired before the next flight 3 Leak Detection A External Leak Detection after Refueling To be able to trace a leak from where it appears on an outer tank or wing skin to its true source inside the tank the exact point where fuel is escaping from tank must be determined 1 Use compressed air to blow and evaporate fuel from seams and crevices of leak area Attempt to define exac...

Page 266: ...be blended into exist ing fillets with a spatula or an appropriate tool 6 Allow all repaired sealant to cure tack free and apply two brush coats of PR 1005 L to repair area Refer to paragraph 28 11 00 4 D 28 13 00 SOAPLESS BUBBLE FLUID FORMU LA PREPARATION FOR LEAK CHECK CAUTION Soapless bubble fluid is slightly corrosive and must be completely removed by washing freely with water followed by scru...

Page 267: ...onnect fuel line at outlet of fuel pump and use boost pump with appropriate fittings and hoses to transfer fuel from both tanks into a suit able storage container Isolate aircraft to outdoor secure area Keep aircraft away from ignition source Ground aircraft and any external fuel pump system if used properly Use suitable container s for fuel storage Have operating fire extinguisher and authorized ...

Page 268: ...rt the transmitter mounting flange and cause a transmitter malfunction E Make certain the wire from outboard transmitter goes under head of insulating sleeve against the in board transmitter flange and not under the mounting screw head F System voltage should NOT BE APPLIED to the transmitter terminal The excitation from the fuel quan tity indicator must be current and voltage limited and in capab...

Page 269: ...rebuild pump In spect fuel lines and connections for leakage and dam age Fuel selector not in proper position Select proper position Air leak in system Repair leak Refer to Garmin G1000 service literature for additional Fuel System Troubleshooting 28 92 00 FLARED FITTINGS When installing flared fittings and hoses make sure threads are properly lubricated with W P petrolatum Figure 28 6 When previo...

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Page 271: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 30 ICE PROTECTION ...

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Page 273: ...VE PAGES CHAPTER SECTION SUBJECT PAGE DATE 30 Effectivity 1 12 06 30 Contents 3 12 06 30 00 00 5 08 10 30 12 00 6 08 10 30 12 01 7 12 06 30 12 01 8 12 06 30 12 02 9 12 06 30 12 02 10 12 06 30 12 02 11 12 06 30 12 02 12 12 06 30 12 02 13 12 06 30 12 02 14 12 06 30 12 03 15 08 10 30 60 00 16 12 06 30 EFFECTIVITY AUGUST 2010 ...

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Page 275: ... Airframe Ice Protection 5 30 11 01 Washing 5 30 11 02 Lubrication 5 30 11 03 Electrical 5 30 12 00 Maintenance Airframe Icing Protection 5 30 12 00 Airframe Ice Protection Electrical Schematic 6 30 12 01 Troubleshooting 7 30 12 02 Maintenance Practices 9 30 12 03 Fluid Level Calibration 15 30 30 00 Pitot Ice Removal Description Operation 15 30 31 00 Stall Warning Vane Heated 15 30 60 00 Propeller...

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Page 277: ...ns moisture Residual fluid that is not washed from the aircraft at recom mended intervals can get into skin laps and other faying surfaces and hold moisture This may eventually dis solve lubricants and break down corrosion protection coatings Solid particles of various foreign materials may attach themselves to the fluid and cause corrosive action of adjacent structural or rotating components 30 1...

Page 278: ...t procedure with both metering pumps 4 Operate Windshield Spray bar on each windshield pump to ensure proper operation and absence of leaks 5 Filter is located at baggage floor stiffener Inspect system filter and replace as needed A The high pressure LED will illuminate YEL LOW if the filter element requires replacing It should NOT illuminate during testing but may be tripped ON occasionally durin...

Page 279: ... ICING PROTECTION FLUID SCHEMATIC FIGURE 30 2 30 12 01 TROUBLESHOOTING AIRFRAME ICING PROTECTION TROUBLE PROBABLE CAUSE REMEDY Airframe Propeller system does not operate Tank contents inadequate Replenish fluid contents High Pressure Warning LED illumi nated Renew Filter Element Pump s inoperative Check electrical power to pump s Check pump or control panel Low Pressure Warning ON Check tank conte...

Page 280: ...h no pressure applied continuity should exist through connections in use LOW PRESSURE WARNING LEDs FLASH RED When system selected ON Check System for proper operation Connect Pin 2 of connector C1 to ground C1 Pin 1 Check wiring from C1 Pin 2 to Low Pressure Warn Switch es for conti nuity Check Low Pressure Warn Switch es With System operating circuit should exist through connections in use When a...

Page 281: ...o determine the immediate serviceability of the equipment without recourse to the use of tools or special procedures Maintenance Practice Notes Check security and condition of visible components Switch on electrical power Check that contents display illuminates and stabilizes at a sensible value within 1 5 minutes Replenish tank contents if necessary for in tended flight The time taken for the dis...

Page 282: ... illuminated and stabilizes at a sensible value within 1 5 minutes Replenish tank contents if necessary If in doubt regarding accuracy of indication make cal ibration check Indicator is electronically damped and should rise from 0 0 at switch ON at an average rate of about one dis play count per second Operate Airframe Propeller system at De Ice Check that both indicator LED s flash RED then chang...

Page 283: ...V Component Checks The following checks are detailed for use in conjunction with SECTION 30 12 01 TROUBLESHOOTING In cases where components can be checked on the aircraft as an alternative to bench testing both methods are described Maintenance Practice Procedures Check fluid delivery rate from Airframe Propeller Pump 1 Fill tanks to top of filler tube Operate pump s at De Ice or Anti Ice as requi...

Page 284: ... at which each operates This pressure should not be greater than 1 5 lbf in2 0 1 bar With the switch at a pressure above the operating pressure there is to be a circuit between Pins 1 2 with a resistance not greater than 10 ohms Switch pump OFF and observe pressure when switch resets This is to be not less than 0 5 lbf in2 0 03 bar OR 2 Remove Low Pressure Switch es and bench test Check Proportion...

Page 285: ...nents be checked out prior to further troubleshooting of Solenoid Valves 1 Check Windshield Pump as detailed above Recon nect Windshield Pump to Solenoid Valve Operate pump by pressing WINDSHIELD switch on control panel Fluid should be discharged onto the windshield if not disconnect Nylon tube from outlet of Solenoid Valve and repeat test Fluid should be discharged from outlet of Solenoid Valve I...

Page 286: ...C1 2 to be 7 5 volts All pins on connector C2 as 1 5 As 1 but with WINDSHIELD 2 selected All pins zero volts except C1 3 9 11 to be aircraft voltage C1 2 to be 7 5 volts All pins on connector C2 as 1 OR 2 Remove Control Panel and bench test 6 As in 1 but with PUMP 1 selected All pins zero volts except C1 3 and 7 to be aircraft voltage C1 2 to be 7 5 volts All pins on connector C2 as 1 7 As in 1 bu...

Page 287: ...enter portion of TKS control head see Figure 30 4 Adjust POT with screwdriver until 6 2 is indicated on Fluid Level Indica tor unusable volume of fluid is 0 10 gallon 6 3 gal lons 6 Remove any spilled de icing fluid per instructions in Section 30 11 01 7 Turn aircraft power OFF 8 Place aircraft on ground 30 30 00 PITOT DESCRIPTION AND OPERA TION A standard heated pitot tube is located on left wing...

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Page 289: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 32 LANDING GEAR ...

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Page 291: ...00 6 08 10 32 10 03 7 12 06 32 10 04 8 12 06 32 12 06 9 08 10 32 20 02 10 08 10 32 30 00 11 08 10 32 30 02 12 12 06 32 30 02 13 12 06 32 30 03 14 12 06 32 30 04 15 12 06 32 30 05 16 12 06 32 30 05 17 12 06 32 30 06 18 12 06 32 31 00 19 12 06 32 40 00 20 12 06 32 40 03 21 12 06 32 40 03 22 08 10 32 40 03 23 12 06 32 41 00 24 12 06 32 50 02 25 08 10 32 50 03 26 08 10 32 80 00 27 12 06 32 82 00 28 12...

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Page 293: ...g 14 32 30 04 Emergency Gear Extension System Rigging 15 32 30 05 Landing Gear Actuator Clutch Spring R R 16 32 30 06 Ldg Gear Act Recoiler Cable Drum R R 18 32 30 07 Manual Emergency Gear Extension System 18 32 30 08 Final Checks 18 32 31 00 Troubleshooting 19 32 40 00 Wheels and Brakes 20 32 40 01 Main Wheels 20 32 40 02 Main Wheel Disassembly Assembly 20 32 40 03 Nose Wheel Disassembly Assembly...

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Page 295: ...es absorb the shock of landing and taxiing LANDING GEAR EMERGENCY EXTENSION SYS TEM Emergency gear extension is available through a manual override system This system is built into the actuator unit The disengage controls are located aft and between front seats LANDING GEAR WARNING SYSTEM The landing gear warning system provides pilot with a gear warning Voice alert Check Gear that landing gear is...

Page 296: ...t and left gear components 12 DO NOT attempt to repair any heat treated com ponent of main landing gear assembly 32 10 02 MAIN GEAR INSTALLATION 1 Lubricate wheel bearings retraction linkage and fore and aft trunnion bearings prior to installation at lu brication fittings 8 Fig 32 2 Refer to Section 5 20 07 for recommended lubricants 2 Installation of main gear is exact reversal of main gear remov...

Page 297: ...pening and that there is no binding or distortion where links attach to door Adjust linkage spacers if required Fig 32 3 Extend gear to adjust then retract to check adjustment 4 Check main gear overcenter preload torque for proper values Re rig entire landing gear system if necessary See Section 32 30 02 32 30 03 R32 4 H L J L E E UP AFT M MAIN GEAR RETRACTION TUBE ADJUSTMENT POINTS FIGURE 32 4 32...

Page 298: ...n in Figure 32 6 Verify that Stop Bolt of Stop just contacts Arm on Bell crank A If contact puts no load on Rod A then proceed to Step 4 No load on the Rod may be verified by being able to move the Rod by finger pressure or rotation If load on the Rod is indicated or no Bellcrank to Stop contact is made proceed with Steps B and C 1 35 R32 5 E D V A C B MAIN INBOARD GEAR DOOR RIGGING FIGURE 32 5 SP...

Page 299: ...AN3 bolt at rod end and AN4 bolt at block remove bungee assembly INSTALLATION 1 Raise aircraft on jacks See Section 7 10 00 2 Compress replacement bungee 250 lbs to align installation rig pin holes Insert 3 16 pin 3 Retract gear 4 Pull gear down with emergency extension until main retract bellcrank and rod end bungee line up Install proper length AN3 bolt through rod end bearing and proper length ...

Page 300: ...9 as required CAUTION Nose gear overcenter preload must be re checked after any adjustment to nose wheel ec centrics 4 Readjust nose gear door linkage as required after eccentrics have been moved K Fig 32 9 32 10 RH GEAR DOOR LH GEAR DOOR LH LINK ADJUST FRONT VIEW LOOKING AFT LINK NUT AND BEARING EXHAUST CAVITY GEAR WELL SKIN IF REQUIRED RH LINK ADJUST IF REQUIRED NOSE GEAR DOORS STANDARD ACCLAIM ...

Page 301: ... See Section 32 30 07 stopping extension the moment the GREEN Gear Down Light comes ON Gear switch in DOWN position C Measure nose gear bungee springs Fig 32 12 Deflection from zero load condition in A above must be 030 to 070 inches for each bungee D If spring deflection is not within prescribed limits adjust tube rod ends F Fig 32 9 in increments of 1 2 turns as required 9 Check main gear overce...

Page 302: ...s On outboard main gear doors disconnect springs On inboard door bellcranks disconnect springs Loosen jamb nut X on retraction tube V Fig 32 1 and back off pressure on spring W by loosening nut Y Disconnect retraction tube V from bellcrank C Fig 32 5 8 Position main retraction bellcrank A so center of forward hole in left outboard arm of bellcrank is 1 56 inches from forward face of truss at F S 3...

Page 303: ...sen Set Screw C Fig 32 15 NOTE Use 1 to 4 560252 011 Shims with 560252 009 Stop to achieve proper clearance Use 063 longer screws with each additional shim Secure screw with Blue Loctite 83 31 Grade C 18 Run actuator down and recheck retraction bell crank clearance at F S 33 Check clearance of bell cranks M Fig 32 4 and center section 19 Reconnect retraction tubes V Fig 32 1 With main gear fully e...

Page 304: ...ocking force with torque wrench 33 Read torque wrench value at the EXACT mo ment shim stock pulls loose 34 Repeat steps 30 through 34 on other side s main landing gear leg 35 Use adjusting nuts Y on retract tubes V to equalize breakaway torque values within 10 0 inch lbs Adjust torque to 250 to 280 inch lbs Ref Fig 32 1 36 Turn Master Switch ON 37 RUN GEAR DOWN ELECTRICALLY AND CHECK THAT TORQUE V...

Page 305: ...32 12 If the springs have deflected less than 030 inches or more than 070 inch es from the static dimension as recorded in Step 2 adjust the length of the bungee assembly s to bring the deflection within tolerance DISENGAGE CABLE ROUTING ACTUATOR FLOORBOARD 5 COVER 3 2 1 R32 14 RETRACTION 4 CABLE EMERGENCY GEAR EXTENSION SYSTEM FIGURE 32 16 32 30 04 EMERGENCY GEAR EXTENSION SYSTEM RIGGING DISENGAG...

Page 306: ...aft DISASSEMBLY EATON ACTUATOR 1 Remove two nuts 1 Fig 32 17 that retain the cable support bracket 2 and remove bracket and dis engage cable intact from actuator body and disengage arm 2 To avoid stripping screw heads use impact screw driver to break Loctite thread seals and remove two long screws 3 two short screws 4 3 With a razor or similar tool slice through identifica tion plate and remove re...

Page 307: ...TE Clutch assembly can now be verified for proper installation by rotating input gear 6 both CW CCW Gears should turn with moderate friction to hand torque Observe that actuator output screw jack rotates in BOTH directions In some instances the new clutch no back spring CHATTERS during electrical extension or retraction cycle Proper shimming of the no back clutch housing assembly items 6 7 8 9 10 ...

Page 308: ...ns Measure cable length from side of housing At full extend the length of cable should be 29 mini mum In retracted position cable length should be 5 to 8 long 10 Bronze clutch 13 should be inspected for dam age or wear at slot where gear assembly engages dur ing manual extension of the landing gear 11 If damaged or worn remove pin 11 from disen gage arm 12 and slide disengage arm out so bronze clu...

Page 309: ...itch for prop er adjustment and operation Does gear retract using override Check system operation Circuit breaker tripped Reset circuit breaker Actuator ball nut binding on me chanical DOWN STOPS Gear may have been extended manually ball nut is jammed tight against STOPS on motor use wrench on ball nut flat to move from STOPS Gear will not retract and gear ac tuator C B trips Manual engage handle ...

Page 310: ...emove wheel by removing cotter key nut and spacer from axle See Fig 32 19 5 Slide wheel off axle 32 40 02 MAIN WHEEL DISASSEMBLY AS SEMBLY 1 Remove snap ring 10 grease seal rings 8 and felt seals 9 See Fig 32 21 2 Remove bearings 7 3 Completely deflate tire R32 17 MAIN GEAR LEG ASSY COTTER PIN LEG ASSY NOSE GEAR NOSE TIRE NOSE WHEEL WASHERS NUT MAIN WHEEL SCREW SPACER COTTER PIN NUT TYP 3 PLCS MAI...

Page 311: ...e 5 00 x 5 Type III nose wheel tire is six ply rated To remove nose wheel 1 Remove cotter key nut and washer from axle Fig 32 18 2 Remove nose wheel 3 Installation is in reverse sequence of removal Nose wheel disassembly 1 Completely deflate tire by removing valve core 2 Remove nuts washers and wheel half retaining bolts 15 Fig 32 21 3 Separate wheel halves 13 and 14 and remove tire and tube Refer...

Page 312: ... CAUTION Do not spin bearing cones with compressed air G Clean parts in cleaning solvent and dry with oil free compressed air CAUTION Assemble brake on a clean flat surface being careful not to nick scratch or damage protective finish of brake parts H Replace linings and rivets Rivet shanks must be rolled with special tool Cleveland Rivet Set Kit 199 1 for proper installation I Inspect brake cylin...

Page 313: ...ulic lines D Disconnect hydraulic cylinder from bracket and remove cylinder E To disassemble master cylinder Parker Hanni fin See Fig 32 22 Refer to M20TN Illustrated Parts Catalog for Master Cylinder part numbers Call MAC for parts availability 1 Unscrew and remove rod end clevis 17 nut 16 and washers 14 15 from piston rod 13 2 Remove snap ring 11 from cylinder housing assembly lift out complete ...

Page 314: ...pongy brake Air in system Bleed brake system Pressure will not hold Leak in brake system Visually check entire system for evidence of leaks Parking brake will not hold Air in system or leak in system downstream of parking brake valve See remedies above Defective parking brake valve Repair or replace the valve Brake grabs Warped or bent disc Replace disc Foreign matter locking disc Clean disc and l...

Page 315: ... between rudder and nose gear as sembly it is cause for rejection if binding occurs A gap of 003 to 020 is acceptable as is on either side of 720095 15 arm assembly If gap is greater than 020 on either side of 720095 15 arm shim as required with 720013 x shims to maintain 003 to 020 gap MAX ALLOWABLE 0 020 GAP TYP BOTH SIDES R32 23 NOSE WHEEL STOP GAP ADJUSTMENT FIGURE 32 25 4 Adjust turn limiter ...

Page 316: ...limit switch will stop the gear actuating motor when the proper force is exerted to hold the gears in the down and locked position Refer to Section 32 30 02 for proper limit switch rigging The gear down and locked position is indicated by 1 Illumination of the green gear down annunciator light The GEAR DOWN annunciator light is dimmed when ever the Navigation Light Switch is ON 2 The gear warning ...

Page 317: ...0 00 MISCELLANEOUS 32 81 00 LANDING GEAR SHOCK DISC IN SPECTION 1 Aircraft with full fuel load and weight on landing gear A Main gear shock discs Fig 32 28 1 Remove dust shield Check gap between re taining collar A and top retaining plate B Allowable gap is 0 00 to 0 85 inches 2 Replace discs when gap exceeds the toler ance Use a shock disc replacement tool C P N GSE 030038 501 Green color to remo...

Page 318: ...EAR SHOCK DISC REPLACEMENT FIGURE 32 29 32 82 00 RECOMMENDED HARD LANDING INSPECTIONS The following are areas recommended to be inspected when a hard landing or overweight landing has oc curred Since a hard landing is a relative term and an overweight landing may have occurred it is up to the owner operator to advise maintenance personnel when the inspections are to be accomplished Howev er since ...

Page 319: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 33 LIGHTS ...

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Page 321: ...HAPTER 33 LIGHTS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 33 Effectivity 1 12 06 33 Contents 3 12 06 33 00 00 5 08 10 33 10 00 6 08 10 33 10 01 7 08 10 33 23 00 8 12 06 33 40 00 9 12 06 33 41 02 10 08 10 33 41 03 11 12 06 33 43 02 12 12 06 33 EFFECTIVITY AUGUST 2010 ...

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Page 323: ...tch Replacement 7 33 22 00 Instrument Flight Panel and Glareshield Lights 7 33 22 01 Light Bulb Replacement 7 33 23 00 Gear Down Indicator Light Floorboard 8 33 23 01 Light Bulb Replacement 8 33 40 00 Exterior Lights Maintenance Practices 8 33 40 01 Troubleshooting Exterior Lights 8 33 41 00 High Intensity Strobe Lights Maintenance 9 33 41 01 Power Supply ies Unit Removal Replace 9 33 41 02 Power ...

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Page 325: ... either the ON AND OFF position CAUTION The cabin light rocker switches are connected directly to the battery NOTE These cabin lights are connected directly to bat tery and will illuminate when pushed ON with aircraft Master Switch OFF and cabin interior Master Light Switch ON All passenger overhead lights are controlled by the Master Light switch located on the pilot s arm rest With Master Light ...

Page 326: ...roluminescent switch pan el by removing the six 6 screws mounting the O H switch panel to the headliner Figure 33 1 2 Switches are a snap fit and may be removed by pressing snap tabs and pushing switch through cover 3 Disconnect wires from Electroluminescent panel harness and replace with new panel Check for proper operation Figure 33 2 4 Reassemble switch assemblies into new panel by snapping in ...

Page 327: ... Remove cover from side panel by removing two 2 screws holding cover to side panel 3 Press snap tab push switch from panel to re move 4 Re assemble in reverse order when complete with maintenance action BAGGAGE COMPARTMENT SWITCH 1 Switch is located at rear of baggage door at front top of hat rack opening Figure 33 1 2 Remove one screw inboard of switch on door frame trim Pull door frame down slig...

