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GENERAL.

This chapter explains the removal and installation procedures for the wings and related components

installed on this aircraft.

DESCRIPTION.

Each wing panel is an all metal, full cantilever, semi-monocoque type structure with removable tips and

access panels. Attached to each wing are the aileron, flap, main landing gear and fuel tank. The wings are
attached to each side of the fuselage by inserting the butt ends of the main spars into a spar box carry through.
The spar box is an integral part of the fuselage structure which provides, in effect, a continuous main spar with
splices at each side of the fuselage. There are also fore and aft attachments at the front and rear spars.

—NOTE—

The major subassemblies of the wing may be removed
individually or the wing may be removed as a unit. To remove a
wing, a fuselage and wing supporting cradle is required.

AUXILIARY STRUCTURE.

REMOVAL OF WING TIP.

1. Remove the screws holding the wing tip to the wing, being careful not to damage the wing or wing tip.
2. Pull off the wing tip far enough to disconnect the position and strobe light wire assembly. The ground

lead may be disconnected at the point of connection on the wing rib, and the positive lead may be disconnected
at the wire terminal or unscrewed from the light assembly.

3. Inspect the wing tip to ascertain that it is free of cracks, severe nicks and minor damage. If repair is

required, refer to Chapter 51.

INSTALLATION OF WING TIP.

1. Place the wing tip in a position that the navigation and strobe light leads may be connected. Connect

the ground lead to the wing rib by use of a screw and nut, and the positive lead to the position light by
connecting the wire terminals or screwing the connectors together. Insulate the wire terminals and be certain
that the ground lead is free of dirt and film to insure a good connection.

2. Insert the wing tip into position and install the screws around the tip. Use caution to refrain from

damaging the wing tip or wing. Check operation of the lights.

REPAIR OF WING TIP.

Fiberglass wing tips may be repaired in accordance with fiberglass repair procedures given in the structural

repairs portion of Chapter 51. Badly damaged thermoplastic tips should be replaced.

57-20-03

Page 57-01

December 1, 1978

2K2

PIPER AIRCRAFT

PA-28RT-201 / 201T

MAINTENANCE MANUAL

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Содержание Arrow IV

Страница 1: ...ARROW IV MAINTENANCE MANUAL CARD 1 OF 3 PA 28RT 201 ARROW IV PA 28RT 201T TURBO ARROW IV PIPER AIRCRAFT CORPORATION PART NUMBER 761 694 1A1 Courtesy of Bomar Flying Service www bomar biz...

Страница 2: ...he major System Chapters are then broken down into Sub System Sections These sections are identified by the second element of the standardized numbering system The number 40 of the basic number series...

Страница 3: ...inental Motors Aircraft Products Division Mobile Alabama 36601 Operators Handbook CONTINENTAL Form No X 30512 Teledyne Continental Motors Aircraft Products Division Mobile Alabama 36601 PROPELLER Over...

Страница 4: ...753 502 Altimatic III C Service Manual Piper P N 761 602 79 Vero Beach Avionics Wiring Diagrams Manual Piper P N 761 713 AEROFICHE PA 28RT 201 201T Parts Catalog Piper P N 761 693 INSPECTION PA 28RT...

Страница 5: ...evision lines indicate only current revisions with changes and additions to existing text and illustrations Changes in capitalization spelling punctuation indexing the physical location of the materia...

Страница 6: ...R 8018001 to 28R 8018106 inclusive PA 28RT 201 Arrow IV 1981 Serial Numbers 28R 8118001 to 28R 8118082 inclusive PA 28RT 201 Arrow IV 1982 Serial Numbers 28R 8218001 to 28R 8218026 inclusive PA 28RT 2...

Страница 7: ...ARKING AND MOORING 1C18 11 REQUIRED PLACARDS 1C22 12 SERVICING 1D5 20 STANDARD PRACT AIRFRAME 1E14 21 ENVIRONMENTAL SYSTEM 1E21 22 AUTOFLIGHT 1H1 23 COMMUNICATIONS 1H8 24 ELECTRICAL POWER 1H17 27 FLIG...

Страница 8: ...S 2J19 57 WINGS 2J24 61 PROPELLER 3A18 70 STANDARD PRACTICES ENGINE 3B9 71 POWER PLANT 3B12 73 ENGINE FUEL AND CONTROL 3C12 74 IGNITION 3D7 77 ENGINE INDICATING 3F16 78 EXHAUST 3G1 79 OIL SYSTEM 3G6 8...

Страница 9: ...12 10 Lubrication Chart Back Up Extender 1E11 12 11 Lubrication Chart Air Conditioning Condenser 1E12 20 1 Torque Wrench Extension 1E16 20 2 Method of Installing Rod End Bearings 1E17 21 1 Cabin Heat...

Страница 10: ...ifier End Shield Assembly 1I14 24 12 Testing Stator 1I16 24 13 Removal of Pulley 1I16 24 14 Removal of Bearing 1I16 24 15 Removal of Rectifier End Shield Bearing 1I16 24 16 Testing Rotor for Ground 1I...

Страница 11: ...Rigging Tool 1L1 27 17 Methods of Securing Trim Cables 1L4 27 18 Stabilator Trim Control 1L5 27 19 Flap Controls 1L9 27 20 Flap Step Adjustment 1L11 27 21 Flap Rigging Tool 1L11 27 22 Flap Rigging 1L...

Страница 12: ...rake 2F8 32 19 Toe Brake Installation 2F9 32 20 Brake Cylinder 17000 Toe Brake 2F10 32 21 Brake Cylinder 10 30 Toe Brake 2F11 32 22 Adjustment of Nose Gear Down Limit Switch 2F15 32 23 Adjustment of M...

Страница 13: ...stallation PA 28RT 201 3C7 71 4 Engine Cowling Installation PA 28RT 201 3C11 73 1 Schematic Diagram of Fuel Injection System 3C15 73 2 Fuel Injector Nozzle Assembly 3C17 73 3 Engine Controls 3C17 73 4...

Страница 14: ...32 Assembly Tool 3E16 74 33 Using Assembly Tool 3E16 74 34 Measuring Lead Assembly Length 3E17 74 35 Cutting Metallic Braid From End of Lead 3E17 74 36 Unbraiding Metallic Shielding 3E17 74 37 Forming...

Страница 15: ...ing Stand 3K7 95 7 York Compressor and Fabricated Oil Dipstick PA 28RT 201 3K7 95 8 Fabricated Gear Back Up Extender Actuator Aligning Tool 3K8 95 9 Fabricated Stabilator Rigging Tool 3K9 95 10 Fabric...

Страница 16: ...ading Particulars Hydraulic System 2C10 2903 Characteristics Hydraulic Pump Motor 2C15 3201 Troubleshooting Landing Gear 2D10 3202 Main Gear Service Tolerances 2D20 3203 Toe In Toe Out Correction Char...

Страница 17: ...0 7704 Troubleshooting Oil Temperature Indicators 3F20 7705 Troubleshooting Exhaust Gas Temperature Gauge Alcor 3F22 7706 Troubleshooting Cylinder Head Temperature Gauge 3F22 8001 Troubleshooting Star...

Страница 18: ...CHAPTER AIRWORTHINESS LIMITATIONS 1A18...

Страница 19: ...LE OF CONTENTS EFFECTIVITY CHAPTER SECTION GRID SUBJECT SUBJECT NO EFFECTIVITY 4 00 00 AIRWORTHINESS LIMITATIONS 1A20 4 00 01 General 1A20 4 Cont Effec Page 1 Revised February 23 1979 1A19 PIPER AIRCR...

Страница 20: ...e safe life of the airframe structure will be released when the information becomes available 2 The safe life limit of the propeller blades is unlimited NOTE Refer to the LIMITATIONS in the Pilot s Op...

Страница 21: ...THIS PAGE INTENTIONALLY LEFT BLANK 1A21 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 22: ...CHAPTER TIME LIMITS MAINT CHECKS 1A22...

Страница 23: ...A24 8 82 5 10 02 Preflight Checks 1A24 5 10 03 Overlimits Inspection 1A24 5 20 00 SCHEDULED MAINTENANCE CHECKS 1B1 5 20 01 Periodic Inspections 1B1 4R 8 82 5 20 02 Programmed Inspection 1B14 3R 12 81...

Страница 24: ...eration is required at each of the inspection intervals as indicated by a circle O If an item is not entirely accessible or must be removed refer to the applicable chapter of this manual for instructi...

Страница 25: ...ct installation O O O 11 Overhaul Hartzell propeller refer to latest revision of Hartzell Service Letter 61 12 Overhaul McCauley propeller refer to latest revision of McCauley Service Bulletin 137 B E...

Страница 26: ...ght of contact springs O O 17 Inspect magnetos to engine timing See Note 17 O O O 18 Overhaul or replace magnetos See Note 7 19 Remove induction air filter and tap gently to remove dirt particles Repl...