Page 328: ...RIOR LIGHTS TROUBLE PROBABLE CAUSE REMEDY STROBE LIGHTS Lights inoperative Circuit breaker switch tripped Check for short circuit Reset circuit breaker Loose connection Check and tighten electrical con nections Battery defective Replace battery or use external power Circuit breaker switch defective Check continuity through switch replace if necessary Faulty power supply Disconnect synch wires to i...

Page 329: ...s or circuit breaker If input voltage is present disconnect connector to flashtube 400 500VDC should be pres ent across Pin 1 and 3 of power supply If not power supply has no output and is defective Turn Master Switch OFF replace power supply 2 If voltage is present across Pin 1 and 3 of power supply connect a known good flashtube to power sup ply If good flashtube fails to operate power supply is...

Page 330: ...s a set screw securing the bulb to the mounting pate to be loosened from mounting plate B Remove three screws 3 that secure the mount ing plate light assembly to the wing tip Pull base plate away from wing tip to expose wiring harness and con nectors WARNING High voltage is involved in circuit between power supply and strobe light assemblies Although a bleed off resistor is incorporated in power s...

Page 331: ...e wheel 7 ft 6 in from wall Position L H R H main landing gear at exact distance from vertical wall i e parallel to wall 2 Place four target crosses on vertical wall at the following positions A Measure 36 5 inches UP on vertical wall from same ground plane aircraft is resting on B At 9 85 feet left and right of nose wheel center line C At 12 375 inches further outboard on both left right side of ...

Page 332: ...om your hands or other maintenance processes Failure to wear clean gloves or wiping the bulb off may result in pre mature bulb failure due to hot spots that will build up from any grease residue on the bulb WARNING When using isopropyl alcohol follow directions and warnings given by the manufacturer 7 Replace new bulb in reverse order of removal 8 Verify beam adjustment has not changed see SECTION...

Page 333: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 34 NAVIGATION AND PITOT STATIC ...

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Page 335: ... 2006 Rev Date CHAPTER 34 NAVIGATION LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 34 Effectivity 1 12 06 34 Contents 3 12 06 34 00 00 5 12 06 34 10 01 6 08 10 34 12 01 7 12 06 34 20 00 8 12 06 34 22 02 9 12 06 34 90 00 10 12 06 34 EFFECTIVITY AUGUST 2010 ...

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Page 337: ...ator Troubleshooting 6 34 12 00 Vertical Speed Indicator 6 34 12 01 Rate Of Climb Indicator Troubleshooting Vertical Speed Indicator 7 34 13 00 Altimeter 7 34 13 01 Altimeter Troubleshooting 7 34 20 00 Horizontal Situation Indicator HSI 8 34 21 00 Slip Skid Indicator 8 34 22 00 Magnetic Compass 8 34 22 01 Demagnetizing and Compass Swinging 8 34 22 02 Compass Troubleshooting 9 34 23 00 Attitude Ind...

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Page 339: ...ture and obstructions Drain Pitot and static systems after humid or wet weather If instrument operation is erratic or inoperative after draining perform the following 1 Pitot system hose inspections Inspect hose sec tions for signs of deterioration Check all tubing for brittleness checks or cracks particularly at bends or connecting points When new hose is installed check system for leaks using PI...

Page 340: ...e a black pointer The pointer remains black until reaching never exceed speed Vne at which point it turns red Speed Ranges A color coded white green yellow and red speed range strip is located on the moving tape The colors denote Flaps Operating Range 59 110 KIAS Normal Operating Range 66 173 KIAS Caution Range 174 194 KIAS Never Exceed Speed Vne 194 KIAS A red range is also present for low speed ...

Page 341: ...l window Kollsman in face of main dial to indicate local barometric pressure This corrects altimeter reading for prevailing conditions The Altimeter provided in the Garmin G1000 PDF dis plays barometric altitude values in feet on a rolling num ber gauge The Altimeter displays the following infor mation Altitude values Altitude reference bug Altitude trend vector Altitude reference box Barometric s...

Page 342: ...ss cannot be compensated within limits Care fully go over entire steel structure with degausser from center to outboard of structure Left Right to remove residual magnetism It is recommended that an Arma ture Growler be used to degauss steel structure Ref 33 22 01 An Associated Growler Armature Tester No AOE 6054 or similar device may be used NOTE Check for outside magnetic influences if exces siv...

Page 343: ...If compass does not read within 10 at any heading proceed to de magnetize cockpit as outlined in Step 3 5 Fill out compass correction card giving Radio ON corrections through 360 Install card on or in close proximity to compass in full view of pilot 34 22 02 COMPASS TROUBLESHOOTING TRADITIONAL COMPASS TROUBLE PROBABLE CAUSE REMEDY Excessive card error Compass not properly compen sated Compensate i...

Page 344: ...000 Maintenance manual for trou bleshooting and service information 34 90 00 MISCELLANEOUS INSTRUMENTS 34 90 01 CLOCK A real time clock is integral to the Garmin G1000 Avionics System 34 90 02 OUTSIDE AIR TEMPERATURE The Garmin GTP 59 OAT Probe provides the GDC 74A with air temperature data The OAT probe is mounted to the bottom side of the right wing Refer to Garmin G1000 System Maintenance Manua...

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Page 347: ...TE 35 Effectivity 1 12 06 35 Contents 3 12 06 35 00 00 5 08 10 35 00 02 6 12 06 35 00 02 7 12 06 35 00 03 8 12 06 35 00 03 9 08 10 35 00 04 10 08 10 35 00 05 11 08 10 35 00 05 12 08 10 35 00 05 13 08 10 35 00 05 14 08 10 35 00 06 15 08 10 35 00 06 16 08 10 35 00 06 17 08 10 35 00 06 18 08 10 35 00 06 19 08 10 35 00 06 20 08 10 35 EFFECTIVITY AUGUST 2010 ...

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Page 349: ...AGE 35 00 00 General 5 35 00 01 AVOX SCOTT Recharging Procedures 5 35 00 02 AVOX SCOTT Maintenance Practices 6 35 00 03 Precise Flight Oxygen System Components 8 35 00 04 Precise Flight Oxygen System Maintenance 10 35 00 05 Precise Flight Bottle Removal Replacement 10 35 00 06 Precise Flight Oxygen Troubleshooting 14 35 CONTENTS AUGUST 2010 ...

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Page 351: ...4 Associated plumbing and fittings 5 A center console panel display and System actua tion switch 6 An overhead distribution manifold with low pres sure transducer and integrated interior LED dome light located just aft of the pilots seats and in front of the passenger seats in the overhead 7 Breathing devices and flowmeters with cannulas or masks Setting the oxygen switch to ON illuminates the dis...

Page 352: ...sing a 70 10 PSI oxygen supply plugged into one cabin out let and a test gauge plugged into another outlet Apply 70 10 PSI to system allow 2 minutes for system to stabilize remove oxygen supply Drop in pressure after 15 minutes shall not exceed 5 PSIG C Remove temporary plug located at end of line at regulator and ensure that cylinder is charged to capac ity D Conduct high pressure test using cyli...

Page 353: ...254 and deburred Then install Cable Stop in regulator lever Attach cable wire to cable stop Check for proper ON OFF position of cockpit control to make sure full travel is ob tained in order for oxygen to be completely ON or OFF Complete cable stop attachment Cut ex cess cable wire off and bend wire end over 90o A Place new cylinder regulator assembly into position in clamps secure and safety New ...

Page 354: ...t 1850 psig Regulator Assembly 2 Converts the high bottle pressure to a usable 70 psig for cabin distribution This is actuated through a latching solenoid assembly with an electrical connec tion to the aircraft cockpit The regulator assembly al lows the bottle to be filled through a separate fill port and a fill gage The fill gage allows the maintenance personnel to monitor the fill operation An o...

Page 355: ...is an electrical short or open circuit to the latching solenoid at the regulator The oxygen control ler supports these functions and ensures a short dura tion signal to drive the latching solenoid Breathing Equipment 1 The breathing equipment can consist of either constant flow and or demand flow regulator breathing stations Both use a connection to the distribution man ifold Precise Flight A4 or ...

Page 356: ...lling the system for use FILLER STATION CLEANING The filler port requires cleaning periodically and prior to filling to keep clean of dirt dust and oils to prevent fire LINE CLEANING Line Cleaning Procedure 1 Preparation a Obtain a suitable container for collecting fluid waste b Wear protective gloves and eyewear c Assemble a reservoir pump and drain line see Figure 35 3 2 Flushing a Fill 2 qt res...

Page 357: ...SCREW LOW PRESSURE FITTING CLAMP GROUND STRAP MOUNTING HARDWARE LOOKING AFT FROM STA 120 PRECISE FLIGHT OXYGEN SYSTEM BOTTLE REGULATOR FIGURE 35 7 OXYGEN FILLER DOOR RH FUSELAGE PANEL OXYGEN FILLER VALVE OXYGEN TANK PURITAN BENNETT CONNECTION PRECISE FLIGHT OXYGEN SYSTEM FILL VALVE FIGURE 35 8 35 00 05 AUGUST 2010 ...

Page 358: ...talled in the distribution ports bleed the system down to below 50psig but above 0psig 6 Repeat steps 3 5 once Leak check not required on second purge 7 Removed the flowmeters from the distribution port and turn the oxygen System OFF and fill to 1500psig 8 Perform Final leak check 9 Fill System to 1800 2000psig as required Pulse Oximeter FlightStat Optional The Non in Medical FlightStat Pulse Oxim...

Page 359: ... cases the flight test is the only approved method for testing the calibration Flight Test Method A Method A of checking the calibration is by flight test This flight is intended to be done during the mainte nance release flight following the annual inspection The procedure is to fly to 11 000ft PA alt setting of 29 92inHg and during the climb to 12 500ft PA with the oxygen system OFF note the alt...

Page 360: ...tic tester increase the static altitude slowly to 11 000ft PA Con tinue increasing the altitude and note when the display indicates O2 REQ D as signified on the display by the flashing amber LED Note the altitude which this oc curred 9 Verify the altitude where the indication first oc curred a If indication is between 11 500ft PA and 12 500ft PA then proceed to the next step b If the indication is...

Page 361: ...han 700 Yes Blinking Yes 2 PRECISE FLIGHT OXYGEN SYSTEM TROUBLE SHOOTING FLOW CHART 1 FIGURE 35 14 Re Fill Oxygen System to Over 1500 psig Re Adjust All Flowmeters to Correct Setting No Yes Yes Blinking No Steady Yes 1 2 3 No Electrical or Pressure Faults Indicated Fault Light OFF Verify Proper Oxygen System Flow Rate Proper Flow Rate Achieved with No Fault Lights Correct System Operation Steady o...

Page 362: ...t the Solenoid the reading should be 0 75 ohm at the DLA D Sub Connector No Yes PRECISE FLIGHT OXYGEN SYSTEM TROUBLE SHOOTING FLOW CHART 3 FIGURE 35 16 Install a New Mark the Bottle Yes Yes 80 psig Less Than 60 pisg 80 psig Less Than 60 pisg 3 4 5 4 5 6 Re Test the System Purge the System per Section 2 4 6 Rebuilt Regulator Bottle Assembly Assembly with a description of the problem and Contact PFI...

Page 363: ... Ground is 11 3 VDC Solenoid Wire to Ground OK Solenoid Failure Remove and Replace the Regulator Bottle Assembly Purge the Oxygen System per Section 2 4 6 Mart Regulator Bottle Assembly with Paperwork indicating Problem and Return to PFI PRECISE FLIGHT OXYGEN SYSTEM TROUBLE SHOOTING FLOW CHART 5 FIGURE 35 18 35 00 06 AUGUST 2010 ...

Page 364: ...age the latching solenoid and turn on the Oxygen flow 2 6 6 6 4 Wiring OK Check Low Pressure Transducer Wiring Fix Wiring between the Display Logic Assembly and the Low Pressure Transducer Turn System OFF Remove and Replace the Low Pressure Transducer or Distribution Manifold Turn ON the System and Re Test Fault Light Yes Steady Blinking No Steady or Blinking Fault Light Purge the System and Perfo...

Page 365: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date Page 19 PRECISE FLIGHT OXYGEN SYSTEM WIRING SCHEMATIC TYPICAL FIGURE 35 19 AUGUST 2010 35 00 06 ...

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Page 367: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 37 VACUUM ...

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Page 369: ... INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 37 VACUUM LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 37 Effectivity 1 12 06 37 Contents 3 12 06 37 00 00 5 12 06 37 00 00 6 12 06 37 EFFECTIVITY ...

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Page 371: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 37 VACUUM TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 37 00 00 General 5 37 CONTENTS ...

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Page 373: ...IATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date Page 5 37 00 00 GENERAL Garmin G1000 equipped aircraft are all electric with no vacuum system requirements on the standard aircraft 37 00 00 ...

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Page 375: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 39 ELECTRICAL PANELS ...

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Page 377: ...RICAL PANELS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 39 Effectivity 1 12 06 39 Contents 3 12 06 39 00 00 5 08 10 39 10 00 6 12 06 39 10 01 7 08 10 39 10 03 8 08 10 39 10 03 9 08 10 39 10 03 11 08 10 39 12 02 12 08 10 39 12 02 13 08 10 39 12 02 14 08 10 39 EFFECTIVITY AUGUST 2010 ...

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Page 379: ...itch 10 39 11 03 Landing Gear Safety Override Switch 10 39 11 04 Clock 11 39 12 01 Annunciator Panel 11 39 12 02 Emergency Locator Trans ELT Switch Opt 11 Ameri King AK 450 11 Ameri King AK 450 ELT Battery Install Replacement 12 Ameri King AK 450 ELT Remote Battery Install Replacement 13 Artex ME 406 14 Artex ME 406 ELT Battery Install Replacement 15 39 12 03 Instrument Radio Light Glareshield Dim...

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Page 381: ...gation For Operation Maintenance and Troubleshooting re fer to Garmin publications available in aircraft docu mentation G1000 Instructions for Continued Airworthiness G1000 Cockpit Reference Guide G1000 Configuration Manual G1000 System Maintenance Manual G1000 Airplane Flight Manual Supplement G1000 Avionics Wiring Diagram G1000 Master Data List G1000 Required Equipment List G1000 Post Installati...

Page 382: ...ponent removal instructions C For Airspeed Indicator Attitude Indicator and Al timeter removal 1 Disconnect plumbing and or electrical con nections from flight instruments to be removed 2 Disconnect and remove any post lights 3 Remove mounting screws securing instru ment to panel 4 Remove instrument by sliding it forward from panel D For Airspeed Indicator Attitude Indicator and Al timeter install...

Page 383: ...A TIT EGT CHT INSTALLATION LOOM HARNESS GDC 74 AIR DATA FORWARD HARNESS ASSY FWD TO GDC74A AFT TO GRS77 FORWARD AFT DISCONNECT SKYWATCH GRS77 WX500 FORWARD AFT DISCONNECT AFT HARNESS PITCH TRIM SERVO PITCH SERVO GDL 69A GTX 33 GIA 63 1 GIA 63 2 RACK AUXILIARY AVIONICS EQUIPMENT GRS 77 SKYWATCH TAILCONE AREA GDU 10 XX PFD GEA HARNESS FORWARD HARNESS ROLL SERVO ON GFC700 ON GFC700 ROLL SERVO ON STEC...

Page 384: ...to slide out E Panel should now tilt down to access the tray as sembly mounting screws 2 Remove the two screws from tray assembly These screws have 2 bushings that will release when tray assembly is removed F From under dash area slide tray out enough to remove mounting screws 2 and separate POSI TRONICSt connector located on backside of tray as sembly G Disconnect Alternator wire by removing moun...

Page 385: ...Map Light and Stormscope Refresh depending on Sales Order configuration See Figures 39 5 through 39 7 for typi cal configurations With aircraft Master Power Off and batteries discon nected switches and controls may be removed for re placement or service by removing retaining screws from nameplate and then detaching electrical connec tions Remove pushbutton switches by carefully pulling plastic pus...

Page 386: ...haped knob must be pulled aft prior to raising or lowering switch to activate landing gear actuator 1 Access to the switch for maintenance is from be low the bottom edge of the instrument panel 2 Disconnect wire connector attaching switch as sembly to harness 3 Unscrew wheel shaped knob counterclockwise to remove from stem 4 Remove nut and washer from face of switch and push switch through panel R...

Page 387: ... 39 12 02 EMERGENCY LOCATOR TRANSMIT TER ELT SWITCH OPTIONAL AMERI KING AK 450 R39 18 EMERGENCY LOCATOR TRANSMITTER ELT REMOTE SWITCH AMERI KING AK 450 FIGURE 39 12 The Ameri King AK 450 remote ELT switch Figure 39 12 is located on the Instrument Panel The location is determined by optional equipment per sales order The ELT is located in the tailcone Figure 39 13 and is accessible by removing radi...

Page 388: ...Reinstall Remote Switch in reverse order of re moval BATTERY INSTALLATION AND REPLACEMENT AMERI KING AK 450 ELT The Ameri King AK 450 ELT is designed to use only Duracell MN1300 Alkaline Batteries which are dated by the manufacturer WARNING The use of any other battery will void any warran ties of the ELT by Ameri King Corp The ELT does not meet the requirements of TSO C91a or FAR 91 52 if used wi...

Page 389: ...screws slight ly and push the O Ring back into place with a thin screwdriver or a flat smooth object 8 Remove any existing battery replacement date la bels from the battery case and install the new label you prepared in a readily visible location on the ELT BATTERY INSTALLATION AND REPLACEMENT AMERI KING AK 450 ELT REMOTE The ELT remote is designed to be powered by a single Duracell DL1 3NB 3 volt...

Page 390: ...ack to ARM The ELT does not have an OFF position A jumper be tween two pins on the front of the D sub connector must be in place for the G switch to activate the unit The jumper is installed on the mating half of the connec tor so that when the connector is installed the beacon is armed This allows the beacon to be handled or shipped without nuisance activation front connector removed NOTE The ELT...

Page 391: ...been pro grammed Does not indicate erroneous or corrupted programmed data 6 Flashes Indicates that the G switch loop be tween pins 5 and 12 at the D sub connector is not installed ELT will not activate during a crash Check that the harness D sub jumper is installed by verifying less than 1 ohm of resistance between pins 5 and 12 7 Flashes Indicates that the ELT battery has too much accumulated ope...

Page 392: ...other The cable should not be twisted and the connector should click into place NOTE The battery connector is keyed to prevent incorrect installation NOTE Mate the ELT to the battery making sure that the seal is positioned correctly during the process Replace the 8 securing screws and torque to 10 12 inch lbs Enter pertinent battery replacement information in the aircraft log book and fill out any...

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Page 395: ... 51 Contents 3 12 06 51 00 00 5 12 06 51 10 01 6 12 06 51 11 00 7 12 06 51 12 01 8 12 06 51 12 01 9 12 06 51 12 02 10 12 06 51 12 03 11 12 06 51 13 02 12 12 06 51 13 03 13 12 06 51 13 03 14 12 06 51 13 04 15 12 06 51 13 07 16 12 06 51 14 00 17 12 06 51 14 03 18 12 06 51 15 00 19 12 06 51 15 03 20 12 06 51 15 04 21 12 06 51 15 05 22 08 10 51 17 00 23 08 10 51 EFFECTIVITY AUGUST 2010 ...

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Page 397: ... Repair 11 51 13 03 Stub Spar Repair 13 51 13 04 Rear Spar Repair 15 51 13 05 Rib Repair 15 51 13 06 Wing Tip Repair 15 51 13 07 Wing Skin Panel Repair 15 51 14 00 Horizontal Stabilizer Vertical Fin Repair 17 51 14 01 Leading Edge Skin Repair 17 51 14 02 Main Spar Repair Outboard of STA 9 00 17 51 14 03 Rib Repair 18 51 14 04 Remating Horizontal Stabilizer to Stinger 18 51 15 00 Fiberglass Laminat...

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Page 399: ...ed to floorboard and structure beneath floorboard The M20TN features two rear passenger seat configu rations a split type rear seat using seat cushions in molded wells over wing spars and individually reclining rear seat backs or a three place bench seat 51 10 00 STRUCTURAL REPAIR GENERAL This section outlines structural repair procedures for the M20TN airplane It is intended to supplement FAA Adv...

Page 400: ... RIVET REMOVAL AND REPLACEMENT A REPLACEMENT STANDARD SIZE RIVETS HOLE OVERSIZE This repair applies only to original aluminum alloy steel or monel rivets of 1 16 3 32 1 8 and 5 32 inch diameters Such rivets may be replaced as noted and limited below and in General Limitations when hole only is oversize 1 Protruding Head Joint If edge distance is a minimum of two times diameter of original rivet it...

Page 401: ...T SIZE MAX ACCEPTABLE DRILL SIZE DIAMETRIC DIMENSION AN470AD3 or AN426AD3 40 0 098 dia 0 108 in AN470AD4 or AN426AD4 30 0 1285 dia 0 141 in MAXIMUM ALLOWABLE DIAMETRIC DIMENSIONS FIGURE 51 4 3 When a hole becomes enlarged beyond ac ceptable diametric limit and the prescribed rivet cannot be used the next larger diameter rivet may be used if a four diameter 4D rivet spacing is maintained and b two ...

Page 402: ... 1 4 of tube circumference Drill out crack smooth hole edges weld hole or dent and file repaired surface smooth Form a patch that will cover twice the diameter of tube from both edges of damaged area and twice the circumferential area of damage as shown in Figure 51 5 Weld patch in place 2 INNER SLEEVE SPLICING Use an inner sleeve splice to partially replace a tube without increasing out side diam...

Page 403: ...pair a damaged tube when parts on each side of the damage cannot be separated to insert an in ner sleeve Figure 51 7 A Form split sleeve from steel tube or sheet steel when outside diameter of original tube is less than one inch B Form split sleeve from sheet steel when outside diameter of the original tube is one inch or more C Form split sleeve from same material AISI 4130 steel condition N with...

Page 404: ...l clean up with a 20 drill may be drilled and repaired per item A C The repair of weld beads on heat treated as semblies may be accomplished without reheat treat ment within the following limits 1 The repair bead will not exceed 375 in length or 1 3 of total length of weld whichever is the lesser 2 Only one repair per weld bead is allowed 6 REPAIR OF SPOT WELDS Failed spot welds on aluminum may be...

Page 405: ...ry control system compo nent with a new part Repairing primary control system components is not recommended Use only new hard ware when installing new parts After installation of new parts check control system travel and rigging as out lined in Chapter 27 Before returning aircraft to service flight test aircraft for proper control system rigging 51 13 00 WING REPAIR 51 13 01 STRINGER REPAIR String...

Page 406: ...olt is too short the shank will not completely fill hole Repair scratches on spar caps that are not deeper than 003 inch by sanding with No 400 abrasive paper Re move no more than 005 inch of material Inspect sanded area use dye penetrant to be sure that scratch is completely removed Clean and prime area where protective coating has been removed 2 SPAR CAP REPAIR Spar caps outboard of STA 103 cons...

Page 407: ...1 13 03 STUB SPAR REPAIR Stub spar splice at wing STA 34 5 3 0 1 Cut stub spar halfway between existing rivets as required by damage incurred Figure 51 13 2 Smooth all rough or sharp edges and prime area to be spliced 3 Locate new outboard section and trim splice to fit with a maximum gap of 020 inch 4 Fabricate 501 angles to pick up 30 existing fas tener holes 30 recommended but 22 minimum 503 an...

Page 408: ...03 PLATE R51 13 18 AN 470 AD5 RIVETS EACH SIDE OF SPLICE 503 REF W S 43 5 20 0 COND N STEEL 503 FLAT PATTERN 040 AISI 4130 COND N STEEL 501 FLAT PATTERN 091 AISI C 130 28 0 1 56 74 1 07 1 66 SECT A A THRU SKIN AND 503 10 AN 470 AD4 RIVETS CAPS AND 501 ANGLES TO ADS THRU SPAR STEP UP AN426 AD4 THIS AREA 210055 CAP REF DETAIL A W S 21 75 A L STUB SPAR REF SECT B B AIRPLANE C 82 505 PLATE REF 98 501 ...

Page 409: ...2248 blind rivets in places inaccessible for rivet bucking Add one extra counter sunk blind rivet between every other pair of cherrylock rivets 51 13 07 WING SKIN PANEL REPAIR Repair wing skin panels as prescribed in AC 43 13 unless an entire skin panel is to be replaced Install new skin panels to exactly match original skin installation Preformed skin panels may be obtained from any Mooney Servic...

Page 410: ...into surrounding skin can be repaired as follows A Stop drill crack with No 60 bit B Cut doubler from same material as skin to be re paired Allow for six rivets at four diameter rivet spac ings with two diameter edge distances in a circular pat tern around cracked dimple C Round corners of doubler and scarf sand wiched edges to about 010 inch by 250 inch D Drill holes for six rivets same size as t...

Page 411: ...T 9 0 OUTBD FIGURE 51 20 2 Repair main spar cap damage between STA 34 and STA 48 5 by forming a splice angle from 3 4 inch by 3 4 inch 050 2024 T3 sheet aluminum Figure 51 20 Pick up five existing holes and drill six new rivet holes between existing holes in the skin on each side of dam aged area Install 11 AD4 rivets through angle and skin and 10 AD4 rivets through angle and web on each side of t...

Page 412: ...WAGE SET 5 6 STRAIGHT HUCK STUMP STUMP DRIVE HUCK STEP 1 SWAGE SET R51 24 RIVET GUN SWAGE SET BENT 5 HUCK COLLAR RIVET GUN INSTALL STEP 2 COLLAR BUCKING BAR COLLAR SWAGE STEP 3 REMATING HORIZONTAL STABILIZER TO STRINGER FIGURE 51 24 51 14 03 RIB REPAIR The repair of damaged stabilizer and fin ribs is not fea sible in most cases Damaged ribs should be replaced with new parts 51 14 04 REMATING HORIZ...

Page 413: ... in Figure 51 26 Figure 51 27 and Figure 51 28 4 Prior to continuing the repair all surfaces in the area of the repair must be cleaned of all contaminates by wiping the area with a clean cloth saturated with Methyl Ethyl Ketone CAUTION Methyl Ethyl Ketone M E K is a flammable liq uid and should be used with proper ventilation and the prescribed safety equipment CAUTION Fiberglass components are at...

Page 414: ...ifications and apply to appearance surface area Care should be taken to assure as smooth as possible surface in this particular operation Permit this surfacing coat to cure prior to any additional applications or further rework CAUTION When sanding and working with fiberglass wear full eye protection ear protection and a respira tor or mask to protect you from airborne fiber glass particles 11 Usi...

Page 415: ...e repaired area while still wet This prevents adhesion to the pressure clamp application paragraph 6 6 Place rigid aluminum plates on both sides of repair area and clamp into place with C clamps Permit lami nate repair to cure 7 After fiberglass repair has cured remove clamps and install 3 AN426 rivets Flush head to be on fin ished surface side The number of rivets and spacing will be determined b...

Page 416: ...rd practices 51 16 00 CARBON FIBER REPAIR The upper and lower cowl assembly base material is preimpregnated fiber reinforced composite laminate carbon fiber prepreg Superficial damage may be buffed out Damage resulting in penetration of the pan el disruption of the carbon fibers or delamination will require replacement of the component CAUTION Extreme caution should be taken when trimming carbon f...

Page 417: ...llowing the illustration depicting the as sembly or component in question If splices are made the system must be checked for leaks 3 Shortening and Lengthening of Tubing Hoses and Flexible Ducting Mooney manufactured assem blies of plumbing tubing hoses and flexible ducting may be modified to allow the use of longer parts of the same size and material to be cut and used as replace ments When the m...

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Page 419: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 52 DOORS ...

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Page 421: ...te 2006 Rev Date CHAPTER 52 DOORS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 52 Effectivity 1 12 06 52 Contents 3 12 06 52 00 00 5 12 06 52 10 00 6 12 06 52 11 00 7 12 06 52 31 00 8 12 06 52 60 00 9 08 10 52 60 00 10 08 10 52 EFFECTIVITY AUGUST 2010 ...

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Page 423: ...R SECTION SUBJECT PAGE 52 00 00 General 5 52 10 00 Cabin Door Maintenance Practices 5 52 11 00 Cabin Door Rigging Adjustment Procedures 7 52 12 00 Cabin Door Seal 7 52 30 00 Baggage Compt Door Maintenance Practices 7 52 31 00 Baggage Compt Door Latching Mechanism 8 52 60 00 Entrance Step Assembly 9 52 CONTENTS AUGUST 2010 ...

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Page 425: ...ov al if door locks are to be removed and replaced 52 10 00 CABIN DOOR MAINTENANCE PRACTICES 1 Removal The cabin door may be removed to re place or repair door or to replace a damaged hinge A Remove interior panel around forward door frame B Remove hold open arm at door frame Remove cotter pin and washers from hold open arm shaft Pull shaft up from doubler plate and clear of door frame C Remove ei...

Page 426: ...positioned between outer skin and mounting plate B When door is properly positioned in door frame mark new hinge for mounting using existing holes ei ther from outer skin locations or from hinge mounting plate inside cabin C Drill new holes in hinge carefully while door is securely in place D Remove door deburr holes and clean shavings from area NOTE The rivets and rivet holes originally used as l...

Page 427: ...e cam at end of its full travel NOTE Slide cam 7 moves 1 13 in from full latched to full open position 52 12 00 CABIN DOOR SEAL The cabin door seal is an extruded rubber seal filled with soft foam Unless deformed or torn seal will pro vide adequate sealing around periphery of cabin door during flight conditions 1 Cabin door seal replacement A The seal is held to inner door frame with adhe sive B R...

Page 428: ... assembly F Apply sealant PR1321 B2 or equivalent to hinge mounting flange and between outer skin and door frame G Reinstall door assembly and cleco securely in place H Install rivets AD4 standard AD5 oversize in all holes Remove clecoes as rivets are being installed to keep door aligned 52 31 00 BAGGAGE COMPARTMENT DOOR LATCHING MECHANISM The baggage compartment door has a direct non ad justable ...

Page 429: ...d or installed by a certified aircraft mechanic If the step is installed decrease the true airspeed at normal cruise power setting by approximately 1 KTAS To remove install step 1 Loosen belly panel camlocs and remove panel to ac cess removeable step mounting hardware 2 Remove mounting hardware attaching step to retain er mount and slide step outward 3 Insert plug assembly into retainer and mount ...

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Page 431: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 53 FUSELAGE ...

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Page 433: ...AL Date 2006 Rev Date CHAPTER 53 FUSELAGE LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 53 Effectivity 1 12 06 53 Contents 3 12 06 53 00 00 5 12 06 53 40 03 6 12 06 53 40 03 7 12 06 53 40 03 8 12 06 53 40 03 9 12 06 53 40 03 10 12 06 53 EFFECTIVITY ...

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Page 435: ...APTER SECTION SUBJECT PAGE 53 00 00 General 5 53 10 00 Main Frame 5 53 10 01 Tubular Structure Frame 5 53 10 02 Tailcone Structure 5 53 20 00 Firewall 5 53 30 00 Plates Skins 5 53 40 00 Attach Fittings 5 53 40 01 Wing Attach Fittings 5 53 40 02 Empennage Attach Fittings 5 53 40 03 Engine Mount Attach Points 6 53 CONTENTS ...

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Page 437: ...ulation and vinyl are placed between firewall and cabin interior to restrict engine compartment heat and noise All engine compartment cabin access holes are sealed tight to prevent fire and smoke in cabin Reference Section 71 30 00 for sealing procedures 53 30 00 PLATES SKINS The fuselage tubular structure is covered with alumi num skins after mating to tailcone The skins are riv eted and bolted t...

Page 438: ...ucture The upper and outboard lower hard points 1 2 Figure 53 7 are for NAS1304 bolts installed for ten sion loads Lower hard points 3 are for shear loads and are used in conjunction w attachment of nose landing gear lower truss assembly Figure 53 7 AN6 bolts are installed at this location Lower hard points 4 are for fittings outside firewall which allow a clevis on each side of engine mount to be...

Page 439: ...UDDER CONTROLS ELEVATORS RUDDER BELLCRANKS 11 BRAKE MASTER CYLINDERS ELECTRIC FUEL PUMPS 12 LANDING GEAR ACTUATOR GASCOLATOR FUEL SELECTOR VALVE 13 LANDING GEAR RERACT TUBES 14 ELECTRIC FLAP ACTUATOR 15 STABILIZER TRIM SCREW AND STOPS 16 ELEVATOR RUDDER AILERON CONTROL SYSTEM 17 ELEVATOR RUDDER AILERON CONTROL SYSTEM BELLCRANKS 18 CONTROL SYSTEM LANDING GEAR ROD END BEARINGS 19 NOSE WHEEL STEERING...

Page 440: ...4 MS21045L3 NUT 4 NAS1149F0363P WASHER 4 TYP BOTH SIDES AN4 15A BOLT 5 MS21045L4 NUT 5 NAS1149F0463P WASHER 5 NAS1149F0432P WASHER 5 NUTS TO BE ON OUTBOARD SIDE TYP BOTH SIDES AN4 16ABOLT NAS1149F0463P WASHER NAS1149F0432P WASHER MS21045L4 NUT AN4 17A BOLT NAS1149F0463P WASHER NAS1149F0432P WASHER MS21045L4 NUT AN3 4A BOLT 8 MS21045L3 NUT 8 NAS1149F0363P 8 TYP BOTH SIDES AN4 20A BOLT 2 NAS1149F046...

Page 441: ...VICE MAINTENANCE MANUAL Date 2006 Rev Date Page 9 1 2 4 3 6 5 1 R53 5 3 EMPENNAGE ASSEMBLY ATTACH POINTS FIGURE 53 5 3 2 1 4 R53 6 TAILCONE EMPENNAGE ATTACH POINTS FIGURE 53 6 2 3 1 4 R53 8 1 ENGINE MOUNT ATTACH POINTS FIGURE 53 7 53 40 03 ...

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Page 443: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 55 STABILIZERS ...

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Page 445: ...NANCE MANUAL Date 2006 Rev Date CHAPTER 55 STABILIZERS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 55 Effectivity 1 12 06 55 Contents 3 12 06 55 00 00 5 12 06 55 10 01 6 12 06 55 30 01 7 12 06 55 40 02 8 08 10 55 EFFECTIVITY AUGUST 2010 ...

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Page 447: ... Horizontal Stabilizer Removal 6 55 10 02 Horizontal Stabilizer Installation 6 55 20 00 Elevator 6 55 20 01 Elevator Removal 6 55 20 02 Elevator Installation 6 55 30 00 Vertical Stabilizer 6 55 30 01 Vertical Stabilizer Removal 7 55 30 02 Vertical Stabilizer Installation 7 55 40 00 Rudder 7 55 40 01 Rudder Removal 7 55 40 02 Rudder Installation 7 55 40 02 Rudder Installation Assembly 8 55 CONTENTS...

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Page 449: ...ance weights per manently installed for stabilization during flight 2 3 4 5 6 7 8 9 10 11 12 R55 1 7 8 8 8 8 9 9 9 9 7 1 9 9 HORIZONTAL STABILIZER FIGURE 55 1 55 10 00 HORIZONTAL STABILIZER The main spar assembly 1 Figure 55 1 is formed from aluminum sheet into a channel Angle doublers 2 3 and 4 are formed and riveted to main spar 1 through spar web section Stub spar 5 is a channel formed from alu...

Page 450: ...skins are attached to leading edge extrusion 5 and ribs 6 with blind rivets Each formed corrugation is matched on top and bottom skins and rivets are installed for strength and rigidity through each corrugation A lead balance weight 7 is installed in each elevator tip with screws 8 Figure 55 2 See Section 27 91 00 for balancing procedures on elevators 55 20 01 ELEVATOR REMOVAL Remove AN3 bolts fro...

Page 451: ...ed left and right halves riv eted to upper skins rib assembly 4 and at leading and trailing edge A stiffener 5 is to support lower rudder ball bearing hinge fitting 6 A weather seal 7 is in cluded in the assembly The rudder control horn 8 is attached with center hinge fitting 9 to rear flange of front spar at junction of lower rib assembly 10 A brace arm on horn assembly is attached to fitting 11 ...

Page 452: ...OONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date Page 8 DETAIL B 6 DETAIL A 5 22 16 7 4 7 3 5 2 1 12 12 14 15 13 10 11 8 9 7 RUDDER ASSEMBLY FIGURE 55 4 55 40 02 AUGUST 2010 ...

Page 453: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 56 WINDOWS ...

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Page 455: ...E MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 56 WINDOWS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 56 Effectivity 1 12 06 56 Contents 3 12 06 56 00 00 5 12 06 56 22 00 6 12 06 56 23 00 7 12 06 56 50 00 8 12 06 56 EFFECTIVITY ...

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Page 457: ...T PAGE 56 00 00 General 5 56 00 01 Cleaning Acrylic 5 56 20 00 Windshield and Cabin Windows 5 56 21 00 Windshield 5 56 21 01 Windshield Removal 5 56 21 02 Windshield Installation 5 56 22 00 Cabin Windows 6 56 22 01 Cabin Windows Removal 6 56 22 02 Cabin Windows Installation 6 56 23 00 Storm Windows 7 56 50 00 Acrylic Drilling 7 56 CONTENTS ...

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Page 459: ... with fine automotive acrylic rubbing and polishing compounds Fol low instructions provided with product 56 20 00 WINDSHIELD AND CABIN WINDOWS The removal and installation of windshield and win dows are accomplished in the following paragraphs 56 21 00 WINDSHIELD 56 21 01 WINDSHIELD REMOVAL The aluminum retainer 1 at bottom of windshield 2 must be removed by drilling out rivets attaching it to cow...

Page 460: ...ble effort may be required to break bond be tween acrylic and outer skin Care should be exercised to keep window from twisting and possibly cracking Remove window and clean all remaining sealant from skin Use M E K and a scraper to remove sealant 56 22 02 CABIN WINDOWS INSTALLATION Remove all old sealant and clean skin area with M E K Place window 1 into position to assure proper fit Trim if neces...

Page 461: ...t 9 is bonded to the storm window for sealing purposes when closed Figure 56 2 56 50 00 ACRYLIC DRILLING Drill bits for acrylic should be ground per Figure 56 3 A fast turning drill bit with light pressure is desirable It is suggested that trial holes be drilled in a scrap piece of acrylic to determine best combination of drill speed and pressure to drill a clean hole CUTTING DIRECTION DUBBED OFF ...

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Page 463: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 57 WINGS ...

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Page 465: ...HAPTER 57 WINGS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 57 Effectivity 1 12 06 57 Contents 3 12 06 57 00 00 5 12 06 57 10 00 6 12 06 57 10 00 7 08 10 57 20 00 8 12 06 57 30 00 9 08 10 57 40 00 10 12 06 57 50 21 11 12 06 57 50 21 12 12 06 57 EFFECTIVITY AUGUST 2010 ...

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Page 467: ...5 57 00 02 Stall Strip Installation 5 57 10 00 Main Frame 5 57 20 00 Auxiliary Structures 8 57 20 01 Jack Points 8 57 20 02 Wing Tips 8 57 30 00 Plates Skin 9 57 40 00 Attach Fittings 10 57 40 01 Landing Gear Attach Points 10 57 50 00 Flight Surfaces 10 57 50 10 Flaps 10 57 50 11 Flap Removal and Installation 10 57 50 20 Ailerons 10 57 50 21 Aileron Removal and Installation 11 57 CONTENTS AUGUST 2...

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Page 469: ...raction tubes e Rudder control tubes f Elevator control tube g Elevator and rudder push pull tubes h Floorboards at rear attach points i Belly skin stringer splice angles j Airspeed indicator line pitot lines and pitot heater wires if installed k Hardware shown in Figure 57 1 CAUTION Have suitable cradle ready to carry fuselage be fore removing all mating hardware 2 Wing installation Installation ...

Page 470: ... BOLT 4 MS21045L3 NUT 4 NAS1149F0363P WASHER 4 TYP BOTH SIDES AN4 15A BOLT 5 MS21045L4 NUT 5 NAS1149F0463P WASHER 5 NAS1149F0432P WASHER 5 NUTS TO BE ON OUTBOARD SIDE TYP BOTH SIDES AN4 16ABOLT NAS1149F0463P WASHER NAS1149F0432P WASHER MS21045L4 NUT AN4 17A BOLT NAS1149F0463P WASHER NAS1149F0432P WASHER MS21045L4 NUT AN3 4A BOLT 8 MS21045L3 NUT 8 NAS1149F0363P 8 TYP BOTH SIDES AN4 20A BOLT 2 NAS11...

Page 471: ...0 500 WING ATTACHING HARDWARE CHART FIGURE 57 1A LEFT WING SHOWN RIGHT WING OPP STA 43 5 RIB RIVET LINE STA 60 12 FWD 2 0 A SKIN STALL STRIP A AN520 6 7 SCREW AN345 6 NUT AN960 6 WASHER FWD NOTE FILL ALL SCREW HEAD HOLES WITH FEATHERFILL SAND SMOOTH PAINT TO MATCH WING NOTE FILL ALL SCREW HEAD HOLES WITH FEATHERFILL SAND SMOOTH PAINT TO MATCH WING FWD C BORE STALL STRIP 406 06 10 DEEP AN515 6R10 S...