Страница 27: ...ng chafing cracks deterioration and correct installation See latest revision of Piper Service Bulletin 561 O O O O 43 Check air conditioning compressor oil level See Note 15 44 Inspect condition and t...

Страница 28: ...to Primary Circuit before working on engine 1 Remove engine cowl and inspect for damage O O O O 2 Clean and inspect cowling for cracks distortion and loose or missing fasteners See Note 25 O O O 3 Dra...

Страница 29: ...continuity O O O 18 Inspect magneto points for condition and proper clearance O O O 19 Inspect magneto for oil leakage O O O 20 Inspect breaker felts for proper lubrication O O O 21 Inspect distributo...

Страница 30: ...ngine baffles O O O 45 Inspect all wiring connected to the engine or accessories O O O 46 Inspect rubber engine mount bushings for deterioration Replace as required O O O 47 Inspect fire wall seals O...

Страница 31: ...d O O O 12 Replace instrument air central air filter O O O 13 Inspect or replace vacuum regulator filter O O O 14 Inspect altimeter Calibrate altimeter system in accordance with FAR 91 170 if appropri...

Страница 32: ...not loosened and locknuts are tight O O O 20 Inspect stabilator surfaces for damage O O O 21 Inspect stabilator tab hinges horn and attachments for damage and operation O O O 22 Inspect stabilator at...

Страница 33: ...and condition O O O 6 Inspect aileron cables pulleys and bellcranks for damage and operation O O O 7 Inspect flaps and attachments for damage and operation O O O 8 Inspect condition of bolts used wit...

Страница 34: ...and bolts for condition and security O O O 16 Inspect downlock for operation and adjustment See Note 20 O O O O 17 Inspect torque link bolts and bushings Rebush as required O O 18 Inspect drag and sid...

Страница 35: ...peration O O O O 14 Check propeller smoothness O O O O 15 Check propeller governor action O O O O 16 Check engine idle O O O O 17 Check electronic equipment operation O O O O 18 Check operation of Aut...

Страница 36: ...eriod 8 Replace flexible oil lines as required but no later than 1000 hours of service 9 Check throttle body attaching screws for tightness the correct torque for these screws is 40 to 50 inch pounds...

Страница 37: ...ix Service Bulletin 612 for inspecting magneto and ignition harnesses 24 Refer to VSP 69 NOTE Printed copies of this 100 Hour Annual Inspection Report can be obtained from Piper Service Sales under Pi...

Страница 38: ...ions or incidents an immediate inspection would be required to insure further safe flight 2 Hard or Overweight Landing This inspection should be performed after a known rough landing is made or when a...

Страница 39: ...THIS PAGE INTENTIONALLY LEFT BLANK 1B15 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 40: ...CHAPTER DIMENSIONS AND AREAS 1B16...

Страница 41: ...EFFECTIVITY 6 10 00 DIMENSIONS 1B18 2 79 6 20 00 Station Reference Lines 1B24 2 79 6 30 00 Access and Inspection Provisions 1C2 2 79 6 40 00 Weight and Balance Data 1C2 6 50 00 Serial Number Plate 1C2...

Страница 42: ...in Width 34 25 in 31 38 in Length 33 65 in 57 08 in Oil Sump Capacity 8 U S quarts 8 U S quarts Oil Consumption Maximum 010 lb bhp hr 009 above 75 power Fuel Aviation Grade Minimum and Specified Octan...

Страница 43: ...tor Overvoltage Relay WICO X16799B X16799B PROPELLER Constant Speed Manufacturer McCauley Hartzell Hub Model B2D34C2131 or 2D34C2152 BHC C2YF 1 BF Blade Model 90DHA 161or 90DJA 14E2 F8459A 8R Diameter...

Страница 44: ...25 in Wheel Tread 10 ft 5 72 in 10 ft 5 72 in Wheel Base 7 ft 10 38 in 7 ft 10 38 in Nose Wheel Travel 30 2 left and right 30 2 left and right Turning Radius Min Nose Wheel 15 ft 8 4 in 15 ft 8 4 in W...

Страница 45: ...Airplane 5 gal 5 gal OVERALL Gross Weight lbs 2750 2900 Wing Loading lbs sq ft 16 2 17 0 Length Ft 24 ft 8 25 in 25 ft 0 23 in Width Span Wing Tip to Wing Tip 35 ft 5 11 in 35 ft 5 11 in Height Static...

Страница 46: ...Figure 6 1 Three View of PA 28RT 201T 6 10 00 Page 6 05 Revised August 17 1982 1B22 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 47: ...Figure 6 2 Three View of PA 28RT 201 6 10 00 Page 6 06 Revised August 17 1982 1B23 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 48: ...in the vertical or horizontal direction from a given reference line which indicates station locations of structural members of the airplane Station O of the fuselage is 44 5 inches ahead of the lower...

Страница 49: ...Figure 6 3 Station Reference Lines of PA 28RT 201 201T 6 20 00 Page 6 08 Revised July 13 1983 1C1 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 50: ...section of the fuselage be sure the airplane is supported at the tail skid WEIGHT AND BALANCE DATA When figuring various weight and balance computations the empty static and gross weight and center o...

Страница 51: ...Figure 6 4 Access Plates and Panels 6 50 00 Page 6 10 Interim Revision February 27 1995 1C3 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 52: ...THIS PAGE INTENTIONALLY LEFT BLANK 1C4 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 53: ...CHAPTER LIFTING AND SHORING 1C5...

Страница 54: ...G AND SHORING TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION GRID SUBJECT SUBJECT NO EFFECTIVITY 7 10 01 JACKING 1C7 7 Cont Effec Page 1 Revised February 23 1979 1C6 PIPER AIRCRAFT PA 28RT 201 201T MAI...

Страница 55: ...ose gear actuating cylinder This may be used along with the wing jack points to raise the airplane or alone it may be used to raise the front end 2 Attach the tail support to the tail skid Place appro...

Страница 56: ...THIS PAGE INTENTIONALLY LEFT BLANK 1C8 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 57: ...CHAPTER LEVELING AND WEIGHING 1C9...

Страница 58: ...NG TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION GRID SUBJECT SUBJECT NO EFFECTIVITY 8 10 01 LEVELING 1C11 8 20 01 WEIGHING 1C11 8 Cont Effec Page 1 Revised February 23 1979 1C10 PIPER AIRCRAFT PA 28R...

Страница 59: ...hen deflate the nose wheel until the proper position is reached 2 To laterally level the airplane place a level across the spar box assembly located under the rear seat Refer to Figure 8 2 Raise or lo...

Страница 60: ...Figure 8 1 Leveling Longitudinally Figure 8 2 Leveling Laterally Figure 8 3 Weighing Arrangement 8 20 01 Page 8 02 Revised July 13 1983 1C12 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 61: ...THIS PAGE INTENTIONALLY LEFT BLANK 1C13 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 62: ...CHAPTER TOWING AND TAXIING 1C14...

Страница 63: ...NG TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION GRID SUBJECT SUBJECT NO EFFECTIVITY 9 10 01 TOWING 1C16 9 20 01 TAXIING 1C16 9 Cont Effec Page 1 Revised February 23 1979 1C15 PIPER AIRCRAFT PA 28RT 2...

Страница 64: ...empting to taxi the airplane ground personnel should be checked out by a qualified pilot or other responsible person Engine starting and shut down procedures should be covered as well When it is ascer...

Страница 65: ...THIS PAGE INTENTIONALLY LEFT BLANK 1C17 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 66: ...CHAPTER PARKING AND MOORING 1C18...

Страница 67: ...NTS EFFECTIVITY CHAPTER SECTION GRID SUBJECT SUBJECT NO EFFECTIVITY 10 10 01 PARKING 1C20 10 20 01 MOORING 1C20 10 20 02 Locking Airplane 1C20 10 Cont Effec Page 1 Revised February 23 1979 1C19 PIPER...

Страница 68: ...ection and security under various weather conditions In order to properly moor the airplane use the following procedures 1 Head the airplane into the wind if possible 2 Block the wheels 3 Lock the ail...

Страница 69: ...THIS PAGE INTENTIONALLY LEFT BLANK 1C21 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 70: ...CHAPTER REQUIRED PLACARDS 1C22...

Страница 71: ...ITY CHAPTER SECTION GRID SUBJECT SUBJECT NO EFFECTIVITY 11 20 00 EXTERIOR PLACARDS AND MARKINGS 1C24 2R 7 81 11 30 00 INTERIOR PLACARDS AND MARKINGS 1D1 11 Cont Effec Page 1 Revised February 23 1979 1...

Страница 72: ...ANK 36 GALLONS 11 PLACARD EXTERNAL POWER 34 PLACARD L TANK 36 GALLONS 12 PLACARD WARNING 35 PLACARD FUEL OFF 13 PLACARD PITCH TRIM 36 PLACARD AIRCRAFTLIMITATIONS 14 PLACARD WARNING PLACARD AIRCRAFT LI...