Page 472: ... WS 43 5 WS 59 25 WS 74 0 WS 88 75 WS 103 5 WS 118 25 WING STRUCTURE FIGURE 57 3 57 20 02 WING TIPS The M20TN wing tips are non structural fiberglass components They are riveted to upper and lower wing skins during final assembly of wing structure 1 Wing tip removal A Remove navigation strobe light assembly per instructions in Chapter 33 41 03 Figure 57 4 B Drill out rivets holding tip to upper an...

Page 473: ...e secured with screws Any access covers that are riveted in place are required for manufacturing only and NOT for routine inspections 4 1 2 3 5 8 10 9 6 13 15 14 12 11 18 20 17 16 7 7 7 7 7 7 19 19 19 3 7 7 7 7 7 7 4 5 6 2 1 11 OAT PROBE RIGHT WING ONLY 12 CONTROL TUBE GUIDE BLOCKS 13 PITOT POST LEFT WING ONLY 14 STROBE LIGHT POWER SUPPLY 15 AILERON BELLCRANK AND CONTROL RODS 16 AUTO PILOT SERVOS ...

Page 474: ...pairs are approved for the main landing gear assembly NOTE Heat treated components should NOT be re paired replace them 57 50 00 FLIGHT SURFACES Refer to Section 27 90 00 for flight control surface bal ancing procedures 57 50 10 FLAPS Refer to Section 27 50 00 for maintenance and rig ging procedures The flap actuator jack shaft is connected by a push pull rod end bearing to flap actuator bracket 1...

Page 475: ...NSTALLA TION Refer to Section 27 10 00 for removal installation balancing procedures NOTE The following rivets are to be used when replac ing existing flush rivets for the installation of trailing edge ribs per wing stations as follows WING STATION RIVET USED 20 25 MS20426AD4 4 PLCS 103 50 147 75 43 50 CR 3213 4 1 4 PLCS 74 00 88 75 118 25 133 00 59 25 MS20426AD4 7 PCS 57 50 21 ...

Page 476: ...AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date Page 12 R57 7 3 1 6 3 5 3 2 3 3 3 7 6 6 1 4 6 10 9 8 7 7 10 3 1 6 A B C DETAIL A DETAIL B DETAIL C AILERON ASSEMBLY FIGURE 57 8 57 50 21 ...

Page 477: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 61 PROPELLERS ...

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Page 479: ...PTER 61 PROPELLERS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 61 Effectivity 1 12 06 61 Contents 3 12 06 61 00 00 5 08 10 61 00 20 6 12 06 61 10 00 7 08 10 61 10 10 8 12 06 61 20 90 9 12 06 61 20 90 10 12 06 61 40 00 11 08 10 61 40 00 12 12 06 61 EFFECTIVITY AUGUST 2010 ...

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Page 481: ...T PAGE 61 00 00 General 5 61 00 10 Spinner Dome and Propeller Removal 5 61 00 20 Propeller Installation 6 61 10 00 Propeller Assembly 7 61 10 10 Minor Propeller Blade Repair 8 61 20 00 Propeller Controlling 8 61 20 10 Propeller Governor Control Rigging 8 61 20 90 Propeller Troubleshooting 9 61 40 00 Dynamic Propeller Balancing 11 61 CONTENTS ...

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Page 483: ...rvals CAUTION Refer to Hartzell Service Letter 61 for most current overhaul Time Between Overhaul limits NOTE Approved propeller shops ONLY are authorized for overhaul or major repairs to these propellers Refer to Federal Aviation Regulations Part 43 FAR 43 and Federal Aviation Agency Advisory Circular No 43 13 AC 43 13 for definition of major or minor repairs or alternations and who may accomplis...

Page 484: ...rque and index the propeller with respect to the engine crankshaft The dowel pin loca tions used on a particular propeller installation are indi cated in the propeller model stamped on the hub The engine TC mark is aligned with one dowel pin hole and will be pointing up and aligned with the engine spit line when cylinder 6 is at TDC The spinner support must be mounted before the pro peller can be ...

Page 485: ...ylinder apply a layer of tape and recheck Repeat until the spinner support fits snug ly on the cylinder NOTE When the spinner dome has been removed to facilitate maintenance check the spinner internal support to cylinder fit If the spinner loosens in service add one or more layers of UHMW tape to the cylinder until the spinner fits snugly 3 Secure the spinner to the spinner bulkhead or adapter rin...

Page 486: ...tion fitting The following lubricants are approved for use in Hart zell propellers Refer to Hartzell Propeller Owner s Manual for ambient operating temperature limitations Aeroshell 6 Recommended all purpose grease Aeroshell 5 Aeroshell 7 Aeroshell 22 Exxon 5114EP Royco 22C A A DRESSED R61 7 A A PROPELLER BLADE MINOR REPAIRS FIGURE 61 5 61 10 10 MINOR PROPELLER BLADE REPAIR 1 Minor nicks dents and...

Page 487: ...the propeller control throughout its operating range from low to high or as directed by the POH 3 Repeat this procedure at least three times to purge air from the pro peller hydraulic system and to introduce warmed oil to the cylinder NOTE Pitch change response on the first operation from low to high blade pitch may be slow but should speed up on the second and third cycles 4 Verify proper operati...

Page 488: ...with RPM Vibration problems that occur in a narrow RPM range are a symptom of res onance which is potentially harmful to the propeller Avoid op eration until the propeller can be checked by an appropriately li censed repair facility Check 1 Control surfaces cowl flaps ex haust system landing gear doors etc for excessive play which may be causing vibration unrelated to the propeller 2 Secure attach...

Page 489: ...ew or newly overhauled propellers be lu bricated after the first one or two hours of operation because centrif ugal loads will pack and redistrib ute grease which may result in a propeller imbalance Redistribu tion of grease may also result in voids in the blade bearing area where moisture can collect Check for 1 Improperly torqued or loose lu brication fitting 2 Defective lubrication fitting 3 Da...

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Page 491: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 71 POWERPLANT ...

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Page 493: ...TION SUBJECT PAGE DATE 71 Effectivity 1 12 06 71 Contents 3 12 06 71 00 00 5 12 06 71 00 20 6 12 06 71 00 40 7 12 06 71 00 50 8 08 10 71 00 50 9 08 10 71 00 50 10 08 10 71 00 51 11 08 10 71 00 51 12 08 10 71 00 52 13 08 10 71 11 00 14 08 10 71 30 00 15 08 10 71 60 02 16 08 10 71 62 00 17 08 10 71 62 00 18 08 10 71 EFFECTIVITY AUGUST 2010 ...

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Page 495: ...2 Engine Set Up Control Rigging 13 71 00 60 Fuel Injection System Maintenance 13 71 00 70 Starter System Maintenance 13 71 00 80 Engine Mixture Control Rigging 13 71 00 90 Starter Trouble Shooting 13 71 10 00 Cowling Removal 13 71 10 01 Top Cowling 13 71 10 02 Bottom Cowling 13 71 11 00 Cowling Installation 14 71 11 01 Bottom Cowling 14 71 11 02 Top Cowling 14 71 12 00 Engine Cowl Flaps Not Applic...

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Page 497: ... cockpit switches are OFF 2 Turn fuel selector valve OFF 3 Remove engine cowling see Section 71 10 00 4 Disconnect battery ground cables 5 Remove propeller refer to section 61 00 10 6 Drain engine oil sump 7 Disconnect the following A Cabin heat ducts at engine B Fuel vent lines from engine mount and air frame C Oil temperature bulb connections D Oil pressure line connections E Manifold pressure l...

Page 498: ...slide the crossover pipe assembly rearward off of the slip joints to prevent binding at the slip joints 21 Slide crossover pipe off of wastegate A slip joint is located between the crossover pipe heat shield as sembly and the wastegate connection Lay wastegate over top of engine and temporarily secure the waste gate to the engine to protect it from damage during en gine removal Set crossover pipe ...

Page 499: ...roper thread grip length 4 Oil drain plugs are tightened and safetied 5 Oil sump is filled to eight quarts 6 Spark plugs are tight and ignition harness is prop erly installed 7 Magneto ground wires are properly installed and safetied 8 Oil temperature bulb connections are tight and safetied 9 Oil pressure relief valve plug is safetied 10 Cylinder head temperature connections are se cure 11 Starter...

Page 500: ...M C Throttle Control Set to Closed D Boost Pump HIGH for 5 seconds or LOW for 25 seconds then set to OFF E Engine Start follow Normal procedures 7 Extreme Cold Weather Starts Refer to TCM Engine Operating Manual OI 18 Section 7 5 1 for extreme cold weather starting proce dures 71 00 50 ENGINE SET UP PROCEDURE It is recommended that the TSIO 550 G engine installed on the Mooney M20TN aircraft be se...

Page 501: ...stem components under test for the duration of the operational check Indi cated fuel pressure at the gauge will increase if the gauges are below the fuel injection system causing erroneous indications J Loosen the test connections at each gauge to bleed the lines of air Hold the gauge at or slightly above the height of fuel system components to allow the fuel to force the air out of the lines Oper...

Page 502: ...d rpm setting Best Power mixture is desirable for minimizing flight time when fuel burn rate or range is not a primary concern When TIT limitations prevent attaining peak TIT then best power is obtained at 1650 F TIT B Recheck idle pressure setting as specified in 2 above and adjust as required C Recheck 100 percent power fuel flow as speci fied in 5 A and adjust as required CAUTION Do not exceed ...

Page 503: ... Page 11 H FORWARD LOW UNMETERED FUEL PRESSURE SLOPE CONTROL ADJUSTMENT HIGH FUEL PRESSURE IDLE SPEED ADJUSTMENT ADJUSTMENT ADJUSTMENT IDLE MIXTURE ADJUSTMENT ENRICHEN MIXTURE INCREASE INCREASE INCREASE INCREASE ENGINE SET UP AND ADJUSTMENT POINTS FIGURE 71 3 71 00 51 AUGUST 2010 ...

Page 504: ...e 2006 Rev Date Page 12 UMTD UNMETERED FUEL PRESSURE TBD UPPER DECK PRESSURE MAN MAP MTD METERED FUEL PRESSURE UMTD UNMETERED FUEL PRESSURE TBD UPPER DECK PRESSURE MAN MAP MTD METERED FUEL PRESSURE ENGINE SET UP AND ADJUSTMENT POINTS FIGURE 71 3 AUGUST 2010 71 00 51 ...

Page 505: ...g on throttle body and manifold valve and conduct a leak check of all connec tions Ensure all hoses are correctly reconnected Re move footwell fitting adapter and replace with footwell cover adapter 71 00 60 FUEL INJECTION SYSTEM MAINTE NANCE For specific injection system inspection and overhaul instructions consult TCM Maintenance and Overhaul Manual M 18 Service Instructions and TCM Service Info...

Page 506: ...ds and lower isolators at all four locations Keep heat shield and mounting hardware lift engine to allow removal of all four upper engine isolator mounts and hardware Inspect Heli Coils in engine legs for any damage i e cross threading Replace legs as re quired 2 ENGINE MOUNT INSTALLATION A Use dummy bolts NAS6607 15 or equival ent and washers to secure each of the upper halves of isolator mounts ...

Page 507: ...RVICE MAINTENANCE MANUAL Date 2006 Rev Date Page 15 AIRCRAFT RIGHT HAND SIDE AIRCRAFT LEFT HAND SIDE VIEW LOOKING DOWN ENG FWD M20TN S N 31 0001 THRU 31 0023 AND 31 0025 THRU 31 0137 ENGINE MOUNT SEQUENCE FIGURE 71 5 71 20 01 AUGUST 2010 ...

Page 508: ...fireseal with Coast Pro Seal 700 or equivalent on engine side of firewall 71 60 00 AIR INTAKES The engine cooling air intakes and exits are calculated for optimum cooling requirements and minimum drag Normal engine operating temperatures are at optimum to facilitate engine efficiency The engine induction air intake is a fiberglass duct that picks up impact air and routes it through rechargeable ai...

Page 509: ... Kit P N CP 99 5050 containing oil red in color Begin re oiling the dry filter by applying a bead or line of red oil along the top only of each pleat of the filter The oil will soak into the length of each pleat It may be necessary to ap ply oil on filter material that has not received oil from the wicking action The entire filter medium must be cov ered with red oil DO NOT OVER OIL If oil drips f...

Page 510: ... BETWEEN ACTUATOR ROD DOOR ASSY WITH CONTROL KNOB IN CLOSED POSITION 13 IN ANNNCIATOR LIGHT SWITCH MEASURE 4 5 TO 7 5 LBS TO OPEN DOOR HERE REF ANNNCIATOR LIGHT SWITCH REF APPROX RECHARGEABLE FILTER ELEMENT 4 MOUNTING SCREWS AND WASHERS DUCT ASSY HOSE CLAMP TRANSFER TUBE AIR INTAKE AIR INTAKE ASSEMBLY AND ALTERNATE AIR DOOR RIGGING FIGURE 71 7 AUGUST 2010 71 62 00 ...

Page 511: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 72 ENGINE ...

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Page 513: ... INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 72 ENGINE LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 72 Effectivity 1 12 06 72 Contents 3 12 06 72 00 00 5 12 06 72 00 00 6 12 06 72 EFFECTIVITY ...

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Page 515: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 72 ENGINE TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 72 00 00 General 5 72 CONTENT ...

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Page 517: ... 2006 Rev Date Page 5 72 00 00 GENERAL Refer to Teledyne Continental Motors TCM TSIO 550 G engine Maintenance and Overhaul Manual M 18 and Installation and Operation Manual OI 18 for detailed information on the TSIO 550 G engine installed in the Mooney M20TN 72 00 00 ...

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Page 519: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 73 ENGINE FUEL SYSTEMS ...

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Page 521: ...E MANUAL Date 2006 Rev Date CHAPTER 73 ENGINE FUEL SYSTEMS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 73 Effectivity 1 12 06 73 Contents 3 12 06 73 00 00 5 12 06 73 40 00 6 12 06 73 60 00 7 08 10 73 60 01 8 12 06 73 EFFECTIVITY AUGUST 2010 ...

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Page 523: ... SECTION SUBJECT PAGE 73 00 00 General 5 73 10 00 Distribution 6 73 20 00 Controlling 6 73 30 00 Fuel Flow Indicating 6 73 31 00 Panel Mounted Instruments 6 73 31 01 Garmin G1000 6 73 31 02 Fuel Flow Transducer 6 73 40 00 Fuel Injector General 7 73 60 00 Fuel Pump Information 7 73 60 01 Auxiliary Fuel Pump LOW BOOST Set Up 7 73 CONTENTS ...

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Page 525: ... FUEL PUMP DECK PRESSURE FROM UPSTREAM OF ENGINE THROTTLE IDLE PRESSURE RELIEF VALVE CW TO INCREASE IDLE CUT OFF MIXTURE CONTROL FULL RICH FULL POWER FUEL PRESSURE ADJUSTMENT COUNTER CLOCKWISE TO INCREASE TURBINE WHEEL FOR ELECTRICAL FUEL FLOW SENSING NOT PART OF ENGINE IDLE MIXTURE SCREW CW TO LEAN FUEL PRESSURE GAUGE ENGINE SET UP ONLY NOT PART OF ENGINE THROTTLE BODY FUEL METERING VALVE POWER S...

Page 526: ...alve to OFF C Remove top cowling from aircraft See Section 71 10 00 for procedures D Remove 2 breeze clamps securing firesleeve on both sides of fuel flow transducer E Slide firesleeve off fuel lines fuel flow transduc er F Cut and remove ty raps securing electrical wires G Slide insulation sleeving up on electrical wire harness H Disconnect transducer electrical harness from aircraft harness I Lo...

Page 527: ...of Section 71 00 50 be followed to as sure engine is set up for proper operation I When all adjustments have been made and all connections checked for security install cowling per Section 71 10 00 73 40 00 FUEL INJECTOR GENERAL The fuel injection system is supplied with engine from TCM It is of a multi nozzle continuous flow type Changes in air throttle position engine speed turbo charger boost or...

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Page 529: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 74 IGNITION ...

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Page 531: ...20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 74 IGNITON LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 74 Effectivity 1 12 06 74 Contents 3 12 06 74 00 00 5 08 10 74 20 00 6 12 06 74 EFFECTIVITY AUGUST 2010 ...

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Page 533: ...ANCE MANUAL Date 2006 Rev Date CHAPTER 74 IGNITION TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 74 00 00 General 5 74 10 00 Electrical Power 5 74 10 01 Ignition System Troubleshooting 5 74 20 00 Engine Firing Order 6 74 30 00 Switching 6 74 CONTENTS ...

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Page 535: ...erly timed to en gine Check magneto timing to engine Refer to TCM Maintenance and Overhaul manual M 18 Shorted Condenser Replace Condenser Magneto internal timing incorrect or timed for opposite rotation Install correctly timed magneto Reference TCM Maintenance and Overhaul manual M 18 for timing procedures Engine roughness Idle Loose fouled or improperly gapped spark plugs Tighten Spark Plugs Cle...

Page 536: ...magneto rotor turns counter clockwise passing in succession terminals of spark plug cables in engine firing order Cables are connected to magne tos so right magneto fires upper plugs on right side and lower plugs on left side The left magneto fires upper plugs on left side and lower plugs on right side The magneto cases spark plugs cables and connections are shielded to prevent radio interference ...

Page 537: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 76 ENGINE CONTROLS ...

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Page 539: ... SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 76 ENGINE CONTROLS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 76 Effectivity 1 12 06 76 Contents 3 12 06 76 00 00 5 12 06 76 20 01 6 08 10 76 EFFECTIVITY AUGUST 2010 ...

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Page 541: ...E MANUAL Date 2006 Rev Date CHAPTER 76 ENGINE CONTROLS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 76 00 00 General 5 76 10 00 Engine Controls Rigging 5 76 20 00 Engine Controls Maintenance 5 76 20 01 Engine Controls Removal Installation 5 76 CONTENTS ...

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Page 543: ...bly to engine or propellor control component 3 Loosen hardware from attaching clamps Remove clamps Loosen hardware attaching cable assembly to throttle switch bracket 4 Loosen jamb nut connecting cable assembly to firewall 5 From inside cockpit behind control panel locate and loosen housing nut securing Throttle Propeller or Mixture Control to instrument structure assembly 6 Remove control cable a...

Page 544: ...ITTING LOCKWASHER NUT ENGINE THROTTLE BODY PROPELLER GOVERNOR ENGINE FUEL CONTROL CONTROL CONTROL CONTROL TYP TYP TYP CLAMP CLAMP HEIM ROD END BEARING HEIM ROD END BEARING HEIM ROD END BEARING CLAMP TN76 1 THROTTLE SWITCH BRACKET ALTERNATE AIR CONTROL REF ALTERNATE AIR DUCT REF ENGINE CONTROL CABLE INSTALLATION FIGURE 76 1 76 20 01 AUGUST 2010 ...

Page 545: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 77 ENGINE INDICATING ...

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Page 547: ...SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 77 ENGINE INDICATING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 77 Effectivity 1 12 06 77 Contents 3 12 06 77 00 00 5 08 10 77 30 01 6 08 10 77 EFFECTIVITY AUGUST 2010 ...

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Page 549: ...al 5 77 00 01 Ranges 5 77 10 00 Power Indicating 5 77 10 01 Tachometer 5 77 10 02 Manifold Pressure 5 77 10 03 Fuel Flow Indicating System 5 77 20 00 Temperature Indicating 5 77 20 01 Exhaust Gas Temperature 5 77 20 02 Cylinder Head Temperature 5 77 20 03 Oil Temperature 5 77 20 04 TIT Instrument Probe 5 77 30 00 Pressure Indicating 5 77 30 01 Oil Pressure 5 77 CONTENTS ...

Page 550: ...MOONEY AIRPLANE COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date INTENTIONALLY LEFT BLANK ...

Page 551: ...ture of hottest cylinder is displayed in degrees Fahr enheit 0 F to 1700 F on Garmin Engine Indication System EIS EGT display Display provides numerical temperature reading and associated cylinder indicated by triangular pointer For Operation Maintenance and Troubleshooting re fer to Garmin publications 77 20 02 CYLINDER HEAD TEMPERATURE The cylinder head temperature CHT instrument pro vides opera...

Page 552: ...eter Cylinder Head Temperature Turbine Inlet Temperature Oil Temperature Oil Pressure Fuel Flow Indicator Fuel Quantity Indicator RPM Gauge Manifold Pressure Gauge 10 9 8 7 6 5 4 3 2 1 GARMIN G1000 DISPLAY PRESS ENGINE SOFT KEY FOR EIS DISPLAY LH SIDE OF G1000 DISPLAY ENGINE INDICATION DISPLAY G1000 SCREEN FIGURE 77 1 77 30 01 AUGUST 2010 ...

Page 553: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 78 EXHAUST ...

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Page 555: ...20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 78 EXHAUST LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 78 Effectivity 1 12 06 78 Contents 3 12 06 78 00 00 5 08 10 78 40 00 6 12 06 78 EFFECTIVITY AUGUST 2010 ...

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Page 557: ...TENANCE MANUAL Date 2006 Rev Date CHAPTER 78 EXHAUST TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 78 00 00 General 5 78 10 00 Exhaust System Installation 5 78 30 00 Exhaust System Servicing 5 78 40 00 Periodic Replacement Components 6 78 CONTENTS ...

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Page 559: ...intenance and troubleshooting 78 30 00 EXHAUST SYSTEM SERVICING 1 CLEANING To properly inspect exhaust system components must be clean and free of oil grease etc Clean as follows A Spray engine exhaust system components with a suitable solvent Stoddard Solvent allow to drain and wipe dry with clean cloth WARNING When using Stoddard Solvent follow directions and warnings given by the manufacturer W...

Page 560: ... borescope is recommended G INSTALLATION TIPS Install only correct parts DO NOT FORCE FIT any component Properly align connecting components Do not reuse gaskets Insure that attach bolts are properly torqued Exhaust flange stud nuts are to be torqued to 100 110 inch lbs 78 40 00 PERIODIC REPLACEMENT COM PONENTS It is recommended that all exhaust system pipes clamps and miscellaneous mounting hardw...

Page 561: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 79 OIL ...

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Page 563: ...INTENANCE MANUAL Date 2006 Rev Date CHAPTER 79 OIL LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 79 Effectivity 1 12 06 79 Contents 3 12 06 79 00 00 5 08 10 79 30 00 6 08 10 79 50 00 7 12 06 79 50 00 8 12 06 79 EFFECTIVITY AUGUST 2010 ...

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Page 565: ...E OF CONTENTS CHAPTER SECTION SUBJECT PAGE 79 00 00 General 5 79 00 01 Oil Filter Removal 5 79 00 02 Oil Filter Installation 5 79 20 00 Distribution 5 79 30 00 Indicating 6 79 30 01 Oil Pressure 6 79 30 02 Oil Temperature 6 79 40 00 Transducer Test 6 79 50 00 Oil System Troubleshooting 7 79 CONTENTS ...

Page 566: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date INTENTIONALLY LEFT BLANK ...

Page 567: ... VALVE OIL THRU OIL TEMPERATURE CONTROL VALVE OIL UNDER PRESSURE OIL FROM GOVERNOR OIL PRESSURE TEMPERATURE CONNECTION OIL TEMPERATURE CONTROL VALVE OIL PRESSURE RELIEF VALVE STARTER IDLER ACCESSORY DRIVES CRANKSHAFT CAMSHAFT TAPPETS OIL COOLER FULL FLOW OIL FILTER WITH BY PASS VALVE SUMP OIL PICK UP CAMSHAFT OIL TRANSFER COLLAR GOV PAD TO PROPELLER R79 1 LUBRICATION DIAGRAM FIGURE 79 1 79 00 01 O...

Page 568: ...URE TRANSDUCER VIEW LOOKING FROM LEFT SIDE R79 2 MANIFOLD PRESSURE TRANSDUCER REF KULITE TRANSDUCER KAVLICO TRANSDUCER KULITE TRANSDUCERS SHOWN OIL PRESSURE TRANSDUCER FIGURE 79 2 79 30 02 OIL TEMPERATURE The oil temperature gauge is an electric unit receiving its signal from a temperature bulb located below oil cooler The probe resistance changes as oil tempera ture changes and this varies readou...

Page 569: ...Thermostat damaged or held open by solid matter Remove clean valve and seat If still inoperative replace Oil viscosity too high Drain and refill with correct sea sonal weight oil See Chapter 5 Prolonged ground operation Limit ground operation to a mini mum Malfunctioning gauge or bulb unit Check wiring Check bulb unit Check gauge Replace malfunc tioning parts Low oil pressure Indication Low oil su...

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Page 571: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 80 STARTING ...

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Page 573: ...0TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 80 STARTING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 80 Effectivity 1 12 06 80 Contents 3 12 06 80 00 00 5 08 10 80 10 00 6 12 06 80 EFFECTIVITY AUGUST 2010 ...

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Page 575: ...MANUAL Date 2006 Rev Date CHAPTER 80 STARTING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 80 00 00 General 5 80 00 01 Troubleshooting 5 80 00 02 Maintenance 5 80 00 03 Removal 5 80 00 04 Installation 5 80 00 05 Brushes 5 80 10 00 Cranking 5 80 CONTENTS ...

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Page 577: ... straps connections for tightness 3 Install new O ring on starter flange 4 Position starter on mounting pad 5 Install attaching nuts and washers 6 Torque nuts 220 0 to 260 0 inch lbs 7 Connect electrical wiring to starter terminals 8 Check starter mounting flange for oil leakage be fore cowling is installed 9 Install cowling 80 00 05 BRUSHES Starter brushes should slide freely in holder and make f...

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Page 579: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 81 TURBOCHARGER ...

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Page 581: ...ANCE MANUAL Date 2006 Rev Date CHAPTER 81 TURBOCHARGER LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 81 Effectivity 1 12 06 81 Contents 3 12 06 81 00 00 5 12 06 81 20 00 6 12 06 81 30 00 7 08 10 81 40 00 8 12 06 81 EFFECTIVITY AUGUST 2010 ...

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Page 583: ...SECTION SUBJECT PAGE 81 00 00 General 5 81 10 00 Turbocharger Control 5 81 10 01 Turbocharger Control System 5 81 10 02 Alternate Air System Turbocharger Operation 5 81 20 00 Turbocharger Troubleshooting 6 81 30 00 Exhaust System Servicing 7 81 30 01 Inspection V Band Clamp 7 81 40 00 Periodic Replacement Components 7 81 CONTENTS ...

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Page 585: ... 10 01 TURBOCHARGER CONTROL SYS TEM The turbocharger output is controlled through coordi nated action of the Density Differential Pressure Con troller system when set up properly CAUTION It is mandatory that the turbocharger system be properly adjusted prior to operation See Chapter 71 00 52 for engine set up procedures TURBOCHARGER OVERBOOST PROTECTION The engine incorporates overboost protection...

Page 586: ...as leakage gaskets at cylinder ex haust ports gaskets at turbine inlet flanges et and correct White smoke exhaust Turbo coking oil forced through turbine housing seal Clean and change turbocharger Low manifold pressure Improperly adjusted controller Adjust according to TCM Mainte nance and Overhaul Manual M 18 section regarding Post Mainte nance Adjustment and Test or re place if adjustment cannot...

Page 587: ...Lok pin areas for cracks See Figure 81 2 If cracks or loose pins are found replace clamp with new multi segment V band clamp NOTE When replacement is required install new V band clamp over the exhaust flanges and torque as shown below TORQUE PROCEDURES Torque V Band coupling to 40 Lb In Tap coupling lightly around circumference with a non metallic ham mer to equalize band tension Re torque couplin...

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Page 589: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 91 ELECTRICAL WIRING DIAGRAMS SCHEMATICS AND HARNESSES ...

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Page 591: ...ECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 91 Effectivity 1 12 06 91 Contents 3 12 06 91 00 00 5 12 06 91 00 02 6 12 06 91 00 03 7 12 06 91 20 00 8 12 06 91 20 01 9 12 06 91 20 01 10 12 06 91 20 01 11 12 06 91 20 01 12 12 06 91 20 01 13 12 06 91 20 01 14 12 06 91 20 01 15 12 06 91 20 01 16 12 06 91 30 00 17 08 10 91 EFFECTIVITY AUGUST 2010 ...

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Page 593: ...SECTION SUBJECT PAGE 91 00 00 General 5 91 00 01 Electrical Systems Notes 5 91 00 02 Wiring Identification System 5 91 00 03 Abbreviations Equipment List 7 91 20 00 Serial Number vs Schematic s Listing 7 91 20 01 Electrical Equipment Hardware Chart 9 91 30 00 Electrical System Schematic Envelopes 17 91 30 01 Electrical System Harness Drawings CD ROM 23 91 CONTENTS AUGUST 2010 ...

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Page 595: ...ockwise with a minimum of three 3 wraps per foot 10 F denotes ground through frame no wires 11 All knife disconnect splices to be insulated with PVC105 and securely string tied with Airtex no 417 cord 12 All wire sizes are minimum sizes acceptable 13 Use 913127 buss bars as necessary for various configuration changes and manufacture interconnect ing buss using no 2170 tubular braid covered with PV...

Page 596: ...TRUMENTS FUEL FLOW DW INSTRUMENTS ENGINE VACUUM EG GEAR ELECTRIC EL ELECTROLUMINESCENCE ET EMERGENCY LOCATOR BEACON FA ALT EMER FRENCH FH FUSE HOLDERS FN PHONES FU FUSES FW ALT EMER FIELD FRENCH GD GROUND HS HORIZONTAL SITUATION INDICATOR JE IGNITION ELECTRONIC JM IGNITION MAGNETO JV IGNITION VIBRATOR LA LIGHT BULBS LB BEACON ROTATING LC LIGHT CABIN LE LENS ANNUNCIATOR LG LIGHTS LOGO LH LAMP HOLDE...

Page 597: ...00 03 ABBREVIATIONS EQUIPMENT LIST The abbreviations to the electrical system hardware charts are necessary due to space limitations in the fields of the computer Airspeed A S Glareshield Glrshld Remote Rem Alternator Altnr Landing Ldg Resistor Res Circuit Breaker Ckt Bkr or C B Left L or L H Rheostat Rheo Console Cnsl Lights Lts Right R or R H Control Cntrl Panel Pnl Safety Sfty Coordinator Coord...

Page 598: ...31 0001 THRU 31 TBA 800422 E ELECTRICAL HARNESS TAILCONE 31 0032 THRU 31 0101 800422 F ELECTRICAL HARNESS TAILCONE 31 0102 THRU 31 TBA 800423 D ELECTRICAL HARNESS FLOORBOARD 31 0001 THRU 31 TBA 800424 B ELECTRICAL HARNESS WINGS 31 0001 THRU 31 TBA 800425 B ELECTRICAL HARNESS OVERHEAD 31 0001 THRU 31 TBA 800426 G ELECTRICAL HARNESS FLIGHT PANEL 31 0001 THRU 31 TBA 800427 C ELECTRICAL HARNESS CONSOL...

Page 599: ... AIR105A SWITCH A C PRESS MOONEY 770029 501 BL5 BULB CONSOLE GE 327 ALT GE 385 BL6 BULB COMPASS GE 327 AV RED BL7 BULB POST LIGHT GE 330 BR1 CIRCUIT BREAKER 1A KLIXON 7277 2 1 7 BR2 CIRCUIT BREAKER 2A KLIXON 7277 2 2 7 BR3 CIRCUIT BREAKER 3A KLIXON 7277 2 3 7 BR5 CIRCUIT BREAKER 5A KLIXON 7277 2 5 7 BR7 5 CIRCUIT BREAKER 7 5A KLIXON 7277 2 7 5 7 BR10 CIRCUIT BREAKER 10A KLIXON 7277 2 10 7 BR15 CIR...

Page 600: ...P 5 PIN MS3057 6A B CL05B CLAMP 5 PIN DEUTSCH BVDSREC02SR CL06A CLAMP 6 PIN MS3057 16A B ALT MS3417 28C CL07A CLAMP 7 PIN MS3057 12B SLEEVE MS3420 CL07B DEUTSCH CPPSR02A CL09A CLAMP 9 PIN LT CONT BOX AMP 206966 1 CL09B CLAMP 9 PIN AMP P O 126 222 CL09C CLAMP 9 PIN DE 24657 LOCK RETAINER DE 51224 1 LOCK RETAINER ALT D110278 LOCK RETAINER ALT D 20419 16 CL09D CLAMP 9 PIN DE19977 5 LOCK RETAINER DE51...

Page 601: ...5854 ALT NTE 5854 D4 DIODE BRIDGE FAGOR FB5001 D5 DIODE BRIDGE FAGOR FB5006 DF101A FUEL XMTR LH RH I B MOONEY 610242 003 DF102A FUEL XMTR LH O B MOONEY 610243 003 DF104A FUEL XMTR LH RH O B MOONEY 610242 005 DH101A PROBE OIL TEMP MOONEY 880061 501 DI101A DIODE 1N2483 1N5060 ALT GE 3720 GE DI102A DIODE SARKES TARZ 10H3P ALT ECG 5854 ALT NTE 5854 DI104A DIODE BRIDGE FAGOR FB5001 DI105A DIODE BRIDGE ...

Page 602: ...K CD 1001 02 JE102A CABLE LASAR SLICK CH1001 XX JM101B SWITCH MAG W CONN JANCO 97 2273 1 JM107A SWITCH IGNITION TCM 10 357240 1 MAGNETO L R TCM BENDIX 10 79020 10 L1 LIGHT ICE WHELEN 01 0790093 000 ALT WHELEN Q5596 L9 LA109A BULB GE 327 AV RED L10 BULB 28V GE 327 LA110A BULB POST LIGHT GE 327 LA113A BULB GE 4596 LA114A BULB PAC PREC P28028 LB102B LIGHT ANTI COLLISION RED WHELEN 90033 19 LB102C LIG...

Page 603: ...B SW BOOST PUMP MOONEY 930023 311 NF109A C B SW HI BOOST PUMP MOONEY 930023 219 PA103A SWITCH ALT FLD SINGLE MOONEY 880052 503 ALTERNATOR ELECTRO SYS ES 10024 PA115A VOLTAGE REGULATOR MOONEY 800397 501 PB102A SWITCH MASTER MOONEY 880052 501 PB102B SWITCH MASTER MOONEY 880052 101 PB103A SWITCH BATTERY 1 2 MOONEY 880052 527 PB103B SWITCH BATTERY 1 2 MOONEY 880052 127 PB105B BATTERY MAINT FREE CONCOR...

Page 604: ...2 10 PS102A C B STARTER SOLENOID KLIXON 7277 2 5 PS104A STARTER TCM 646275 ALT TCM 637847 R3 RS103A RESISTOR MAPLIGHT 500 OHM MOONEY 919029 501 R5RS105A RESISTOR 7 5 OHM DALE RH 50 7 5 OHM ALT SPECTROL 149 11 502 2 R9 RS109A RESISTOR 3 9K OHM 1 2W OHMITE N A R10 RS110A RESISTOR 3 0K OHM 1 2W OHMITE N A R12 RS112A RESISTOR 70 OHM 10W DALE RH 10 70 OHM R13 RESISTOR 10 0K OHM 1W OHMITE N A RB103A AUT...

Page 605: ...W OHMITE N A RS112A RESISTOR 70 OHM 10W DALE RH 10 70 OHM RS113A RESISTOR 15 0K OHM 1 4W OHMITE N A RS115A RESISTOR 1 6K OHM 1 2W OHMITE N A RS116A RESISTOR 1 0K OHM 1 8W OHMITE N A RS117A RESISTOR 82 OHM 1 2W OHMITE N A RS118A RESISTOR 20 0K OHM 1 4W ALLEN BRADLEY RC07CB203J SA101A ALTERNATOR STAND BY B C BC410 1 HOUSING CONNECTOR B C 12 003 TERMINAL 1 4 B C 14 026 SA103A SWITCH STD BY ALT EMER B...

Page 606: ...B OMRON A3B 028 VC102A TRANSELECTRIC SM2412 5 VR1 VR101A VARISTOR GE V47ZA05 WS103A SWITCH STALL WARNING MOONEY 800364 509 WT101B ANNUNCIATOR MOONEY 880090 XXX 3 NOTES 1 PL02C RC02C MAY BE PURCHASED FROM DEAN AS P N 7020 2 SEAL BACK OF SWITCH WITH DOW CORNING 738 ELECTRICAL SEALANT AFTER WIRES ARE SOLDERED TO TERMINALS MOONEY CODE 225905 WHEN USED AS THROTTLE SWITCH GEAR WARNING 3 ANNUNCIATOR P N ...

Page 607: ...GFC700 800419 F 31 0001 THRU 31 TBA CIRCUIT BREAKER PANEL INSTAL 800420 G 31 0001 THRU 31 TBA ELECTRICAL HARNESS CABIN 800421 F 31 0001 THRU 31 TBA ELECTRICAL HARNESS TAILCONE 800422 E 31 0032 THRU 31 0101 ELECTRICAL HARNESS TAILCONE 800422 F 31 0102 THRU 31 TBA ELECTRICAL HARNESS FLOORBOARD 800423 D 31 0001 THRU 31 TBA ELECTRICAL HARNESS WINGS 800424 B 31 0001 THRU 31 TBA ELECTRICAL HARNESS OVERH...

Page 608: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date Page 18 INTENTIONALLY LEFT BLANK 91 30 00 ...

Page 609: ...N EFFECTIVITY RELATED S M MANUAL PAGES 800416 TN1 1st PROD 31 0001 thru 31 0031 91 20 01 pages 7 thru 20 CAUTION Be certain that the Serial Number of the aircraft being serviced agrees with the Serial Number effectivity of the schematic being used NOTE All Optional Equipment Schematics are to be depicted on the System Installation Drawings and will not be on these Basic Aircraft Schematics AUGUST ...

Page 610: ...MOONEY AVIATION COMPANY INC M20R SERVICE MAINTENANCE MANUAL Page Date 2 2006 Rev Date INTENTIONALLY LEFT BLANK ...

Page 611: ......

Page 612: ...CABIN 800421 F 31 0001 THRU 31 TBA ELECTRICAL HARNESS TAILCONE 800422 E 31 0032 THRU 31 0101 ELECTRICAL HARNESS TAILCONE 800422 F 31 0102 THRU 31 TBA ELECTRICAL HARNESS FLOORBOARD 800423 D 31 0001 THRU 31 TBA ELECTRICAL HARNESS WINGS 800424 B 31 0001 THRU 31 TBA ELECTRICAL HARNESS OVERHEAD 800425 B 31 0001 THRU 31 TBA ELECTRICAL HARNESS FLIGHT PANEL 800426 G 31 0001 THRU 31 TBA ELECTRICAL HARNESS ...

Page 613: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Page Date 2 Rev Date INTENTIONALLY LEFT BLANK AUGUST 2010 ...

Page 614: ...8 SH 5 1 1 22 Mil Spec 2 Cond 18 AWG Shielded A R 919026 107 18 5 1 7 23 Mil Spec 2 Cond 20 AWG Shielded A R 919026 107 20 5 1 6 24 Mil Spec 3 Cond 20 AWG Shielded A R 919026 059 20 5 1 2 25 Mil Spec 4 Cond 24 AWG A R 919026 065 5 1 22 26 TYCO Plug 2 pin 5 1 480318 0 5 1 4 27 TYCO Plug 3 pin 5 1 480303 0 5 1 14 28 TYCO Plug 3 pin 3 206037 2 5 1 8 29 MOLEX Plug 3 pin 1 22 01 3037 5 1 27 30 Mil Spec...

Page 615: ...5 97 Molex Socket 22 AWG 2 08 50 0114 5 1 8 98 TYCO Socket 08 AWG 4 66741 6 5 1 8 99 TYCO Socket 14 AWG 4 66740 6 5 1 8 100 Positronics Socket 14 AWG 18 FC114N2 5 1 8 102 TYCO Clamp 4 Pin 8 Pin HD 6 206062 5 1 4 105 TYCO Clamp 9 Pin 5 206966 1 5 1 10 107 TYCO Clamp 14 Pin 16 Pin 28 Pin HD A R 206070 1 5 1 6 109 Matrix Clamp RC32A 2 M85049 52 1 22N 5 1 1 110 Mil Spec Bushing Rubber 2 MS3420 14 5 1 ...

Page 616: ... Nut 8 MS21044N04 6 1 1 150 Mil Spec Washer 16 NAS1149FN416P 6 1 1 151 Mil Spec Screw 10 MS35206 216 6 1 1 153 Mil Spec Nut 4 MS21044N08 6 1 1 154 Mil Spec Washer 8 NAS1149FN816P 6 1 1 155 Mil Spec Screw 4 MS35206 245 6 1 1 157 Brim Tinned Copper Braid A R 1115 3 32 8 1 1 158 Type 1 CS1900 Sealant A R MIL S 38249 6 1 1 160 MAC Wire 3 Cond Shielded A R 919026 059 22 161 MAC 2 Cond 22 AWG Shielded A...

Page 617: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 04 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E TABLE OF CONTENTS ...

Page 618: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 05 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E NOTES ...

Page 619: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 06 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 1 ...

Page 620: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 07 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 2 ...

Page 621: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 08 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 3 ...

Page 622: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 09 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 4 ...

Page 623: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 010 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 5 ...

Page 624: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 011 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 6 ...

Page 625: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 012 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 7 ...

Page 626: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 013 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 8 ...

Page 627: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 014 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 9 ...

Page 628: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 015 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 10 ...

Page 629: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 016 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 11 ...