Страница 73: ...INTERIOR PLACARDS AND MARKINGS Figure 11 1 Placards and Decals cont 11 30 00 Page 11 02 Revised February 23 1979 1D1 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 74: ...THIS PAGE INTENTIONALLY LEFT BLANK 1D2 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 75: ...THIS PAGE INTENTIONALLY LEFT BLANK 1D3 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 76: ...THIS PAGE INTENTIONALLY LEFT BLANK 1D4 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 77: ...CHAPTER SERVICING 1D5...

Страница 78: ...ing Gear 1D14 12 20 03 Oleo Struts 1D14 12 20 04 Filling Oleo Struts 1D15 12 81 12 20 05 Inflating Oleo Struts 1D16 12 20 06 Brake System 1D16 12 20 07 Filling Brake Cylinder Reservoir 1D16 12 20 08 D...

Страница 79: ...Exterior Surfaces 1D21 12 20 26 Windshield and Windows 1D21 12 20 27 Headliner Side Panels and Seats 1D22 12 20 28 Carpets 1D22 12 20 29 Lubrication Instructions 1D22 12 20 30 Application of Oil 1D22...

Страница 80: ...plenishment of fuel oil hydraulic fluid tire pressures lubrication requirements and other required items Figure 12 1 Servicing Points PA 28RT 201 12 00 00 Page 12 01 Revised February 23 1979 1D8 PIPER...

Страница 81: ...Figure 12 2 Servicing Points PA 28RT 201T 12 00 00 Page 12 02 December 1 1978 1D9 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 82: ...o the filler neck Each wing tank has a capacity of 38 1 2 U S gallons for a total capacity of 77 U S gallons Five U S gallons are considered unusable fuel FUEL ANTI ICING ADDITIVE This aircraft is app...

Страница 83: ...e fuel strainer by opening the quick drain on the strainer 3 Examine the contents of the container placed under the fuel strainer drain for water and sediment and dispose of the contents CAUTION When...

Страница 84: ...y removing the lockwire from the bolthead at the end of the filter loosening the bolt and removing the filter assembly from the adapter 2 Before discarding the filter element remove the outer perforat...

Страница 85: ...the following Also refer to the latest revision of Lycoming Service Information No 1014 1 In engines that have been operating on straight mineral oil for several hundred hours a change to additive oi...

Страница 86: ...cribed determine whether it needs air or oil by rocking the airplane If the oleo strut oscillated with short strokes approximately one inch and the airplane settles to its normal position within one o...

Страница 87: ...ber By watching the fluid pass through the plastic hose it can be determined when the strut is full and no air is present in the chamber D When air bubbles cease to flow through the hose compress the...

Страница 88: ...ficiency Spongy brake pedal action is often an indication that the brake fluid reservoir is running low on fluid Instructions for filling the reservoir are given in the next paragraph When found neces...

Страница 89: ...the inside of the tire with toluol Apply a coat of patch cement to both the patch and the inside center of the tire in line with the chalk marks When the cement has dried install the patches making c...

Страница 90: ...For detailed information on this system refer to Chapter 24 of this manual BATTERY Access to the battery is through the aft side of the baggage compartment on the PA 28RT 201T and located in the engin...

Страница 91: ...secure 2 Adjust the control cable to position the roller on the arm assembly clear of the door in the closed position Check that when the cockpit control is in the closed position the door is properl...

Страница 92: ...in accordance with the Lubrication Chart Additional service information for the propeller may be found in Chapter 61 CLEANING ENGINE COMPARTMENT Before cleaning the engine compartment place a strip of...

Страница 93: ...solution with a rag sponge or soft bristle brush 3 To remove stubborn oil and grease use a cloth dampened with naptha 4 Where exhaust stains exist allow solution to remain on the surface longer 5 Any...

Страница 94: ...regarding the locations time intervals and type of lubricants used may be found in the Lubrication Chart To insure the best possible results from the application of lubricants the following precaution...

Страница 95: ...bearings from the wheel hub and clean thoroughly with a suitable solvent When repacking with grease be sure the lubricant enters the space between the rollers in the retainer ring Do not pack the gre...

Страница 96: ...IL L 7870 100 HRS 10 OLEO STRUT FILLER POINT MAIN GEAR MIL H 5606 AS REQUIRED 11 HYDRAULIC PUMP RESERVOIR MIL H 5606 100 HRS 12 BRAKE RESERVOIR MIL H 5606 100 HRS SPECIAL INSTRUCTIONS 1 Main Wheel Bea...

Страница 97: ...Figure 12 4 Lubrication Chart Landing Gear Main cont 12 20 32 Page 12 18 December 1 1978 1E1 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 98: ...TENSION SPRING SHIMMY DAMPENER AND ALIGNING ROLLER PIVOT POINTS MIL L 7870 100 HRS 10 STEERING BELLCRANK PIVOT POINTS AND ROD ENDS MIL G 7711 100 HRS 11 NOSE GEAR OLEO STRUT FILLER POINT MIL H 5606 A...

Страница 99: ...Figure 12 5 Lubrication Chart Landing Gear Nose cont 12 20 32 Page 12 20 December 1 1978 1E3 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 100: ...TRIM CONTROL WHEEL MIL L 7870 100 HRS 7 O RING CONTROL SHAFT BUSHING PARKER O RING LUBRICANT AS REQUIRED 8 TEE BAR PIVOT POINT MIL L 7870 100 HRS 9 CONTROL COLUMN CHAIN MIL L 7870 500 HRS 10 CONTROL C...

Страница 101: ...ISM AERO LUBRIPLATE MAG 1 AND TURNBUCKLE END OR AERO SHELL 7 100 HRS 4 FLAP RETURN AND TENSION CHAINS MIL L 7870 500 HRS 5 AILERON CONTROL ROD END BEARINGS MIL L 7870 100 HRS 6 AILERON BELLCRANK CABLE...

Страница 102: ...S 4 BRAKE ROD ENDS MIL L 7870 100 HRS 5 STABILATOR TRIM SCREW AERO LUBRIPLATE MAG 1 FISKE BROS REFINING CO OR AERO SHELL 7 100 HRS 6 STABILATOR SCREW ROD ENDS MIL L 7870 100 HRS 7 STABILATOR HINGE POI...

Страница 103: ...THIS PAGE INTENTIONALLY LEFT BLANK 1E7 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 104: ...1 LEG RETAINER CLIP AND CAM FISKE BROS REFINING CO OR AERO SHELL 7 100 HRS 5 SEAT LATCH STOP PIVOT POINT COPILOT MIL L 7870 100 HRS SPECIAL INSTRUCTIONS Apply fluorocarbon dry lubricant to door seals...

Страница 105: ...500 HRS 7 ALTERNATOR AND COMPRESSOR IDLER PULLEY BEARINGS MIL G 81322 100 HRS SPECIAL INSTRUCTIONS 1 Air Filter To clean filter tap gently to remove dirt particles Do not blow out with compressed air...

Страница 106: ...ured or damaged 2 See latest revision of TCM Service Bulletin M75 2 for recommended oil and filter change period The engine lubricating oil system is serviced with MIL C 6529 Type II for the initial f...

Страница 107: ...G ATTACHMENT POINTS MIL L 7870 100 HRS 4 ACTUATING ROD CONTACT POINTS AERO LUBRIPLATE AERO SHELL 7 100 HRS SPECIAL INSTRUCTIONS 1 Diaphragm Shaft and Bushing Soft film silicone compound MIL C 21567 is...

Страница 108: ...G 23827 500 HRS SPECIAL INSTRUCTIONS Transmission to be 1 2 full of grease Apply grease during assembly and lubricate transmission ball nut and screw with MIL G 23827 grease Figure 12 11 Lubrication...

Страница 109: ...THIS PAGE INTENTIONALLY LEFT BLANK 1E13 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 110: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E14...

Страница 111: ...0 00 02 Method of Installing Rod End Bearings 1E17 20 10 00 AIRCRAFT FINISH CARE CLEANING 1E18 20 10 01 Exterior Surfaces 1E18 20 10 02 Windshield and Windows 1E18 20 10 03 Headliner Side Panels and S...

Страница 112: ...r to Figure 20 1 T Torque desired at the part A Basic lever length from center of wrench shank to center of handle or stamped on wrench or listed for that model wrench B Length of adapter extension ce...

Страница 113: ...METHOD OF INSTALLING ROD END BEARINGS Figure 20 2 Method of Installing Rod End Bearings 20 00 02 Page 20 02 December 1 1978 1E17 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 114: ...surfaces with clean water 2 Wash with mild soap and warm water or an aircraft plastic cleaner using a soft cloth or sponge and a straight rubbing motion Do not harshly rub surfaces 3 Remove oil and g...