Page 630: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 017 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 12 ...

Page 631: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 018 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 13 ...

Page 632: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 019 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 14 ...

Page 633: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 020 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 15 ...

Page 634: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 021 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 16 ...

Page 635: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 022 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 17 ...

Page 636: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 023 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 18 ...

Page 637: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 024 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 19 ...

Page 638: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 025 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 20 ...

Page 639: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 026 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 21 ...

Page 640: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 027 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 22 ...

Page 641: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 028 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 23 ...

Page 642: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 029 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 24 ...

Page 643: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 030 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 25 ...

Page 644: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 031 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 26 ...

Page 645: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 032 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 27 ...

Page 646: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 033 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 28 ...

Page 647: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 034 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 29 ...

Page 648: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 035 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 30 ...

Page 649: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 036 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 31 ...

Page 650: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 037 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 32 ...

Page 651: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 038 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 33 ...

Page 652: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 039 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 34 ...

Page 653: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 040 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 35 ...

Page 654: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 041 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 36 ...

Page 655: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 042 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 37 ...

Page 656: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 043 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 38 ...

Page 657: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 044 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 5 1 39 ...

Page 658: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417E 045 AUGUST 2010 ELECTRICAL HARNESS 800417 501 E FIGURE 6 1 1 ...

Page 659: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date PageEH417E 046 AUGUST 2010 INTENTIONALLY LEFT BLANK ...

Page 660: ...5 5 2 32 42 MAC Plug 50 pin 1 930021 511 5 2 22 43 TYCO Plug 9 pin 1 205161 1 5 2 5 4 44 Mil Spec Plug 4 pin A R MS3116E8 4S 5 2 9 45 Mil Spec Modular Plug 1 RJ 11 6P4C 5 2 22 51 TYCO Receptacle 3 pin 2 1 480305 0 5 2 4 53 TYCO Receptacle 4 pin 1 1 480305 0 5 2 9 54 Clamp Backshell A R MS3417 28C 5 2 4 55 Mil Spec Receptacle 6 Pin 1 MS3100K 28 22P 5 2 4 56 TYCO Receptacle 8 Pin 1 205841 2 5 2 14 5...

Page 661: ...Solder Sleeve A R AS83519 1 X 5 2 1 127 Mil Spec Resistor 20K OHM 1 4w 1 RC07GF203J 5 2 3 128 Mil Spec Heat Shrink Tubing A R M23053 5 X Y 5 2 7 129 Alpha Wire Braid Shield A R 2170 5 2 8 130 TYCO Fusion Tape A R 605980 1 5 2 4 Alt for item 128 131 Mil Spec Terminal 10 22 18 AWG A R MS25036 103 5 2 37 Alt for Tyco 31891 132 Mil Spec Diode A R 1N2483 5 2 4 134 Mil Spec Terminal 8 8 AWG 1 MS20659 14...

Page 662: ... Spec 1 Cond 20 AWG WHT A R 919026 044 20 5 2 1 182 Mil Spec 1 Cond 18 AWG WHT A R 919026 044 18 5 2 2 183 Mil Spec 1 Cond 16 AWG WHT A R 919026 044 16 5 2 22 184 Mil Spec 1 Cond 14 AWG WHT A R 919026 044 14 5 2 7 185 Mil Spec 1 Cond 10 AWG WHT A R 919026 044 10 5 2 8 186 Mil Spec 1 Cond 08 AWG WHT A R 919026 044 08 5 2 8 187 Mil Spec 1 Cond 06 AWG WHT A R 919026 044 06 5 2 8 188 Mil Spec 1 Cond 2...

Page 663: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 04 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G TABLE OF CONTENTS ...

Page 664: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 05 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G NOTES ...

Page 665: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 06 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 1 ...

Page 666: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 07 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 2 ...

Page 667: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 08 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 3 ...

Page 668: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 09 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 4 ...

Page 669: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 010 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 5 ...

Page 670: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 011 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 6 ...

Page 671: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 012 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 7 ...

Page 672: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 013 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 8 ...

Page 673: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 014 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 9 ...

Page 674: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 015 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 10 ...

Page 675: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 016 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 11 ...

Page 676: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 017 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 12 ...

Page 677: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 018 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 13 ...

Page 678: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 019 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 14 ...

Page 679: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 020 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 15 ...

Page 680: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 021 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 16 ...

Page 681: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 022 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 17 ...

Page 682: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 023 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 18 ...

Page 683: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 024 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 19 ...

Page 684: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 025 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 20 ...

Page 685: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 026 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 21 ...

Page 686: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 027 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 22 ...

Page 687: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 028 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 23 ...

Page 688: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 029 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 24 ...

Page 689: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 030 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 25 ...

Page 690: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 031 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 26 ...

Page 691: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 032 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 27 ...

Page 692: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 033 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 28 ...

Page 693: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 034 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 29 ...

Page 694: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 035 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 30 ...

Page 695: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 036 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 31 ...

Page 696: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 037 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 32 ...

Page 697: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 038 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 33 ...

Page 698: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 039 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 34 ...

Page 699: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 040 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 35 ...

Page 700: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 041 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 36 ...

Page 701: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 042 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 37 ...

Page 702: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 043 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 38 ...

Page 703: ...VIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 044 AUGUST 2010 6 0 3 0 2 0 2 0 3 0 6 0 5 0 1 0 4 0 15 0 5 5 2 5 3 0 3 0 9 00 6 0 0 0 ELECTRICAL HARNESS 800417 503 G FIGURE 5 2 39 ...

Page 704: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 045 AUGUST 2010 ELECTRICAL HARNESS 800417 503 G FIGURE 6 2 1 ...

Page 705: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417G 046 AUGUST 2010 INTENTIONALLY LEFT BLANK ...

Page 706: ...c Receptacle 6 pin 1 MS3100K 28 22P 5 4 4 56 TYCO Receptacle 8 pin 1 205841 2 5 4 14 57 TYCO Receptacle 9 pin 1 206705 2 5 4 34 58 TYCO Receptacle 16 pin A R 206036 3 5 4 6 60 MAC Receptacle 20 pin 4 930021 502 5 4 13 61 MAC Receptacle 26 pin A R 930021 506 5 4 7 62 TYCO Receptacle 28 pin 1 206152 1 5 4 15 63 Matrix Receptacle 32 pin 2 M83723 83K2232N 5 4 1 65 Positronics Receptacle 104 pin 1 GMCT...

Page 707: ... 4 36 Alt for Tyco 31890 136 Mil Spec Terminal Ring 1 4 6 AWG 1 MS20659 109 5 4 4 Alt for Tyco 31905 138 Mil Spec Terminal Ring 6 22 18 AWG 4 MS25036 102 5 4 25 Alt for Tyco 31885 140 Mil Spec Butt Splice In Line A R M81824 1 X 5 4 3 141 Mil Spec Terminal Ring 6 22 18 AWG A R MS25036 101 5 4 36 Alt for Tyco 31881 142 Mil Spec Screw 3 MS35207 263 6 2 2 143 Mil Spec Washer 3 NAS1149F0332P 6 2 2 144 ...

Page 708: ...nd 14 AWG WHT A R 919026 044 14 5 4 7 185 Mil Spec 1 Cond 10 AWG WHT A R 919026 044 10 5 4 8 187 Mil Spec 1 Cond 06 AWG WHT A R 919026 044 06 5 4 8 188 Mil Spec 1 Cond 20 AWG BLK A R 919026 035 20 5 4 11 190 Mil Spec 1 Cond 20 AWG WHT Shielded A R 919026 044 20 SH 5 4 1 191 Mil Spec 1 Cond 18 AWG WHT Shielded A R 919026 044 18 SH 5 4 1 192 Mil Spec 2 Cond 18 AWG Shielded A R 919026 107 18 5 4 7 19...

Page 709: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 04 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H TABLE OF CONTENTS ...

Page 710: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 05 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H NOTES ...

Page 711: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 06 AUGUST 2010 4A 8A 8A 6A 19C ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 1 ...

Page 712: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 07 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 2 ...

Page 713: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 08 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 3 ...

Page 714: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 09 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 4 ...

Page 715: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 010 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 5 ...

Page 716: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 011 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 6 ...

Page 717: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 012 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 7 ...

Page 718: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 013 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 8 ...

Page 719: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 014 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 9 ...

Page 720: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 015 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 10 ...

Page 721: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 016 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 11 ...

Page 722: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 017 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 12 ...

Page 723: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 018 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 13 ...

Page 724: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 019 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 14 ...

Page 725: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 020 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 15 ...

Page 726: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 021 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 16 ...

Page 727: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 022 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 17 ...

Page 728: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 023 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 18 ...

Page 729: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 024 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 19 ...

Page 730: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 025 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 20 ...

Page 731: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 026 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 21 ...

Page 732: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 027 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 22 ...

Page 733: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 028 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 23 ...

Page 734: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 029 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 24 ...

Page 735: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 030 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 25 ...

Page 736: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 031 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 26 ...

Page 737: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 032 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 27 ...

Page 738: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 033 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 28 ...

Page 739: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 034 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 29 ...

Page 740: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 035 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 30 ...

Page 741: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 036 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 31 ...

Page 742: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 037 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 32 ...

Page 743: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 038 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 33 ...

Page 744: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 039 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 34 ...

Page 745: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 040 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 35 ...

Page 746: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 041 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 36 ...

Page 747: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 042 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 37 ...

Page 748: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 043 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 38 ...

Page 749: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 044 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 5 4 39 ...

Page 750: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 045 AUGUST 2010 ELECTRICAL HARNESS 800417 507 H FIGURE 6 2 2 ...

Page 751: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH417H 046 AUGUST 2010 INTENTIONALLY LEFT BLANK ...

Page 752: ... R PVC 105 3 8 5 1 1 49 Mil Spec Bushing Rubber 3 MS3420 14 5 1 1 50 Mil Spec Plug 32 pin 2 M83723 86R2232N 5 1 1 51 Mil Spec Ring Terminal 1 4 16 14 AWG 1 MS25036 154 5 1 4 Alt for Tyco 31906 52 Mil Spec Ring Terminal 6 22 18 AWG 1 MS25036 102 5 1 1 Alt for Tyco 31885 53 Mil Spec Ring Terminal 6 16 14 AWG 1 MS25036 107 5 1 1 Alt for Tyco 31901 54 Mil Spec Ring Terminal 6 12 10 AWG 1 MS25036 111 5...

Page 753: ...800409 13 6 1 1 90 B C Contacts 1 14 026 5 1 4 91 B C Connector 1 12 003 5 1 4 92 TYCO PIN 1 201570 1 5 10 1 93 TYCO Fusion Tape A R 608036 1 5 10 1 94 TYCO PIN 3 200336 1 5 10 1 95 TYCO PIN 7 201578 1 5 1 1 96 TYCO Receptacle 4 Pin A R 796096 2 5 1 1 97 Washer 2 NAS1149F0463P 6 1 1 98 Washer 1 NAS1149F0363P 6 1 1 99 Washer 66 NAS1149F0332P 6 1 1 100 Washer 4 NAS1149FN832P 6 1 1 101 Washer 4 55008...

Page 754: ...ble Tie sm A R TYB231M 151 Pro Seal 700 Sealer A R 6 1 1 155 Mil Spec 1 Cond 20 AWG WHT A R 919026 044 20 5 1 1 156 Mil Spec 1 Cond 18 AWG WHT A R 919026 044 18 5 1 4 157 Mil Spec 1 Cond 20 AWG BLK A R 919026 035 20 5 1 4 158 Mil Spec 1 Cond 14 AWG WHT A R 919026 044 14 5 1 1 159 Mil Spec 1 Cond 10 AWG WHT A R 919026 044 10 5 1 4 160 Mil Spec 1 Cond 18 AWG BLK A R 919026 035 18 5 1 3 161 Mil Spec ...

Page 755: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 04 AUGUST 2010 SCHEMATIC 800418 501 E TABLE OF CONTENTS ...

Page 756: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 05 AUGUST 2010 SCHEMATIC 800418 501 E NOTES ...

Page 757: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 06 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 5 1 1 ...

Page 758: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 07 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 5 1 2 ...

Page 759: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 08 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 5 1 3 ...

Page 760: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 09 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 5 1 4 ...

Page 761: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 010 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 5 1 5 ...

Page 762: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 011 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 5 2 1 ...

Page 763: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 012 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 5 2 2 ...

Page 764: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 013 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 5 2 3 ...

Page 765: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 014 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 5 2 4 ...

Page 766: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 015 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 5 2 5 ...

Page 767: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 016 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 1 1 ...

Page 768: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 017 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 1 2 ...

Page 769: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 018 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 1 3 ...

Page 770: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 019 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 1 4 ...

Page 771: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 020 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 1 5 ...

Page 772: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 021 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 1 6 ...

Page 773: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 022 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 2 1 ...

Page 774: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 023 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 2 2 ...

Page 775: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 024 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 2 3 ...

Page 776: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 025 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 2 4 ...

Page 777: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 026 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 2 5 ...

Page 778: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 027 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 2 6 ...

Page 779: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 028 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 3 1 ...

Page 780: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 029 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 3 2 ...

Page 781: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 030 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 3 3 ...

Page 782: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 031 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 3 4 ...

Page 783: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 032 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 3 5 ...

Page 784: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 033 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 3 6 ...

Page 785: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 034 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 3 7 ...

Page 786: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 035 AUGUST 2010 SCHEMATIC 800418 501 E FIGURE 6 3 8 ...

Page 787: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418E 036 AUGUST 2010 INTENTIONALLY LEFT BLANK ...

Page 788: ...96094 2 5 3 1 46 Mil Spec Clamp 32 pin 2 M85049 52 1 22N 5 3 1 47 Heat Shrink Tubing A R M23053 5 X Y 5 3 1 48 Alpha Wire Clear PVC Tubing A R PVC 105 3 8 5 3 1 49 Mil Spec Bushing Rubber 3 MS3420 14 5 3 1 50 Mil Spec Plug 32 pin 2 M83723 86R2232N 5 3 1 51 Mil Spec Ring Terminal 1 4 16 14 AWG 1 MS25036 154 5 3 4 Alt for Tyco 31906 52 Mil Spec Ring Terminal 6 22 18 AWG 1 MS25036 102 5 3 1 Alt for T...

Page 789: ... 1 313001 5 3 5 87 Littel Fuse Fuseholder 1 155020 5 3 5 88 MAC R F Filter Assy 1 800409 13 6 3 1 89 TYCO Ring Terminal 5 16 4 AWG A R 33115 5 4 1 90 B C Contacts 1 14 026 5 3 4 91 B C Connector 1 12 003 5 3 4 93 TYCO Fusion Tape A R 608036 1 94 TYCO Socket 10AWG 1 66741 6 5 4 5 97 Washer 2 NAS1149F0463P 6 3 1 98 Washer 1 NAS1149F0363P 6 3 1 99 Washer 66 NAS1149F0332P 6 3 1 100 Washer 4 NAS1149FN8...

Page 790: ...6 044 14 5 3 1 159 Mil Spec 1 Cond 10 AWG WHT A R 919026 044 10 5 3 4 160 Mil Spec 1 Cond 18 AWG BLK A R 919026 035 18 5 3 3 161 Mil Spec 1 Cond 06 AWG WHT A R 919026 044 06 5 3 4 162 Mil Spec 1 Cond 02 AWG WHT A R 919026 044 02 5 3 5 163 Mil Spec 1 Cond 22 AWG GRN A R M22759 16 22 5 5 3 1 164 Mil Spec 1 Cond 22 AWG BLK A R M22759 16 22 0 5 3 1 165 Mil Spec 1 Cond 20 AWG WHT Shielded A R 919026 04...

Page 791: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 04 AUGUST 2010 SCHEMATIC 800418 501 E TABLE OF CONTENTS ...

Page 792: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 05 AUGUST 2010 SCHEMATIC 800418 501 E NOTES ...

Page 793: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 06 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 3 1 M20R ...

Page 794: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 07 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 3 2 M20TN ...

Page 795: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 08 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 3 3 ...

Page 796: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 09 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 3 4 ...

Page 797: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 010 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 3 5 ...

Page 798: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 011 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 3 6 ...

Page 799: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 012 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 4 1 ...

Page 800: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 013 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 4 2 ...

Page 801: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 014 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 4 3 ...

Page 802: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 015 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 4 4 ...

Page 803: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 016 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 4 5 ...

Page 804: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 017 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 4 6 ...

Page 805: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 018 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 5 10 1 ...

Page 806: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 019 AUGUST 2010 S HIELD L INE L OAD SCHEMATIC 800418 501 H FIGURE 6 3 1 ...

Page 807: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 020 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 3 2 ...

Page 808: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 021 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 3 3 ...

Page 809: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 022 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 3 4 ...

Page 810: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 023 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 3 5 ...

Page 811: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 024 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 3 6 AUGUST 2009 ...

Page 812: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 025 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 3 7 ...

Page 813: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 026 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 3 8 ...

Page 814: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 027 AUGUST 2010 S HIELD L INE L OAD SCHEMATIC 800418 501 H FIGURE 6 4 1 ...

Page 815: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 028 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 4 2 ...

Page 816: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 029 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 4 3 ...

Page 817: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 030 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 4 4 ...

Page 818: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 031 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 4 5 ...

Page 819: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 032 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 4 6 ...

Page 820: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 033 AUGUST 2010 SCHEMATIC 800418 501 H FIGURE 6 4 7 ...

Page 821: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH418H 034 AUGUST 2010 INTENTIONALLY LEFT BLANK ...

Page 822: ... 17 5 1 3 24 Left Panel Harness 1 800421 29 5 2 1 26 Placard C B 1 150056 2034 6 2 4 27 Tailcone Harness 1 800422 1 6 1 1 28 Master Relay 1 Harness 1 800422 3 6 1 1 29 Battery Ground Cable 2 800422 5 6 1 1 30 Battery Power Cable 1 800422 7 6 1 1 31 Master Relay 2 Harness 1 800422 9 6 1 1 32 Aux Power Harness 1 800422 11 6 1 1 33 Condenser Relay Harness 1 800422 13 6 1 6 34 Tail Strobe Harness 1 80...

Page 823: ...21 5 1 2 See Dwg Note 87 Fuel Pump Harness 1 800423 23 5 1 2 See Dwg Note 90 Flap Relay Assembly 1 800376 501 9 2 1 91 IAI Flap Relay Assembly 1 9500587001 9 2 1 101 Left Wing INBD Harness 1 800424 1 7 1 3 102 Left Wing OUTBD Harness 1 800424 3 7 1 2 103 Right Wing INBD Harness 1 800424 5 8 1 1 104 Right Wing OUTBD Harness 1 800424 7 8 1 2 105 Left Right INBD Fuel Harness 2 800424 9 7 1 3 106 Left...

Page 824: ...05 5 7 4 154 Light Control Box 1 800399 503 5 7 4 155 Bracket Assy 1 820338 501 5 7 2 156 Flight Panel Assy 1 820357 503 5 7 4 157 Bracket 1 820252 41 5 5 3 158 Current Monitor 1 800221 505 5 5 3 159 IAI Light Control Box 1 9500585002 5 7 4 160 Console Harness 1 800427 1 5 6 1 161 A C Switch Harness 1 800427 3 5 6 1 162 Post Light Harness 1 800427 5 5 6 1 163 E Bus Relay Harness 1 800427 7 5 5 2 1...

Page 825: ...D 3A186 5 7 3 259 Annunciator A R 880090 501 5 7 3 260 Legend w o TKS 1 880090 R047 5 7 3 261 Legend w TKS A R 880090 R048 5 7 3 275 Mount 24 SMB003 0200 9 5 8 1 278 Airspeed Indicator 1 820308 531 5 7 3 279 Artifical Horizon 1 820192 511 5 7 3 282 Mid Continent Altimeter STD 1 5934PA 3A 122 5 7 3 283 Mid Continent Altimeter OPT Dual Window A R 5934PAD 3A186 5 7 3 286 Type 1 CS900 Sealant A R MIL ...

Page 826: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 05 AUGUST 2010 SCHEMATIC 800419 F NOTES ...

Page 827: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 06 AUGUST 2010 SCHEMATIC 800419 F FIGURE 2 1 2 ...

Page 828: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 07 AUGUST 2010 SCHEMATIC 800419 F FIGURE 2 1 3 ...

Page 829: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 08 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 1 1 ...

Page 830: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 09 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 1 1 1 ...

Page 831: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 010 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 1 2 ...

Page 832: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 011 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 1 3 ...

Page 833: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 012 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 1 4 ...

Page 834: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 013 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 1 5 ...

Page 835: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 014 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 1 6 ...

Page 836: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 015 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 1 7 ...

Page 837: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 016 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 1 8 ...

Page 838: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 017 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 2 1 ...

Page 839: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 018 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 2 1 1 ...

Page 840: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 019 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 2 2 ...

Page 841: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 020 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 3 1 ...

Page 842: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 021 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 3 2 ...

Page 843: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 022 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 4 1 ...

Page 844: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 023 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 4 2 ...

Page 845: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 024 AUGUST 2010 A PR H DG S T EC NAV C C FIFTY FIVE X REV A LT VS SCHEMATIC 800419 F FIGURE 5 5 1 ...

Page 846: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 025 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 5 2 ...

Page 847: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 026 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 5 3 ...

Page 848: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 027 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 5 4 ...

Page 849: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 028 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 6 1 ...

Page 850: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 029 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 8 1 ...

Page 851: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 030 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 9 1 ...

Page 852: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 031 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 9 2 ...

Page 853: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 032 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 9 3 ...

Page 854: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 033 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 9 4 ...

Page 855: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 034 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 9 4 ...

Page 856: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 035 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 10 2 ...

Page 857: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 036 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 10 3 ...

Page 858: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 037 AUGUST 2010 SCHEMATIC 800419 F FIGURE 5 10 4 ...

Page 859: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 038 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 1 1 1 ...

Page 860: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 039 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 1 1 2 ...

Page 861: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 040 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 1 1 3 ...

Page 862: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 041 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 1 2 ...

Page 863: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 042 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 1 2 1 ...

Page 864: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 043 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 1 3 ...

Page 865: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 044 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 1 4 ...

Page 866: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 045 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 1 5 ...

Page 867: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 046 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 1 6 2 ...

Page 868: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 047 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 1 7 2 ...

Page 869: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 048 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 1 8 ...

Page 870: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 049 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 2 3 ...

Page 871: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 050 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 2 4 ...

Page 872: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 051 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 3 4 ...

Page 873: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 052 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 3 2 1 ...

Page 874: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 053 AUGUST 2010 SCHEMATIC 800419 F FIGURE 6 3 3 ...

Page 875: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 054 AUGUST 2010 SCHEMATIC 800419 F FIGURE 7 1 1 ...

Page 876: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 055 AUGUST 2010 SCHEMATIC 800419 F FIGURE 7 1 1 1 ...

Page 877: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 056 AUGUST 2010 SCHEMATIC 800419 F FIGURE 7 1 2 ...

Page 878: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 057 AUGUST 2010 SCHEMATIC 800419 F FIGURE 7 1 3 ...

Page 879: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 058 AUGUST 2010 SCHEMATIC 800419 F FIGURE 8 1 1 ...

Page 880: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 059 AUGUST 2010 SCHEMATIC 800419 F FIGURE 8 1 2 ...

Page 881: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 060 AUGUST 2010 SCHEMATIC 800419 F FIGURE 8 1 3 ...

Page 882: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 061 AUGUST 2010 SCHEMATIC 800419 F FIGURE 8 1 4 ...

Page 883: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 062 AUGUST 2010 SCHEMATIC 800419 F FIGURE 9 1 1 ...

Page 884: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 063 AUGUST 2010 SCHEMATIC 800419 F FIGURE 9 2 1 ...

Page 885: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH419F 064 AUGUST 2010 INTENTIONALLY LEFT BLANK ...

Page 886: ...7 2 2 6 1 1 30 Klixon Circuit Breaker A R 7277 2 3 6 1 1 31 Klixon Circuit Breaker A R 7277 2 5 6 1 1 32 Klixon Circuit Breaker A R 7277 2 7 5 6 1 1 33 Klixon Circuit Breaker A R 7277 2 10 6 1 1 34 Klixon Circuit Breaker A R 7277 2 15 6 1 1 35 Klixon Circuit Breaker A R 7277 2 20 6 1 1 36 Klixon Circuit Breaker A R 4200 002 25 6 1 1 37 Klixon Circuit Breaker A R 700 001 30 6 1 1 38 ETA Circuit Bre...

Page 887: ... R FC114N2 5 1 4 87 TYCO Pin 10 08 AWG A R 66259 2 5 1 2 88 TYCO Pin 14 16 AWG 2 66261 2 5 1 2 89 TYCO Plug 3 Pin 1 1 480303 0 5 2 1 90 TYCO Socket 3 60619 1 5 2 1 91 Mil Spec Terminal 5 16 22 18 AWG 1 MS25036 104 5 2 1 Alt for Tyco 31895 92 TYCO Plug 37 Pin 1 206150 1 5 1 6 93 TYCO Clamp 37 Pin 1 206138 1 5 1 6 94 TYCO Terminal 1 4 4 AWG 6 31811 5 2 1 95 Mil Spec Screw 73 MS35207 226 7 1 2 96 Mil...

Page 888: ...18 5 1 3 140 Mil Spec 1 Cond 14 AWG WHT A R 919026 044 14 5 1 1 141 Mil Spec 1 Cond 10 AWG WHT A R 919026 044 10 5 1 1 See Note 2 142 Mil Spec 1 Cond 08 AWG WHT A R 919026 044 08 5 1 2 143 Mil Spec 1 Cond 06 AWG WHT A R 919026 044 06 5 1 2 See Note 2 144 Mil Spec 1 Cond 02 AWG WHT A R 919026 044 02 5 1 2 See Note 2 145 Mil Spec 2 Cond 20 AWG Shielded A R 919026 107 20 SH 5 1 9 146 Mil Spec 1 Cond ...

Page 889: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 04 AUGUST 2010 SCHEMATIC 800420 G NOTES ...

Page 890: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 05 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 1 1 ...

Page 891: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 06 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 1 2 ...

Page 892: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 07 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 1 3 ...

Page 893: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 08 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 1 4 ...

Page 894: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 09 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 1 5 ...

Page 895: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 010 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 1 6 ...

Page 896: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 011 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 1 7 ...

Page 897: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 012 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 1 8 ...

Page 898: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 013 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 1 8 ...

Page 899: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 014 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 2 1 ...

Page 900: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 015 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 2 2 ...

Page 901: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 016 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 2 3 ...

Page 902: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 017 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 2 4 ...

Page 903: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 018 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 2 5 ...

Page 904: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 019 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 2 6 ...

Page 905: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 020 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 2 7 ...

Page 906: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 021 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 2 8 ...

Page 907: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 022 AUGUST 2010 SCHEMATIC 800420 G FIGURE 5 2 9 ...

Page 908: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 023 AUGUST 2010 SCHEMATIC 800420 G FIGURE 6 1 1 ...

Page 909: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 024 AUGUST 2010 SCHEMATIC 800420 G FIGURE 6 1 2 ...

Page 910: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 025 AUGUST 2010 SCHEMATIC 800420 G FIGURE 6 1 3 ...

Page 911: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 026 AUGUST 2010 SCHEMATIC 800420 G FIGURE 6 2 1 ...

Page 912: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 027 AUGUST 2010 SCHEMATIC 800420 G FIGURE 6 2 2 ...

Page 913: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 028 AUGUST 2010 SCHEMATIC 800420 G FIGURE 7 1 2 ...

Page 914: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 029 AUGUST 2010 SCHEMATIC 800420 G FIGURE 7 1 4 ...

Page 915: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 030 AUGUST 2010 SCHEMATIC 800420 G FIGURE 7 2 1 ...

Page 916: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 031 AUGUST 2010 SCHEMATIC 800420 G FIGURE 7 2 2 ...

Page 917: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 032 AUGUST 2010 SCHEMATIC 800420 G FIGURE 7 3 1 ...

Page 918: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 033 AUGUST 2010 SCHEMATIC 800420 G FIGURE 8 1 1 ...

Page 919: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 034 AUGUST 2010 SCHEMATIC 800420 G FIGURE 8 1 2 ...

Page 920: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 035 AUGUST 2010 SCHEMATIC 800420 G FIGURE 8 1 3 ...

Page 921: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH420G 036 AUGUST 2010 INTENTIONALLY LEFT BLANK ...

Page 922: ... 29 0475 thru 29 TBA 11 MAC Electrical Harness Cabin 800421 21 31 0001 thru 31 TBA 29 0475 thru 29 TBA 12 MAC Electrical Harness Cabin 800421 23 31 0001 thru 31 TBA 29 0475 thru 29 TBA 13 MAC Electrical Harness Cabin 800421 25 31 0001 thru 31 TBA 29 0475 thru 29 TBA 14 MAC Electrical Harness Cabin 800421 27 31 0001 thru 31 TBA 29 0475 thru 29 TBA 15 MAC Electrical Harness Cabin 800421 29 31 0001 o...

Page 923: ...ond 22 AWG GRN A R M22759 16 22 5 5 1 1 65 Mil Spec 1 Cond 22 AWG BLK A R M22759 16 22 0 5 5 1 66 Mil Spec 1 Cond 22 AWG RED A R M22759 16 22 2 5 5 1 68 Dale Resistor 70 OHM 10w 1 RH 10 70 5 9 1 69 Dean Recepatcle 2 Pin 1 7021 5 10 1 70 Dean Plug 2 Pin 1 7022 5 10 1 72 Mil Spec 2 Cond SH 22 AWG A R 919026 107 22 5 6 1 74 Tubing A R PVC105 7 5 5 1 76 Newark Potentiometer 1 149 11 502 5 11 1 77 G E ...

Page 924: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 03 AUGUST 2010 SCHEMATIC 800421 F NOTES ...

Page 925: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 04 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 1 1 ...

Page 926: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 05 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 1 2 ...

Page 927: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 06 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 2 1 ...

Page 928: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 07 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 2 2 ...

Page 929: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 08 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 3 1 ...

Page 930: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 09 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 5 1 ...

Page 931: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 010 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 6 1 ...

Page 932: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 011 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 7 1 ...

Page 933: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 012 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 7 2 ...

Page 934: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 013 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 7 3 ...

Page 935: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 014 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 7 4 ...

Page 936: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 015 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 8 1 ...

Page 937: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 016 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 8 2 ...

Page 938: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 017 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 8 3 ...

Page 939: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 018 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 9 1 ...

Page 940: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 019 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 10 1 ...

Page 941: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH421F 020 AUGUST 2010 SCHEMATIC 800421 F FIGURE 5 11 1 ...

Page 942: ... 57 Newark Diode 2 1N2483 5 1 1 59 Kissling Kissling Relay 1 26 57 01 5 3 1 61 Kissling Kissling Relay Adapter 1 26 57 51 5 3 1 63 Anixter Pentacon 5 AMP Fuse 3 313005 5 3 1 64 Anixter Pentacon 10 AMP Fuse A R 313010 5 3 1 70 Transelectric Voltage Converter 1 SM2412 5 5 7 1 73 Electrospec Diode Bridge 1 FB5001 5 3 1 93 Panduit Label 1 CM SCE TP 1 2 4H 9 5 1 1 102 TYCO Plug 3 Pin 1 1 480303 0 5 1 1...

Page 943: ...ot 2 MS25171 3S 5 3 1 154 Mil Spec Ring Terminal 8 22 18 AWG 2 MS25036 149 5 1 1 Alt for Tyco P N 31890 158 Mil Spec Ring Terminal 10 16 14 AWG 1 MS25036 108 5 1 1 Alt for Tyco P N 31903 165 Mil Spec Ring Terminal 5 16 22 18 AWG 1 MS25036 104 5 3 1 Alt for Tyco P N 31893 166 Mil Spec Ring Terminal 5 16 16 14 AWG 1 MS25036 109 5 3 1 Alt for Tyco P N 31905 167 Mil Spec Ring Terminal 5 16 2 AWG 1 MS2...

Page 944: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422E 03 AUGUST 2010 SCHEMATIC 800422 E NOTES ...

Page 945: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422E 04 AUGUST 2010 SCHEMATIC 800422 E FIGURE 5 1 1 ...

Page 946: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422E 05 AUGUST 2010 SCHEMATIC 800422 E FIGURE 5 1 2 ...

Page 947: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422E 06 AUGUST 2010 SCHEMATIC 800422 E FIGURE 5 1 3 ...

Page 948: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422E 07 AUGUST 2010 SCHEMATIC 800422 E FIGURE 5 3 1 ...

Page 949: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422E 08 AUGUST 2010 SCHEMATIC 800422 E FIGURE 5 4 1 ...

Page 950: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422E 09 AUGUST 2010 SCHEMATIC 800422 E FIGURE 5 5 1 ...

Page 951: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422E 010 AUGUST 2010 SCHEMATIC 800422 E FIGURE 5 6 1 ...

Page 952: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422E 011 AUGUST 2010 SCHEMATIC 800422 E FIGURE 5 7 1 ...

Page 953: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422E 012 AUGUST 2010 INTENTIONALLY LEFT BLANK ...

Page 954: ...MAC Tailcone Harness 1 800422 35 5 2 3 31 SR1537 thru 31 TBA 29 SR1537 thru 29 TBA 15 MAC Master Relay 1 Harness 1 800422 37 5 3 3 31 SR1537 thru 31 TBA 29 SR1537 thru 29 TBA 16 MAC Master Relay 2 Harness 1 800422 39 5 4 3 31 SR1537 thru 31 TBA 29 SR1537 thru 29 TBA 17 MAC Battery Ground Cable 1 800422 41 5 3 3 31 SR1537 thru 31 TBA 29 SR1537 thru 29 TBA 18 MAC Battery Power Cable 1 800422 43 5 3 ...

Page 955: ...2 66740 6 5 6 2 80 TYCO Receptacle 3 Pin 1 206207 1 5 6 2 81 TYCO Pin 12 16 AWG 2 66261 2 5 6 2 83 Mil Spec Receptacle 1 MS3506 1 5 5 1 87 MAC BusBar 1 913127 61 5 2 1 88 Klixon Circuit Breaker 5 A A R 7277 2 5 5 2 1 89 Klixon Circuit Breaker 10 A A R 7277 2 10 5 3 2 93 Panduit Label 1 CM SCE TP 1 2 4H 9 5 1 1 94 Screw 1 MS35206 227 5 2 1 95 Screw 3 MS35206 226 5 2 1 96 Lockwasher 4 MS35338 42 5 2...

Page 956: ... Ring Terminal 10 22 18 AWG A R MS25036 103 5 1 2 Alt for Tyco P N 31891 158 Mil Spec Ring Terminal 10 16 14 AWG 1 MS25036 108 5 1 1 Alt for Tyco P N 31903 159 Mil Spec Ring Terminal 10 12 10 AWG A R MS25036 112 5 6 1 Alt for Tyco P N 35109 160 Mil Spec Ring Terminal 6 22 18 AWG 3 MS25036 101 5 2 1 Alt for Tyco P N 31881 161 Mil Spec Ring Terminal 6 16 14 AWG 3 MS25036 101 5 9 1 Alt for Tyco P N 3...

Page 957: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 04 AUGUST 2010 SCHEMATIC 800422 F NOTES ...

Page 958: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 05 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 2 1 ...

Page 959: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 06 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 2 2 ...

Page 960: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 07 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 2 3 ...

Page 961: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 08 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 2 4 ...

Page 962: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 09 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 3 2 ...

Page 963: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 010 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 3 3 ...

Page 964: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 011 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 4 2 ...

Page 965: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 012 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 4 3 ...

Page 966: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 013 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 5 1 ...

Page 967: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 014 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 5 2 ...

Page 968: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 015 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 6 2 ...

Page 969: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 016 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 7 1 ...

Page 970: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 017 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 8 1 ...

Page 971: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 018 AUGUST 2010 SCHEMATIC 800422 F FIGURE 5 9 1 ...

Page 972: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 019 AUGUST 2010 SCHEMATIC 800422 F FIGURE 6 1 1 ...

Page 973: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH422F 020 AUGUST 2010 INTENTIONALLY LEFT BLANK ...

Page 974: ... TBA SR1490 thru 29 TBA 13 MAC Boost Pump Harness M20R 1 800423 23 5 1 9 29 0475 thru SR1490 20 MAC Bracket 2 800375 001 5 1 3 28 Mil Spec Butt Splice 22 16 AWG A R D 436 37 5 1 5 31 Mil Spec Stub Splice 2 D 436 59 5 1 8 33 Mil Spec 1 Cond 20 AWG BLK A R 919026 035 20 5 1 8 34 Mil Spec 1 Cond 20 AWG YEL A R 919026 039 20 5 1 8 35 Mil Spec 1 Cond 22 AWG WHT A R 919026 044 22 5 1 3 36 Mil Spec 1 Con...

Page 975: ...14 AWG A R 201570 1 5 1 1 98 Mil Spec Solder Sleeve Med A R AS83519 1 3 5 1 1 99 Mil Spec Heat Shrink Tubing A R MS23053 5 X Y 5 1 1 102 MAC Plug 8 Pin 1 205838 1 5 1 4 104 MAC Plug 14 Pin 1 930021 001 5 1 6 105 TYCO Plug 4 Pin 1 1 480424 0 5 1 6 106 TYCO Receptacle 4 Pin 1 1 480426 0 5 1 7 107 TYCO Receptacle 8 Pin 1 205841 2 5 1 4 108 TYCO Receptacle 9 Pin 1 206705 2 5 1 8 109 MAC Receptacle 14 ...

Page 976: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH423D 03 AUGUST 2010 ELECTRICAL HARNESS 800423 D NOTES ...

Page 977: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH423D 04 AUGUST 2010 ELECTRICAL HARNESS 800423 D FIGURE 5 1 1 ...

Page 978: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH423D 05 AUGUST 2010 ELECTRICAL HARNESS 800423 D FIGURE 5 1 2 ...

Page 979: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH423D 06 AUGUST 2010 ELECTRICAL HARNESS 800423 D FIGURE 5 1 3 ...

Page 980: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH423D 07 AUGUST 2010 ELECTRICAL HARNESS 800423 D FIGURE 5 1 4 ...

Page 981: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH423D 08 AUGUST 2010 ELECTRICAL HARNESS 800423 D FIGURE 5 1 5 ...

Page 982: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH423D 09 AUGUST 2010 ELECTRICAL HARNESS 800423 D FIGURE 5 1 6 ...

Page 983: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH423D 010 AUGUST 2010 ELECTRICAL HARNESS 800423 D FIGURE 5 1 7 ...

Page 984: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH423D 011 AUGUST 2010 ELECTRICAL HARNESS 800423 D FIGURE 5 1 8 ...

Page 985: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH423D 012 AUGUST 2010 ELECTRICAL HARNESS 800423 D FIGURE 5 1 9 ...

Page 986: ...9 16 22 5 5 1 1 15 Mil Spec 1 Cond 20 AWG WHT A R 919026 44 20 5 1 1 16 Mil Spec 1 Cond 18 AWG WHT A R 919026 44 18 5 1 4 17 Mil Spec 1 Cond 14 AWG WHT A R 919026 44 14 5 1 2 21 Mil Spec 11 Cond Cable Assy A R 919030 505 5 1 2 22 Mil Spec 12 Cond Cable Assy A R 919030 507 5 1 1 24 Mil Spec 3 Cond SH 20 AWG A R 919026 059 20 5 1 2 25 Mil Spec 2 Cond SH 20 AWG A R 919026 107 20 5 1 1 26 TYCO Plug 2 ...

Page 987: ... TYCO Clamp 9 Pin A R 206966 1 5 1 2 59 MAC Receptacle 20 Pin 1 930021 502 5 1 2 60 MAC Plug 20 Pin 2 930021 501 5 1 1 63 MAC Ring Terminal 6 22 18 AWG 1 MS25036 102 5 1 2 64 Mil Spec Ring Terminal 8 22 18 AWG A R MS25036 149 5 1 1 65 Mil Spec Ring Terminal 8 16 18 AWG A R MS25036 153 5 1 1 66 Mil Spec Ring Terminal 10 22 18 AWG A R MS25036 103 5 1 3 ...

Page 988: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH424B 03 AUGUST 2010 SCHEMATIC 800424 B NOTES ...

Page 989: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH424B 04 AUGUST 2010 SCHEMATIC 800424 B FIGURE 5 1 1 ...

Page 990: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH424B 05 AUGUST 2010 SCHEMATIC 800424 B FIGURE 5 1 2 ...

Page 991: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH424B 06 AUGUST 2010 SCHEMATIC 800424 B FIGURE 5 1 3 ...

Page 992: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH424B 07 AUGUST 2010 SCHEMATIC 800424 B FIGURE 5 1 4 ...

Page 993: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH424B 08 AUGUST 2010 SCHEMATIC 800424 B FIGURE 5 2 1 ...

Page 994: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH424B 09 AUGUST 2010 SCHEMATIC 800424 B FIGURE 5 2 2 ...

Page 995: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH424B 010 AUGUST 2010 SCHEMATIC 800424 B FIGURE 5 2 3 ...