Страница 115: ...additional solvent and allow to dry CAUTION Do not operate engine until excess solvent has evaporated or otherwise been removed 4 Remove the protective covers from the magnetos 5 Lubricate controls b...

Страница 116: ...THIS PAGE INTENTIONALLY LEFT BLANK 1E20 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 117: ...CHAPTER ENVIRONMENTAL SYSTEM 1E21...

Страница 118: ...20 21 50 10 Discharging 1F20 21 50 11 Evacuating the System 1F21 21 50 12 Charging the System 1F22 21 50 13 With a Charging Stand 1F23 21 50 14 Using the Airplane Compressor to Charge the System 1F23...

Страница 119: ...alve Installation 1G16 21 50 37 Evaporator Assembly 1G16 21 50 38 Evaporator Assembly Removal 1G16 21 50 39 Evaporator Assembly Installation 1G18 21 50 40 Pressure Relief Switch Ranco 1G18 21 50 41 El...

Страница 120: ...the exhaust air from the cabin interior The Air Conditioning System consists of a compressor with its special bracketry an evaporator a condenser a receiver dehydrator circulating fan thermal expansio...

Страница 121: ...tion service valve OK replace expansion valve Restriction in liquid line Check for kinked hoses and from condenser stopped up filter Low discharge pressure Undercharge of refrigerant Add refrigerant u...

Страница 122: ...hand If suction pressure charge does not charge replace expansion valve Restriction anywhere in Locate restriction and liquid line Restriction repair will show frost High suction pressure Capillary b...

Страница 123: ...wire to see ground wire if loose broken or dis connected Clutch coil burned out or Check current flow to disconnected clutch replace if in operative Thermostat sensing element Check thermostat and ca...

Страница 124: ...sary in receiver dehydrator or expansion valve plugged hose or coil System will not produce Electrical sufficient cooling Blower motor sluggish Remove blower motor for in operation service or replacem...

Страница 125: ...em replace bulb has lost charge expansion valve Clogged screen in receiver Purge system replace dehydrator receiver dehydrator Excessive moisture in Purge system replace system receiver dehydrator Air...

Страница 126: ...or replacement Compressor oil level low Fill with correct amount of specified oil Refrigeration Excessive charge in system Discharge excess freon until high pressure gauge drops within specifications...

Страница 127: ...Figure 21 1 Cabin Heater and Defroster PA 28RT 201 21 00 01 Page 21 08 December 1 1978 1F7 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 128: ...Figure 21 2 Cabin Heater and Defroster PA 28RT 201T 21 00 01 Page 21 09 December 1 1978 1F8 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 129: ...Figure 21 3 Overhead Vent System and Fresh Air System NOT AVAILABLE WITH AIR CONDITIONING 21 00 01 Page 21 10 December 1 1978 1F9 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 130: ...cools the air as it cycles through the evaporator The unit is operated from controls mounted on the right side of the instrument panel The air conditioning master switch has three positions FAN only O...

Страница 131: ...ER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL 1 COMPRESSOR 8 PRESSURE SWITCH 2 FREON LINES 9 RECEIVER DEHYDRATOR 3 ALTERNATOR 10 EVAPORATOR 4 PULLEY POSITIONS 11 SLOWER MOTOR 5 DUCT ASSEMBLY 12 COND...

Страница 132: ...68 14 6 10 126 70 15 8 12 129 71 17 1 14 132 72 18 3 16 134 73 19 7 18 137 74 21 20 140 75 22 4 22 144 76 23 1 23 148 77 23 8 24 152 78 24 6 25 156 79 25 3 26 160 80 26 1 27 162 81 26 8 28 165 82 27...

Страница 133: ...ry or 1 2 psi higher than the chart indicates It must be pointed out that the actual temperature of the air passing over the coils of the evaporator will be several degrees warmer allowing for a tempe...

Страница 134: ...o avoid the possibility of dirt entering the eye d Rush to a physician or hospital for immediate professional aid e DO NOT ATTEMPT TO TREAT IT YOURSELF 3 If liquid R 12 strikes the skin frostbite can...

Страница 135: ...ring joints See Chart 2104 CHART 2104 ALUMINUM TUBING TORQUE Metal Tube Thread and Fitting Alum Tubing O D Size Torque 1 4 7 16 5 7 ft lbs 3 8 5 8 11 13 ft lbs 1 2 3 4 15 20 ft lbs 5 8 7 8 21 27 ft l...

Страница 136: ...Figure 21 5 Service Valves Figure 21 6 Test Gauge and Manifold Set 21 50 04 Page 21 17 December 1 1978 1F16 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 137: ...old is a device having fittings for both gauges and connection hoses with provisions for controlling the flow of refrigerant through the manifold See Figures 21 6 and 21 7 The center port of the manif...

Страница 138: ...Figure 21 7 Manifold Set Operation 21 50 07 Page 21 19 December 1 1978 1F18 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 139: ...gauge to reach 50 psi at which time close the high side manifold valve 5 Close the refrigerant container service valve and remove the hose if no leaks are evident 6 It is advisable to use an electron...

Страница 140: ...o check the system in accordance with one of the methods outlined for any other leaks 8 If no further repair is required on the system it is now ready to evacuate in accordance with Evacuating the Sys...

Страница 141: ...tem we lower the boiling temperature of the water moisture that may be present Then we are able to pull this water in the form of vapor out of the system The following table demonstrates the effective...

Страница 142: ...p until 26 to 28 inches of vacuum is attained on the low pressure gauge then extend the operation for another 25 minutes 7 If the system cannot maintain 26 to 28 inches of vacuum close both manifold h...

Страница 143: ...be used during entire charging operation 7 Close valve 1 low pressure control fully open valve 4 refrigerant control and allow all the liquid refrigerant contained in the charging cylinder to enter h...

Страница 144: ...Figure 21 10 Charging Stand Figure 21 11 Charging Hookup 21 50 14 Page 21 25 December 1 1978 1F24 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 145: ...e and observe the pressure gauges At 1000 RPM the gauge pressure should be 15 to 20 psi on the low side and 150 to 200 on the high side NOTE Suspect leaks or an inaccurate scale if two pounds of refri...

Страница 146: ...belt Contact Sankyo International 3529 Miller Park Drive P O Box 2903 Garland Texas 75042 for special tools and instructions for detailed compressor maintenance NOTE An important factor in air condit...

Страница 147: ...COMPRESSOR INSTALLATION 1 The installation instructions for the York compressor are as follows A Place the compressor to the mounting brackets Install the six bolts and progressively torque to 14 17 f...

Страница 148: ...check A It will be necessary to discharge the system Refer to Discharging B Fabricate an oil dipstick Refer to Figure 21 14 C Remove the oil fill plug A 375 inch plug in the top side of the compressor...

Страница 149: ...the number of increments of oil The acceptable oil level in increments is 7 to 10 This represents between 2 6 and 4 4 fluid ounces H When oil is added Piper refrigerant oil PMS L2000 or equivalent 50...

Страница 150: ...2 Top Dead Center Casting Mark Sankyo Compressor Figure 21 13 Rotation of Clutch Front Plate Sankyo Compressor Oil Check 21 50 20 Page 21 31 December 1 1978 1G6 PIPER AIRCRAFT PA 28RT 201 201T MAINTEN...

Страница 151: ...r checking belt and pulley alignment A nominal dimension must be established between the forward edge of the compressor belt and the forward machined surface of the ring gear This dimension should be...

Страница 152: ...01 is very important to obtain long belt life and proper component operation Refer to Parts Catalog for belt numbers Adjust the belt tensions on PA 28RT 201 as follows A Tighten the new compressor bel...

Страница 153: ...Figure 21 15 Compressor and Alternator Belt Installation PA 28RT 201 21 50 21 Page 21 34 December 1 1978 1G9 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 154: ...ervicing the test area should be clean and free of any loose objects lying on the ramp Only the service valve located on the evaporator assembly should be used for testing C Shutdown engine and rechec...

Страница 155: ...e of the compressor 2 Secure the field assembly with four capscrews and lockwashers do not torque at this time 3 Connect the electrical lead from the field assembly NOTE The compressor shaft must be c...

Страница 156: ...rd side of the evaporator assembly housing 1 Discharge the system of all refrigerant See Discharging 2 Uncouple the refrigerant lines at the receiver dehydrator See Special Servicing Procedures B 7 3...

Страница 157: ...racket and insert the screws into the piano hinge 3 Attach the side hinges and actuating rod and rig per Condenser Assembly Rigging Instructions 4 Seal and couple the hose fittings seal with Loctite r...

Страница 158: ...Figure 21 17 Condenser Air Scoop Installation 21 50 32 Page 21 39 Revised August 17 1982 1G14 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 159: ...measured gap of 16 of an inch exists along the trailing edge of the door at the instant the forward edge of the door becomes flush with the fuselage skin 3 With the door fully closed adjust the CLOSE...