Page 996: ...16 22 5 5 1 1 28 Mallory Sonalert Stall Warning 1 SC628 5 1 1 31 MAC Lamp Holder 4 RL6900 1 5 1 1 33 Allyn Welch Bulb Light 4 998502 1 5 1 1 Replacement for Item 31 36 Blaupunkt Cabin Speaker 1 ODX352 5 1 1 38 TYCO Plug 2 Pin 1 1 480318 0 5 1 1 39 TYCO Socket 14 20 AWG A R 60619 1 5 1 1 42 TYCO Receptacle 2 Pin 1 1 480319 0 5 1 1 43 TYCO Pin 14 20 AWG A R 60620 1 5 1 1 44 TYCO Plug 20 Pin 1 930021...

Page 997: ... cond 18 AWG WHT A R 919026 044 18 5 1 3 92 Mil Spec 1 cond 20 AWG BLK A R 919026 035 20 5 1 5 93 Mil Spec 1 cond 14 AWG WHT A R 919026 044 14 5 1 1 94 Mil Spec 1 cond 20 AWG RED A R 919026 037 20 5 1 5 95 Mil Spec 1 cond 08 AWG WHT A R 919026 044 08 5 1 3 96 Mil Spec 1 cond 20 AWG YEL A R 919026 039 20 5 1 5 97 Mil Spec 2 cond SH 20 AWG A R 919026 107 20 5 1 1 98 Mil Spec 3 cond SH 22 AWG A R 919...

Page 998: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH425B 03 AUGUST 2010 SCHEMATIC 800425 B NOTES ...

Page 999: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH425B 04 AUGUST 2010 SCHEMATIC 800425 B FIGURE 5 1 1 ...

Page 1000: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH425B 05 AUGUST 2010 SCHEMATIC 800425 B FIGURE 5 1 2 ...

Page 1001: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH425B 06 AUGUST 2010 SCHEMATIC 800425 B FIGURE 5 1 3 ...

Page 1002: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH425B 07 AUGUST 2010 SCHEMATIC 800425 B FIGURE 5 1 4 ...

Page 1003: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH425B 08 AUGUST 2010 SCHEMATIC 800425 B FIGURE 5 1 5 ...

Page 1004: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH425B 09 AUGUST 2010 SCHEMATIC 800425 B FIGURE 5 1 6 ...

Page 1005: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH425B 010 AUGUST 2010 SCHEMATIC 800425 B FIGURE 5 2 1 ...

Page 1006: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH425B 011 AUGUST 2010 SCHEMATIC 800425 B FIGURE 5 2 2 ...

Page 1007: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH425B 012 AUGUST 2010 SCHEMATIC 800425 B FIGURE 5 2 3 ...

Page 1008: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH425B 013 AUGUST 2010 SCHEMATIC 800425 B FIGURE 5 2 4 ...

Page 1009: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH425B 014 AUGUST 2010 INTENTIONALLY LEFT BLANK ...

Page 1010: ...l Harness 2 1 800426 21 5 1 9 31 0032 thru 31 TBA 29 0475 thru 29 0489 12 MAC G A Switch Harness 1 800426 23 5 1 12 31 0032 thru 31 0049 29 0475 thru 29 0483 13 MAC G A Switch Harness 1 800426 25 5 1 12 31 0050 thru 31 TBA 29 0484 thru 29 TBA 14 MAC Ignition Switch Harness 1 800426 27 5 1 3 31 0001 thru 31 TBA 29 0475 thru 29 TBA 15 MAC Flight Panel 2 Harness 1 800426 29 5 2 1 31 SR1537 thru 31 TB...

Page 1011: ...70 TYCO Pin 20 24 AWG A R 201578 1 5 1 1 71 TYCO Pin 20 24 AWG HD A R 205089 1 5 1 2 72 TYCO Lock Assy 1 D 20419 16 5 1 2 73 Mil Spec Butt Splice In Line A R M81824 1 X 5 1 1 74 TYCO Plug 9 Pin 1 205162 1 5 1 2 Alt for P N DE9P 75 TYCO Clamp 9 Pin 1 DE 24657 5 1 2 76 Fagor Diode Bridge 1 FB5006 5 1 6 79 Littel Fuse Holder A R 155020U 5 1 6 80 Littel Fuse 2A 1 313002 5 1 6 81 Littel Fuse 5A 1 31300...

Page 1012: ... 7 MS35206 227 5 1 6 123 Washer A R MS35338 41 5 1 6 124 Label A R CM SCE TP XXX 134 Mil Spec 1 Cond 22 AWG RED A R M22759 22 2 5 1 3 135 Mil Spec 1 Cond 22 AWG WHT A R 919026 044 22 5 1 2 136 Mil Spec 1 Cond 20 AWG WHT A R 919026 044 20 5 1 1 137 Mil Spec 1 Cond 18 AWG WHT A R 919026 044 18 5 1 4 138 Mil Spec 1 Cond 14 AWG WHT A R 919026 044 14 5 1 5 139 Mil Spec 1 Cond 10 AWG WHT A R 919026 044 ...

Page 1013: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 04 AUGUST 2010 SCHEMATIC 800426 G NOTES ...

Page 1014: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 05 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 1 ...

Page 1015: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 06 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 2 ...

Page 1016: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 07 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 3 ...

Page 1017: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 08 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 4 ...

Page 1018: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 09 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 5 ...

Page 1019: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 010 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 6 ...

Page 1020: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 011 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 7 ...

Page 1021: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 012 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 8 ...

Page 1022: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 013 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 9 ...

Page 1023: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 014 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 10 ...

Page 1024: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 015 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 11 ...

Page 1025: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 016 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 12 ...

Page 1026: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 017 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 1 13 ...

Page 1027: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 018 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 2 1 ...

Page 1028: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 019 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 2 2 ...

Page 1029: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 020 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 2 3 ...

Page 1030: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 021 AUGUST 2010 SCHEMATIC 800426 G FIGURE 5 3 1 ...

Page 1031: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH426G 022 AUGUST 2010 INTENTIONALLY LEFT BLANK ...

Page 1032: ... 23 TYCO Relay 1 1432826 1 5 1 3 24 TYCO Socket 1 4 1419106 0 5 1 3 25 TYCO Push On Terminal 4 2 1393310 0 5 1 3 26 Cherry Switch Switch Defroster Blower 1 E51 50B 5 1 1 28 SLOAN Lamp Holder 2 855S 0 U 5 1 1 30 General Electric Bulb Light 2 GE327 5 1 1 32 Cutler Hammer Switch Flap 2 8906K4731 5 1 1 33 TYCO Plug 2 Pin 1 1 480318 0 5 1 1 34 MAC Plug 20 Pin 1 930021 501 5 1 1 35 TYCO Socket 14 20 AWG...

Page 1033: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH427C 02 AUGUST 2010 SCHEMATIC 800427 C NOTES ...

Page 1034: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH427C 03 AUGUST 2010 SCHEMATIC 800427 C FIGURE 5 1 1 ...

Page 1035: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH427C 04 AUGUST 2010 SCHEMATIC 800427 C FIGURE 5 1 2 ...

Page 1036: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH427C 05 AUGUST 2010 SCHEMATIC 800427 C FIGURE 5 1 3 ...

Page 1037: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH427C 06 AUGUST 2010 INTENTIONALLY LEFT BLANK ...

Page 1038: ... 31 MAC COM2 Antenna Cable 810506 0012 9 1 1 32 MAC NAV Antenna Cable 810506 0013 9 1 1 33 MAC Data Link Antenna Cable 810506 0014 9 1 2 34 MAC DME Antenna Cable 810506 0015 9 1 2 35 MAC COM2B Antenna Cable 810506 0016 9 1 2 36 MAC ADF Antenna Cable 810506 0017 9 1 2 38 Mil Spec Coaxial Cable A R RG400 5 1 1 39 Elect Cable Antenna Cable 352001 9 1 2 42 Telegartner BNC 90 Male A R J01000A0024 5 1 1...

Page 1039: ...34 Pin 1 930021 515 5 1 1 115 MAC Plug PL14B 1 930021 1 5 1 3 116 MAC Receptacle RC14B 1 930021 2 5 1 2 120 Magnecraft Relay Opt 1 W67CSX 3 7 1 1 121 Magnecraft Base Relay Opt 1 70 303 7 1 1 122 MAC Bracket Relay Opt 1 830131 001 7 1 1 124 Positronic Plug PL78A 1 0DD78F00Y600 5 1 1 Alt for item 171 125 Positronic Receptacle RC78A 1 0DD78M00Y600 5 1 2 Alt for item 172 128 Garmin Configuration Modul...

Page 1040: ...01 7 4 1 28 168 Switchcraft Stereo Jack 1 35RAPC4BV4 6 1 8 170 BF Goodrich Installation Kit Skywatch 1 817 10009 002 7 1 1 29 171 TYCO Plug PL78A 1 204509 1 5 1 1 172 TYCO Receptacle RC78A 1 204508 1 5 1 2 173 TYCO Backshell PL RC78A 1 747098 1 5 1 1 174 TYCO Jackscrew Female RC78A 1 207719 1 5 1 1 175 TYCO Jackscrew Male RC78A 1 747784 3 5 1 2 181 Brim Tinned Copper Braid Flat A R 1110 3 32 8 1 4...

Page 1041: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 04 AUGUST 2010 SCHEMATIC 810506 A NOTES ...

Page 1042: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 05 AUGUST 2010 SCHEMATIC 810506 A FIGURE 5 1 1 ...

Page 1043: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 06 AUGUST 2010 SCHEMATIC 810506 A FIGURE 5 1 2 ...

Page 1044: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 07 AUGUST 2010 SCHEMATIC 810506 A FIGURE 5 1 3 ...

Page 1045: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 08 AUGUST 2010 SCHEMATIC 810506 A FIGURE 5 1 4 ...

Page 1046: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 09 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 1 ...

Page 1047: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 010 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 2 ...

Page 1048: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 011 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 3 ...

Page 1049: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 012 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 4 ...

Page 1050: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 013 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 5 ...

Page 1051: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 014 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 6 ...

Page 1052: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 015 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 7 ...

Page 1053: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 016 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 8 ...

Page 1054: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 017 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 9 ...

Page 1055: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 018 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 10 ...

Page 1056: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 019 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 11 ...

Page 1057: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 020 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 12 ...

Page 1058: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 021 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 13 ...

Page 1059: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 022 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 14 ...

Page 1060: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 023 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 15 ...

Page 1061: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 024 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 16 ...

Page 1062: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 025 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 17 ...

Page 1063: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 026 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 18 ...

Page 1064: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 027 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 19 ...

Page 1065: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 028 AUGUST 2010 SCHEMATIC 810506 A FIGURE 6 1 20 ...

Page 1066: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 029 AUGUST 2010 SCHEMATIC 810506 A FIGURE 7 1 1 ...

Page 1067: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 030 AUGUST 2010 SCHEMATIC 810506 A FIGURE 7 2 1 ...

Page 1068: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 031 AUGUST 2010 SCHEMATIC 810506 A FIGURE 7 3 1 ...

Page 1069: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 032 AUGUST 2010 SCHEMATIC 810506 A FIGURE 7 4 1 ...

Page 1070: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 033 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 1 ...

Page 1071: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 034 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 2 ...

Page 1072: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 035 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 3 ...

Page 1073: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 036 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 4 ...

Page 1074: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 037 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 5 ...

Page 1075: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 038 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 6 ...

Page 1076: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 039 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 7 ...

Page 1077: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 040 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 8 ...

Page 1078: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 041 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 9 ...

Page 1079: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 042 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 10 ...

Page 1080: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 043 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 11 ...

Page 1081: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 044 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 12 ...

Page 1082: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 045 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 13 ...

Page 1083: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 046 AUGUST 2010 SCHEMATIC 810506 A FIGURE 8 1 14 ...

Page 1084: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 047 AUGUST 2010 SCHEMATIC 810506 A FIGURE 9 1 1 ...

Page 1085: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH506A 048 AUGUST 2010 SCHEMATIC 810506 A FIGURE 9 1 2 ...

Page 1086: ...ntenna Cable 1 810508 14 34 MAC Data Link Antenna Cable 1 810508 15 35 MAC COM2B Antenna Cable 1 810508 16 36 MAC ADF Antenna Cable 1 810508 17 37 MAC GPS2 Antenna Cable 1 810508 18 38 Mil Spec Coaxial Cable A R RG400 6 1 21 39 Elect Cable Spc Coaxial Cable A R 352001 42 Telegartner BNC 90 Male A R J01000A0024 43 Telegartner BNC 0 Male A R J01000A1255Z 44 Telegartner BNC 0 Female A R J01000A1265 4...

Page 1087: ...Clear Vinyl Tubing A R PVC 105 X 106 Western Filament String Tie BLK or NAT A R WF 25N0F9W 5 1 1 Panduit Cable Tie LG 14 7 A R 1LT4S C 5 1 1 Panduit Cable Tie MED 8 3 A R 1LT2S C 5 1 1 107 Panduit Cable Tie SM 4 8 A R 1LT1M M 5 1 1 108 Cobra Cable Cable Tie MED A R C750LP9M 5 1 1 109 AMP Plug 3 Pin 1 03 09 1032 6 1 22 110 AMP Socket 2 02 09 1119 6 1 22 112 Electrospec Resistor R1 1 3 3K 1 4W 10 6 ...

Page 1088: ... 1 1 172 TYCO Receptacle RC78 1 204508 1 6 1 1 173 TYCO Back Shell PL RC78 2 747098 1 6 1 1 174 TYCO Jackscrew Female PL78 2 207719 1 6 1 1 175 TYCO Jackscrew Male RC78 2 747784 3 6 1 1 180 Brim Tinned Copper Braid Flat A R 1115 13 64 5 1 4 181 Brim Tinned Copper Braid Flat A R 1115 3 32 183 TYCO Label A R CM SCE TP 1 4 4H 9 5 1 1 184 TYCO Label A R CM SCE TP 1 2 4H 9 5 1 1 186 Mil Spec Butt Splic...

Page 1089: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 04 AUGUST 2010 SCHEMATIC 810508 E NOTES ...

Page 1090: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 05 AUGUST 2010 SCHEMATIC 810508 E FIGURE 5 1 1 ...

Page 1091: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 06 AUGUST 2010 SCHEMATIC 810508 E FIGURE 5 1 2 ...

Page 1092: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 07 AUGUST 2010 SCHEMATIC 810508 E FIGURE 5 1 3 ...

Page 1093: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 08 AUGUST 2010 SCHEMATIC 810508 E FIGURE 5 1 4 ...

Page 1094: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 09 AUGUST 2010 SCHEMATIC 810508 E FIGURE 5 1 5 ...

Page 1095: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 010 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 1 ...

Page 1096: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 011 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 2 ...

Page 1097: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 012 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 3 ...

Page 1098: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 013 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 4 ...

Page 1099: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 014 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 5 ...

Page 1100: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 015 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 6 ...

Page 1101: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 016 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 7 ...

Page 1102: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 017 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 8 ...

Page 1103: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 018 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 9 ...

Page 1104: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 019 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 10 ...

Page 1105: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 020 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 11 ...

Page 1106: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 021 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 12 ...

Page 1107: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 022 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 13 ...

Page 1108: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 023 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 13 1 ...

Page 1109: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 024 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 14 ...

Page 1110: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 025 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 14 1 ...

Page 1111: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 026 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 15 ...

Page 1112: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 027 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 16 ...

Page 1113: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 028 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 17 ...

Page 1114: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 029 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 18 ...

Page 1115: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 030 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 19 ...

Page 1116: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 031 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 20 ...

Page 1117: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 032 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 21 ...

Page 1118: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 033 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 1 22 ...

Page 1119: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 034 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 1 ...

Page 1120: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 035 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 2 ...

Page 1121: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 036 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 3 ...

Page 1122: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 037 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 4 ...

Page 1123: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 038 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 5 ...

Page 1124: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 039 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 6 ...

Page 1125: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 040 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 7 ...

Page 1126: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 041 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 8 ...

Page 1127: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 042 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 9 ...

Page 1128: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 043 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 10 ...

Page 1129: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 044 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 11 ...

Page 1130: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 045 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 12 ...

Page 1131: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 046 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 13 ...

Page 1132: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 047 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 14 ...

Page 1133: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 048 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 15 ...

Page 1134: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 049 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 16 ...

Page 1135: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 050 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 17 ...

Page 1136: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 051 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 18 ...

Page 1137: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 052 AUGUST 2010 SCHEMATIC 810508 E FIGURE 6 2 19 ...

Page 1138: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 053 AUGUST 2010 VIEW LOOKING DOWN C2 C1 C N C N O SCHEMATIC 810508 E FIGURE 7 1 1 ...

Page 1139: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 054 AUGUST 2010 SCHEMATIC 810508 E FIGURE 7 2 1 ...

Page 1140: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 055 AUGUST 2010 SCHEMATIC 810508 E FIGURE 7 3 1 ...

Page 1141: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 056 AUGUST 2010 SCHEMATIC 810508 E FIGURE 7 4 1 ...

Page 1142: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 057 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 1 ...

Page 1143: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 058 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 2 ...

Page 1144: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 059 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 3 ...

Page 1145: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 060 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 4 ...

Page 1146: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 061 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 5 ...

Page 1147: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 062 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 5 1 ...

Page 1148: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 063 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 5 2 ...

Page 1149: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 064 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 6 ...

Page 1150: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 065 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 7 ...

Page 1151: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 066 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 8 ...

Page 1152: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 067 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 9 ...

Page 1153: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 068 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 10 ...

Page 1154: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 069 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 11 ...

Page 1155: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 070 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 12 ...

Page 1156: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 071 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 13 ...

Page 1157: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 072 AUGUST 2010 SCHEMATIC 810508 E FIGURE 8 1 14 ...

Page 1158: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 073 AUGUST 2010 SCHEMATIC 810508 E FIGURE 9 1 1 ...

Page 1159: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date Rev Date Page EH508E 074 AUGUST 2010 SCHEMATIC 810508 E FIGURE 9 1 2 ...

Page 1160: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL CHAPTER 95 SPECIAL TOOLS ...

Page 1161: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL INTENTIONALLY LEFT BLANK ...

Page 1162: ...ANCE MANUAL Date 2006 Rev Date CHAPTER 95 SPECIAL TOOLS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 95 Effectivity 1 12 06 95 Contents 3 12 06 95 00 00 5 12 06 95 00 00 6 08 10 95 00 00 7 08 10 95 00 00 8 12 06 95 EFFECTIVITY AUGUST 2010 ...

Page 1163: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date INTENTIONALLY LEFT BLANK ...

Page 1164: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date CHAPTER 95 SPECIAL TOOLS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 95 00 00 Special Tools 5 95 CONTENTS ...

Page 1165: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date INTENTIONALLY LEFT BLANK ...

Page 1166: ... 30 LB CYLINDER R 134A CHARGING MANIFOLD W GAUGES ELECTRONIC LEAK DETECTOR ESTER RL 500S R 134A REFRIGERANT OIL LOCTITE 55431 THREAD SEALANT HOSE ADAPTER 1 2 MALE ACME TO 1 4 FEMALE FLARE VACUUM PUMP 0 30 IN HG THERMOMETER 0 150oF SCALE 0 50 LBS R 134A RECLAIM RECYCLE CART 21 54 03 8082A BORROUGH S TOOL 21 54 04 BT 33 73F OR BORROUGH S TOOL 22 AUTOPILOT SYSTEM 22 10 04 T10 00110 01 GARMIN SERVO AD...

Page 1167: ...0038 501 SHOCK DISC REPLACEMENT TOOL GSE 030010 SHOCK DISC REPLACEMENT TOOL 33 LIGHTS 34 NAVIGATION 34 22 00 AOE 6054 ASSOCIATED GROWLER ARMA TURE TESTER 35 OXYGEN 35 00 01 MAC 870025 501 AVOX SYSTEMS SCOTT AVI ATION RECHARGING VALVE 35 00 03 PURITAN BENNETT RECHARGING VALVE 37 VACUUM 39 ELECTRICAL PANELS 51 STRUCTURE 52 DOORS 53 FUSELAGE 55 STABILIZERS 56 WINDOWS 57 WINGS 61 PROPELLERS 61 00 20 B...

Page 1168: ...TION MANUAL 73 ENGINE FUEL 74 IGNITION 74 00 00 M 18 TCM MAINTENANCE AND OVERHAUL MANUAL 76 ENGINE CONTROLS 77 ENGINE INDICATING 190 00450 03 Rev A OR LATER GARMIN G1000 INTEGRATED FLIGHT DECK 78 EXHAUST 79 OIL 80 STARTING X30592 TCM STARTER MOTOR SER VICE INSTRUCTIONS 81 TURBOCHARGER 81 20 00 M 18 TCM MAINTENANCE AND OVERHAUL MANUAL 91 SCHEMATICS 95 SPECIAL EQUIPMENT 1 Part of Aircraft Flyaway Ki...

Page 1169: ...MOONEY AVIATION COMPANY INC M20TN SERVICE MAINTENANCE MANUAL Date 2006 Rev Date Page 8 INTENTIONALLY LEFT BLANK 95 00 00 ...

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