Страница 160: ...and plumbing The housing is fabricated of Cycolac type material The condensed moisture is dumped overboard through a hose clamped to a fitting on the bottom of the evaporator housing EVAPORATOR ASSEMB...

Страница 161: ...Figure 21 19 Components Installation Figure 21 20 Adjustment of Air Conditioning Throttle Switch PA 28RT 201 21 50 38 Page 21 42 December 1 1978 1G17 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 162: ...it should be replaced and sealed in the original manner to prevent exhaust gases from entering the cabin After removing and replacing the rear panel conduct a carbon monoxide test on the ground and i...

Страница 163: ...Figure 21 21 Air Conditioning Wiring Schematic 21 50 41 Page 21 44 Revised July 13 1983 1G19 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 164: ...the three speed blower REMOVAL OF BLOWER ASSEMBLY 1 Remove the access door from the aft wall of the baggage area 2 With the master switch off disconnect the plug assemblies at the blower assembly 3 Re...

Страница 165: ...blower assembly and secure it with screws washers and nuts The screws must be installed with their heads inside the duct 9 After cleaning the surfaces of all old sealant use white rubber chalk PRC 50...

Страница 166: ...in Nos Elect Company Harness Nos Ground Plug 2 Brown AC26A 2 Receptacle Low Speed Plug 1 Yellow Black 1 Receptacle Medium Speed Receptacle 2 Red White 2 Plug High Speed Receptacle 1 Orange Red 1 Plug...

Страница 167: ...THIS PAGE INTENTIONALLY LEFT BLANK 1G23 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 168: ...THIS PAGE INTENTIONALLY LEFT BLANK 1G24 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 169: ...CHAPTER AUTO FLIGHT 1H1...

Страница 170: ...N GRID SUBJECT SUBJECT NO EFFECTIVITY 22 00 00 GENERAL 1H3 A 8 82 22 10 00 NON PIPER A F C S EQUIPMENT CONTACTS 1H3 A 8 82 22 10 01 PIPER A F C S EQUIPMENT 1H4 A 8 82 22 Cont Effec Page 1 Revised Augu...

Страница 171: ...and service literature Bendix Avionics Division 2100 N W 62nd Street Fort Lauderdale Fla 33310 305 776 4100 TWX 5109559884 Collins General Aviation Division Rockwell International Cedar Rapids Iowa 52...

Страница 172: ...model name in order to consult the appropriate service manual Each manual identifies the revision level and revision status as called out on the Master Parts Price List Aerofiche published monthly by...

Страница 173: ...THIS PAGE INTENTIONALLY LEFT BLANK 1H5 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 174: ...THIS PAGE INTENTIONALLY LEFT BLANK 1H6 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 175: ...THIS PAGE INTENTIONALLY LEFT BLANK 1H7 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 176: ...CHAPTER COMMUNICATIONS 1H8...

Страница 177: ...1H10 7 81 23 10 02 Battery Removal and Installation C C C 1H10 7 81 23 10 03 Battery Removal and Installation Narco 1H11 A 7 81 23 10 03 Pilot s Remote Switch 1H13 23 10 04 Testing Emergency Locator...

Страница 178: ...itch to the OFF position 3 Disconnect the antenna coax cable twist left then pull outwards 4 Disconnect the harness to the pilot s remote switch 5 Remove the forward mounting bracket by pulling the bl...

Страница 179: ...l head section into the battery pack being careful not to pinch any wires and replace the four screws If the four holes do not line up rotate the battery pack 180 and reinsert 10 Slide the portable an...

Страница 180: ...Figure 23 1 ELT Portable Folding Antenna Narco Figure 23 2 ELT Using Fixed Aircraft Antenna Narco 23 10 03 Page 23 03 Added July 24 1981 1H12 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 181: ...ng procedures 1 Test should be no longer than three audio sweeps 2 If the antenna is removed a dummy load should be substituted during the test 3 Test should be conducted only within the time period m...

Страница 182: ...ting Emergency Locator Transmitter must be observed 1 Tune the aircraft communications receiver to 121 5 MHz and switch the receiver ON deactivate the squelch and turn the receiver volume up until a s...

Страница 183: ...the OFF position and then to the ARM position 2 If the transmitter is inadvertently activated through impact deactivate by pushing in on the OFF ARM ON switch NOTE As a routine precaution it is recom...

Страница 184: ...Figure 23 3 ELT Schematics 23 10 07 Page 23 07 Revised July 24 1981 1H16 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL NOTE AIRCRAFTG POWER USED TO SHUT OFF THE ELT WITH REMOTE SWITCH...

Страница 185: ...CHAPTER ELECTRICAL POWER 1H17...

Страница 186: ...esting of Negative Rectifiers Using C 3829 Tester 1I13 8 82 24 32 08 Testing of Rectifier Assemblies Using Test Lamp 1I13 A 8 82 24 32 09 Removal of Rectifier and Heat Sink Assembly 1I15 A 8 82 24 32...

Страница 187: ...ntion 1J9 2 79 24 35 00 Voltage Regulator Wico 1J9 24 35 01 Checking Voltage Regulator 1J9 24 36 00 OverVoltage Relay Wico 1J10 24 36 02 Checking OverVoltage Relay 1J10 24 37 00 Ammeter 1J10 24 40 00...

Страница 188: ...al and avionics equipment in case of a regulator malfunction The Overvoltage Relay and Voltage Regulator are located under the instrument panel mounted to a plate which is connected to longerons on th...

Страница 189: ...age regu lator and alternator field terminal Interruption of voltage through any of these points isolates the faulty components or wire which must be re placed See wiring schematic Chapter 91 Open out...

Страница 190: ...gneto switch to off before turning prop If resistance is high check brushes for spring tension and excessive wear and re place if necessary If brushes are okay and field reads open replace alternator...

Страница 191: ...ny of the six rectifiers pressed into the rear bell housing of the alternator open up internally it will result in a definite limitation on the current that can be drawn from the alternator After havi...

Страница 192: ...uiting of the field can occur at various positions of the rotor there fore reconnect field reset breaker pull propeller slowly by hand turning alternator rotor through 360 of travel Observe circuit br...

Страница 193: ...arity cannot occur in the airplane due to any fault in the alternator system Excessive ammeter fluctua Excessive resistance in field Check all connections and tion circuit wire terminals in field circ...

Страница 194: ...is short Overcharge due to level of Maintain electrolyte electrolyte being below top of plates Sulfation due to disuse Replace Impurities in electrolyte Replace battery Low charging rate Check voltag...

Страница 195: ...d and battery Always recharge battery for not charged immediately 1 2 hour following addition of water in freezing weather Leaking battery jar Frozen Replace Battery polarity reversed Connected backwa...

Страница 196: ...urned out Replace operate No current to sensor Check all wire segments and connections Sensor activates at a too Replace low setting Defective sensor Replace OIL warning light fails to Sensor activate...

Страница 197: ...r terminals bridged Remove material between terminals Defective sensor Replace ALT warning light fails to Bulb burned out Replace operate No current from bus to Check all wire segments and resistor co...

Страница 198: ...ed into this circuit to prevent the reverse flow of current from the battery to the alternator The circuit breaker panel contains a 5 ampere circuit breaker marked ALT FIELD If the field circuit break...

Страница 199: ...r the 60 ampere alternator This approximate 48 ampere value plus approximately two amperes for a fully charged battery will appear continuously under these flight conditions If the ammeter reading wer...

Страница 200: ...tor or circuits 4 Grounding of the alternator output terminal may damage the alternator and or circuit and components 5 Reversed battery connections may damage the rectifiers wiring or other component...

Страница 201: ...lamp to the field terminal Attach the remaining test probe to a machined surface at one of the alternator end shields The test lamp should not light Refer to Figure 24 4 2 Should the test lamp light p...

Страница 202: ...Alternator Chrysler Figure 24 3 Checking Field Coil Current Draw Figure 24 4 Testing Field Circuit 24 32 03 EFFECTIVITY Page 24 15 CHRYSLER ALTERNATOR Revised July 13 1983 1I10 PIPER AIRCRAFT PA 28RT...

Страница 203: ...tests always touch test probe to metal strap nearest rectifier TESTING OF POSITIVE RECTIFIERS USING C 3829 TESTER Refer to Figure 24 5 1 Place rectifier end shield and stator assembly on an insulated...

Страница 204: ...6 Testing Negative Rectifiers With C 3829 Tester With C 3829 Tester Figure 24 7 Rectifier End Shield and Stator Assembly 24 32 06 EFFECTIVITY Page 24 17 CHRYSLER ALTERNATOR Revised July 13 1983 1I12 P...

Страница 205: ...ield 3 Test the rectifiers with a 12 volt battery and a test lamp equipped with a No 67 bulb A Connect one side of the test lamp to the positive battery post and the other side of the lamp to a test p...

Страница 206: ...Rectifiers With Test Lamp With Test Lamp Figure 24 l0 Rectifier and Heatsink Figure 24 l l Rectifier End Shield Assembly Assembly Removal 24 32 08 EFFECTIVITY Page 24 19 CHRYSLER ALTERNATOR Revised J...

Страница 207: ...ad is grounded 4 Press one of the test probes firmly on one stator lead and press the other test probe firmly onto each of the other two stator leads one at a time The test lamp should light If the la...

Страница 208: ...4 13 Removal of Pulley Figure 24 14 Removal of Bearing Figure 24 15 Removal of Rectifier End Shield Bearing 24 32 11 EFFECTIVITY Page 24 21 CHRYSLER ALTERNATOR Revised July 13 1983 1I16 PIPER AIRCRAFT...

Страница 209: ...s and further testing or replacement may be required 3 To check for a shorted field coil connect an ohmmeter to the two slip rings If the reading is below 1 5 ohms the field coil is shorted SLIP RINGS...

Страница 210: ...tallation of Rectifier End Shield Bearing Figure 24 20 Installation of Drive End Figure 24 21 Installation of Pulley Shield Bearing 24 32 14 EFFECTIVITY Page 24 23 CHRYSLER ALTERNATOR Revised July 13...

Страница 211: ...tsink mounting stud in the end shield 7 Install the round plastic insulator flat face up in the battery stud hole in the end shield Refer to Figure 24 22 8 Install the positive heatsink assembly by pl...

Страница 212: ...lation of Positive Rectifier Assembly Figure 24 24 Installation of Capacitor Figure 24 25 Installation of Battery Output Insulator 24 32 14 EFFECTIVITY Page 24 25 CHRYSLER ALTERNATOR Revised July 13 1...

Страница 213: ...ss the stator and both end shields manually and install through bolts and washers Torque 25 to 55 inch pounds 18 Place field brushes in insulated holders and install in rectifier end shield Place an i...

Страница 214: ...ernator and regulator are designed for use on only one polarity system the following precautions must be observed when testing or servicing the electrical system Failure to observe these precautions w...

Страница 215: ...e mounted in the rectifier mounting plate while the three negative rectifiers are mounted in the slip ring end head Each pair of rectifiers is connected to a stator lead with high temperature solder T...

Страница 216: ...Slip Ring Figure 24 30 Removal of Rectifier End Bearing THIS SPACE INTENTIONALLY LEFT BLANK 24 33 03 EFFECTIVITY Page 24 29 PRESTOLITE ALTERNATOR Revised July 13 1983 1I24 PIPER AIRCRAFT PA 28RT 201...

Страница 217: ...or shaft When bearing replacement is necessary always replace the complete bearing assembly including the inner race 7 On PA 28RT 201 models to remove the drive end head from the rotor shaft use a pul...

Страница 218: ...re 24 32 Removal of End Head Bearing Figure 24 33 Testing Rotor for Ground Figure 24 34 Testing Rotor for Shorts 24 33 06 EFFECTIVITY Page 24 31 PRESTOLITE ALTERNATOR Revised July 13 1983 1J2 PIPER AI...

Страница 219: ...windings shorted windings are almost impossible to locate However shorted stator windings will usually cause the alternator to growl or be noisy during operation and will usually show some signs of ov...

Страница 220: ...f Drive End Head Figure 24 36 Installation of Rectifier Figure 24 37 Terminal Assembly Prestolite 24 33 07 EFFECTIVITY Page 24 33 PRESTOLITE ALTERNATOR Revised July 13 1983 1J4 PIPER AIRCRAFT PA 28RT...

Страница 221: ...indicate the amount of rotor resistance listed with Alternator Service Test Specifications TESTING OF ALTERNATOR 1 Wiring connections for bench testing the alternator are shown in Figure 24 39 Refer...

Страница 222: ...amperes Ground Polarity Negative Negative Rotation Bi Directional Bi Directional Rotor Current Draw 77 F 3 0 to 3 3 amps 12 0 volts 2 4 to 4 0 amps 12 0 volts Resistance 77 F 3 6 to 3 9 ohms 3 0 to 5...

Страница 223: ...e cowl It is enclosed in a stainless steel box with a vent system and a drain The vents allow fresh air to enter the box and draw off fumes that may accumulate due to the charging process of the batte...

Страница 224: ...o the positive battery terminal and secure 4 Connect the ground cable to the negative battery terminal and secure 5 Install the battery box cover and secure with wing nuts 6 Install access panel or co...

Страница 225: ...of the unit impractical and if it does not meet the specifications it must be replaced The regulator may be tested by the following procedure 1 Be sure that the battery is fully charged and in good c...

Страница 226: ...Wico CHECKING OVER VOLTAGE RELAY The relay may be tested with the use of a good quality accurate voltmeter with a scale of at least 20 volts and a suitable power supply with an output of at least 20...

Страница 227: ...IVE terminal 3 Insert the plug of jumper cable into the socket located on the aircraft fuselage 4 Turn the aircraft MASTER SWITCH ON and proceed with NORMAL engine starting technique 5 After the engin...

Страница 228: ...ch OFF remove external battery and then reconnect the battery at the negative terminal E Turn master switch ON and check ammeter for battery charging current 2 When starting with a power cart and the...

Страница 229: ...THIS PAGE INTENTIONALLY LEFT BLANK 1J13 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 230: ...THIS PAGE INTENTIONALLY LEFT BLANK 1J14 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 231: ...THIS PAGE INTENTIONALLY LEFT BLANK 1J15 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 232: ...THIS PAGE INTENTIONALLY LEFT BLANK 1J16 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 233: ...CHAPTER FLIGHT CONTROLS 1J17...

Страница 234: ...on Controls 1K11 2R 8 84 27 20 00 RUDDER CONTROLS 1K14 27 20 01 Removal of Rudder and Steering Pedal Assembly 1K14 27 20 02 Installation of Rudder and Steering Pedal Assembly 1K16 2R 8 82 27 20 03 Rem...

Страница 235: ...or Trim Assembly Aft 1L7 1R 2 79 27 35 05 Rigging and Adjustment of Stabilator Trim 1L7 1R 2 79 27 50 00 FLAPS 1L8 27 50 01 Removal of Wing Flap Controls 1L8 27 50 02 Installation of Wing Flap Control...

Страница 236: ...ontrol cable which is routed through the center of the fuselage to the main spar and out through the wings to a bellcrank in each wing A balance cable is also connected to the bellcrank As the control...

Страница 237: ...cable tension Control column horizontal Adjust chain tension chain improperly adjusted Pulleys binding or rubbing Replace binding pulleys and or provide clearance between pulleys and brackets Cables...

Страница 238: ...ull control wheel and control travel cables RUDDER CONTROL SYSTEM Lost motion between rud Cable tension too low Adjust cable tension der pedals and rudder Linkage loose or worn Check linkage and tight...

Страница 239: ...ion rudder pedal to stop before rudder neutral position or rudder trim or nose gear rods and rerig either Trim control knob moves System not lubricated Lubricate system with excessive resistance prope...

Страница 240: ...es incor Rerig stabilator cables cannot be obtained by ad rectly rigged or incorrect justing stops stop in control column Replace stop Lost motion between trim Cable tension too low Adjust cable tensi...

Страница 241: ...ctly rigged Check and or adjust rigging travel Trim drum incorrectly Check and or adjust rigging wrapped Trim indicator fails to indi Trim indicator unit not ad Adjust trim indicator cate correct trim...

Страница 242: ...CHART 2702 CABLE TENSION VS AMBIENT TEMPERATURE 27 00 02 Page 27 07 December 1 1978 1K2 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 243: ...Figure 27 1 Rod End Installation Method 27 00 02 Page 27 08 December 1 1978 1K3 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 244: ...kles may be safetied in accordance with Advisory Circular 43 13 1A Chapter 4 Section 2 9 When push rods or rod ends are provided with an inspection hole the screw must be screwed in far enough to pass...

Страница 245: ...Figure 27 2 Control Column Assembly 27 05 01 Page 27 10 December 1 1978 1K5 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 246: ...nd secure with attaching bolts washers and nuts inserted in through each side of the floor tunnel B Connect the stabilator controls to the lower end of the tee bar with bolt washer nut and cotter pin...

Страница 247: ...t and tighten AILERON CONTROLS REMOVAL OF AILERON CONTROL CABLES Refer to Figure 27 3 1 For the removal of either the control cables in the fuselage or the wings first remove the rear seat bottom on t...

Страница 248: ...Figure 27 3 Aileron Controls Typical 27 10 01 Page 27 13 December 1 1978 1K8 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 249: ...enter of the aileron D Disconnect the cable from the aft end of the aileron bellcrank by removing the cotter pin nut washer and bolt E Draw the cable from the wing INSTALLATION OF AILERON CONTROL CABL...

Страница 250: ...LCRANK ASSEMBLY Refer to Figure 27 3 1 Remove the bottom half of the rear seat of the airplane 2 Remove the access plate to the aileron bellcrank located on the underside of the wing forward of the ce...

Страница 251: ...ition of the bellcranks is the position at which the forward and aft cable connection holes are an equal distance from the adjacent outboard wing rib 2 With each bellcrank set at neutral the ailerons...

Страница 252: ...Figure 27 4 Aileron Rigging Figure 27 5 Bellcrank Rigging Tool 27 10 05 Page 27 17 Revised August 17 1982 1K12 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 253: ...rigging tool from each wing 4 Check the ailerons for correct travel from neutral per dimensions given in Figure 27 4 by the following procedure A Center the bubble of a protractor over the surface of...

Страница 254: ...attaching bolts with their washers and nuts which are through each side of the floor tunnel Pull the lower end of the tee bar aft 6 Disconnect the control cable ends from the arms on the torque tube...

Страница 255: ...Figure 27 7 Rudder and Steering Pedal Assembly 27 20 01 Page 27 20 December 1 1978 1K15 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 256: ...7 94 inches between hole centers 8 Connect the ends of the brake cylinder rods and clevis rods to the idler arms and secure with clevis and cotter pins 9 Connect the steering rods to the rudder pedal...

Страница 257: ...Figure 27 8 Rudder Controls 27 20 02 Page 27 22 Revised November 6 1979 1K17 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 258: ...Figure 27 9 Rudder Rigging Tool Figure 27 10 Clamping Rudder Pedals Figure 27 11 Rudder Rigging 27 20 02 Page 27 23 Revised August 17 1982 1K18 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 259: ...e A Remove the rudder fairing by removing its attaching screws B Disconnect the cable from the rudder sector by disconnecting the turnbuckles C Draw the cable through the fuselage INSTALLATION OF RUDD...

Страница 260: ...Step B D Should the rudder travel be incorrect showing a gap between the tool and any part of the control surfaces the rudder fairing should be removed and the stops reset to obtain correct rudder tra...

Страница 261: ...nut only finger tight and safety with cotter pin 4 Clamp the rudder pedals in neutral and position the threaded bushing in the mounting channel Turn the control shaft until the holes in the bushing a...

Страница 262: ...Figure 27 12 Rudder and Stabilator Travel Adjustments Figure 27 13 Rudder Trim Control 27 30 01 Page 27 27 Revised February 23 1979 1K22 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 263: ...crank of the stabilator by removing the cotter pin nut washer and bolt B Remove the cotter pin cable guard at the pulley located forward on lower cable See Figure 27 14 C Remove the cable from the air...

Страница 264: ...Figure 27 14 Stabilator Controls 27 30 02 Page 27 29 December 1 1978 1K24 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 265: ...Figure 27 15 Stabilator and Stabilator Trim Travel Adjustments Figure 27 16 Stabilator Rigging Tool 27 30 02 Page 27 30 Revised August 8 1984 1L1 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 266: ...the number of degree up travel as given in Figure 27 15 and place it on the rigging tool Raise the trailing edge of the stabilator and determine that when the stabilator contacts its stops the bubble...

Страница 267: ...fer to Figure 27 17 3 Loosen the cables if the trim control wheel is to be removed or disconnect if the cables are also to be removed Do this at the trim cable turnbuckles in the aft section of the fu...

Страница 268: ...ontrol wheel and looking at this side wrap the drum with three wraps of the cable in a clockwise direction B Attach the control wheel to the cable drum by aligning the long lug of the drum with the lo...

Страница 269: ...Figure 27 18 Stabilator Trim Control 27 35 02 Page 27 34 Revised February 23 1979 1L5 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 270: ...and Adjustment of Stabilator Trim Check safety of all turnbuckles 4 Install the tunnel cover on the tunnel and secure with screws 5 Install the carpet over the floor tunnel 6 Install the cover over t...

Страница 271: ...access panel to the aft section of the fuselage RIGGING AND ADJUSTMENT OF STABILATOR TRIM Refer to Figure 27 18 1 Level the airplane Refer to Leveling Chapter 8 2 Check for proper stabilator trim cab...

Страница 272: ...pin nut and clevis bolt H Remove the tube support blocks by removing the block attaching bolts I Remove the nuts washers and bolts securing the right and left cranks and stop fittings on the torque t...

Страница 273: ...Figure 27 19 Flap Controls 27 50 01 Page 27 38 Interim Revision February 27 1995 1L9 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 274: ...stop fittings H Install the tube support blocks on their support brackets and secure with bolts I Connect the flap return spring to the return chain and or at the spar housing J Connect the control c...

Страница 275: ...Figure 27 20 Flap Step Adjustment Figure 27 21 Flap Rigging Tool 27 50 02 Page 27 40 Revised August 8 1984 1L11 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 276: ...t enough to allow tube to be pulled away from its stops 7 To check up neutral position of the flaps place a flap rigging tool as shown in Figure 27 21 against the underside of the wing and flap as clo...

Страница 277: ...any work on the lift detector warning horn or light Place reference marks on holding plate and wing skin for use when reinstalling wing 1 Remove four screws holding the plate around the tab The lift...

Страница 278: ...y of the setting is to fly the airplane into a stall condition and NOTE the speed at which the stall warning comes on The stall should be made with the flaps up and power off It may be necessary to ma...

Страница 279: ...GRIDS 1L15 THRU 1L24 INTENTIONALLY LEFT BLANK 1L15 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 280: ...ARROW IV MAINTENANCE MANUAL CARD 2 OF 3 PA 28RT 201 ARROW IV PA 28RT 201T TURBO ARROW IV PIPER AIRCRAFT CORPORATION PART NUMBER 761 694 2A1 Courtesy of Bomar Flying Service www bomar biz...

Страница 281: ...he major System Chapters are then broken down into Sub System Sections These sections are identified by the second element of the standardized numbering system The number 40 of the basic number series...

Страница 282: ...inental Motors Aircraft Products Division Mobile Alabama 36601 Operators Handbook CONTINENTAL Form No X 30512 Teledyne Continental Motors Aircraft Products Division Mobile Alabama 36601 PROPELLER Over...

Страница 283: ...753 502 Altimatic III C Service Manual Piper P N 761 602 79 Vero Beach Avionics Wiring Diagrams Manual Piper P N 761 713 AEROFICHE PA 28RT 201 201T Parts Catalog Piper P N 761 693 INSPECTION PA 28 RT...

Страница 284: ...t following list of Illustrations 4 A complete list of paragraphs titles and appropriate Grid location numbers is given at the beginning of each Chapter relating to the information within that Chapter...

Страница 285: ...R 8018001 to 28R 8018106 inclusive PA 28RT 201 Arrow IV 1981 Serial Numbers 28R 8118001 to 28R 8118082 inclusive PA 28RT 201 Arrow IV 1982 Serial Numbers 28R 8218001 to 28R 8218026 inclusive PA 28RT 2...

Страница 286: ...ARKING AND MOORING 1C18 11 REQUIRED PLACARDS 1C22 12 SERVICING 1D5 20 STANDARD PRACT AIRFRAME 1E14 21 ENVIRONMENTAL SYSTEM 1E21 22 AUTOFLIGHT 1H1 23 COMMUNICATIONS 1H8 24 ELECTRICAL POWER 1H17 27 FLIG...

Страница 287: ...WS 2J19 57 WINGS 2J24 61 PROPELLER 3A18 70 STANDARD PRACTICES ENGINE 3B9 71 POWER PLANT 3B12 73 ENGINE FUEL AND CONTROL 3C12 74 IGNITION 3D7 77 ENGINE INDICATING 3F16 78 EXHAUST 3G1 79 OIL SYSTEM 3G6...

Страница 288: ...12 10 Lubrication Chart Back Up Extender 1E11 12 11 Lubrication Chart Air Conditioning Condenser 1E12 20 1 Torque Wrench Extension 1E16 20 2 Method of Installing Rod End Bearings 1E17 21 1 Cabin Heat...

Страница 289: ...ifier End Shield Assembly 1I14 24 12 Testing Stator 1I16 24 13 Removal of Pulley 1I16 24 14 Removal of Bearing 1I16 24 15 Removal of Rectifier End Shield Bearing 1I16 24 16 Testing Rotor for Ground 1I...

Страница 290: ...Rigging Tool 1L1 27 17 Methods of Securing Trim Cables 1L4 27 18 Stabilator Trim Control 1L5 27 19 Flap Controls 1L9 27 20 Flap Step Adjustment 1L11 27 21 Flap Rigging Tool 1L11 27 22 Flap Rigging 1L...

Страница 291: ...rake 2F8 32 19 Toe Brake Installation 2F9 32 20 Brake Cylinder 17000 Toe Brake 2F10 32 21 Brake Cylinder 10 30 Toe Brake 2F11 32 22 Adjustment of Nose Gear Down Limit Switch 2F15 32 23 Adjustment of M...

Страница 292: ...stallation PA 28RT 201 3C7 71 4 Engine Cowling Installation PA 28RT 201 3C11 73 1 Schematic Diagram of Fuel Injection System 3C15 73 2 Fuel Injector Nozzle Assembly 3C17 73 3 Engine Controls 3C17 73 4...

Страница 293: ...32 Assembly Tool 3E16 74 33 Using Assembly Tool 3E16 74 34 Measuring Lead Assembly Length 3E17 74 35 Cutting Metallic Braid From End of Lead 3E17 74 36 Unbraiding Metallic Shielding 3E17 74 37 Forming...

Страница 294: ...ing Stand 3K7 95 7 York Compressor and Fabricated Oil Dipstick PA 28RT 201 3K7 95 8 Fabricated Gear Back Up Extender Actuator Aligning Tool 3K8 95 9 Fabricated Stabilator Rigging Tool 3K9 95 10 Fabric...

Страница 295: ...ading Particulars Hydraulic System 2C10 2903 Characteristics Hydraulic Pump Motor 2C15 3201 Troubleshooting Landing Gear 2D10 3202 Main Gear Service Tolerances 2D20 3203 Toe In Toe Out Correction Char...

Страница 296: ...0 7704 Troubleshooting Oil Temperature Indicators 3F20 7705 Troubleshooting Exhaust Gas Temperature Gauge Alcor 3F22 7706 Troubleshooting Cylinder Head Temperature Gauge 3F22 8001 Troubleshooting Star...

Страница 297: ...CHAPTER FUEL 2A18...

Страница 298: ...mp Airborne PA 28RT 201T 2B6 28 20 10 Removal and Installation of Electric Fuel Pump 2B6 28 20 11 Auxiliary Fuel Pump System Adjustment Installed 2B7 A 8 82 28 20 12 Auxiliary Fuel Pump Operational Ch...

Страница 299: ...an individual quick drain located at the bottom inboard rear corner The fuel strainer also incorporates a quick drain which is located in the left front corner of the firewall The quick drain protrude...

Страница 300: ...plied for up to approximately 75 power Manual leaning to the correct fuel flow will be required at altitudes above 15 000 feet and for engine speeds less than 2300 RPM An absolute pressure switch auto...

Страница 301: ...to flow Fuel line blocked Flush fuel system Fuel vent cap blocked Check and clean vent hole in cap Mechanical or electrical Check and replace if fuel pump failure necessary Fuel selector valve in Rep...

Страница 302: ...e gauge Fuel selector valve in Reposition fuel selector improper position valve lever Low pressure or pressure Obstruction in inlet side Trace lines and locate surges of pump obstruction Air in line t...

Страница 303: ...Figure 28 1 Fuel System Diagram PA 28RT 201 28 00 01 Page 28 05 December 1 1978 2A24 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 304: ...Figure 28 2 Fuel System Diagram PA 28RT 201T 28 00 01 Page 28 06 December 1 1978 2B1 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 305: ...a result of the metal nozzle of the gas filler hose nicking the compound The following items are recommended 1 The entire interior of the main tanks should be inspected with the tanks drained This is...

Страница 306: ...etin 625A Fuel and Vapor Return Lines Support DISASSEMBLY OF LOCKING FUEL CAP Refer to Figure 28 4 1 Remove two screws on back of fuel cap 2 Remove screw which secures the pawl to the back of key lock...

Страница 307: ...nding on the type installed Be certain that all electrical leads are disconnected prior to removal of the cowl 3 Disconnect the fuel lines from the filter bowl housing 4 Cut the safety wire loosen the...

Страница 308: ...ion the bowl and bail wire and tighten the bail nut 6 Safety the bail nut and the bail wire assembly INSTALLATION OF FUEL FILTER BOWL AND SCREEN 1 Position the top of the filter bowl to the bracket an...

Страница 309: ...urn on the electric fuel pump and flush fuel through the system until it is determined there is no dirt and foreign matter in the fuel valve or tank During this operation agitation of the fuel within...

Страница 310: ...xternal power source 6 Check the calibrated pressure gauge At least 31 to 37 psi should be indicated 7 Connect the positive lead to the LOW power terminal of the slide resistor 8 Adjust the power supp...

Страница 311: ...brated pressure gauge The pressure on the gauge should be higher than that recorded in step c but not more than 24 5 psi 5 Switch off Master Switch and reconnect leads to the Manifold Pressure Switch...

Страница 312: ...mp should be replaced D Reassemble the plunger spring if installed and adjusting screw to the pump E Adjust the pump pressure as described in Adjustment of Electric Fuel Pump Bench Test or Adjustment...

Страница 313: ...sition the fuel pump inside the cover assembly and secure with cap screws washers and plate 2 Connect the fuel lines to the fuel pump 3 Connect the electrical leads to the pump 4 Turn the fuel selecto...

Страница 314: ...e of the tubing nut Refer to Figure 28 7 for tolerances 6 Any fittings found to be out of tolerance must be replaced Refer to Replacement of Fittings 7 After all of the unions have been checked for pr...

Страница 315: ...efully align the tube into the union and snug up the nut using a wrench C Using a wrench tighten the nut one to two flats 1 6 to 1 3 turn 4 If a repair is being made using Parker Hannifin unions and t...

Страница 316: ...ith a maximum deviation of 1 2 needle width If not within this tolerance the gauge should be replaced 4 With the master switch in the ON position and no fuel in the tanks the gauge needle should be ce...

Страница 317: ...erance Actual Fuel in Gauge Reading Plus or Minus Tank U S Gal U S Gal Needle Widths Full F 2 32 5 30 2 22 5 20 2 12 5 10 1 2 5 Zero Plus 0 Minus 1 0 Empty Empty Dot 1 2 28 40 04 Page 28 19 Revised De...

Страница 318: ...gauge fails to indicate Broken wiring Check and repair Gauge not operating Replace Fuel gauge indicates empty Incomplete ground Check ground connections when tanks are full at fuel transmitter in wing...

Страница 319: ...ion in electric pump Check bypass valve Air leak in intake lines Defective gauge Replace gauge Pressure low or pressure Obstruction in inlet side of Trace lines and locate surges pump obstruction Faul...

Страница 320: ...CHAPTER HYDRAULIC POWER 2B17...

Страница 321: ...al Check of Retractable Landing Gear System 2C21 1R 2 79 29 10 13 Nose Gear Actuating Cylinder 2C22 29 10 14 Removal of Nose Gear Actuating Cylinder 2C22 29 10 15 Disassembly of Nose Gear Actuating Cy...

Страница 322: ...gures 29 1 and 29 2 to ascertain which system is installed and is then directed on to the actuating cylinders As fluid pressure increases at one side of a cylinder piston fluid at the other side is di...

Страница 323: ...Figure 29 1 Schematic Diagram of Hydraulic System 29 00 02 Page 29 02 Revised November 6 1979 2B20 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 324: ...Figure 29 2 Schematic Diagram of Hydraulic System 29 00 02 Page 29 03 Added November 6 1979 2B21 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 325: ...Figure 29 3 Hydraulic System Installation 29 00 02 Page 29 04 Revised November 6 1979 2B22 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 326: ...Figure 29 4 Hydraulic System Installation 29 00 02 Page 29 05 Added November 6 1979 2B23 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 327: ...er must also be held in the raised position when hydraulic system operational checks are being conducted An override lock allows the emergency extension lever to be locked in the up override position...

Страница 328: ...en Safety squat switch out Readjust switch Refer to of adjustment Adjustment of Safety Switch Chapter 32 Squat switch inoperative Replace switch Pressure switch inopera Replace switch tive Pump retrac...

Страница 329: ...ad air passage Check condition of battery obstructed Pressure head hose off Reconnect hose Split or hole in diaphragm Replace unit of auxiliary extender Can be checked by using override Landing gear e...

Страница 330: ...ar selector switch Check ground ground incomplete Gear selector switch Replace switch inoperative Hydraulic pump ground Check ground incomplete Hydraulic pump inopera Replace or overhaul pump tive Hyd...

Страница 331: ...on check system to allow pressure to Isolate and determine build up and shut off pump cause before gear has retracted Shuttle valve sticking in Check cause pump base Pump stops during gear Landing gea...

Страница 332: ...n unit valve for external leakage Check gear actuating cylinders for external leakage Check for broken or damaged hydraulic lines or hoses Pump relief valve out of Replace pump adjustment Pump fails t...

Страница 333: ...y be determined by noting which down light is not lit Pump running intermit Leakage of high pressure Remove pump and replace tently after gear has re check valve check valve tracted Internal leakage o...

Страница 334: ...ils to open replace Gear free falls at airspeeds Back up extender unit Check extender unit spring above that required hydraulic valve fails to adjustment close Check hydraulic valve for sticking open...

Страница 335: ...er extender and clean out speed above actuator speed actuator hoses and head Also upon trying to over ride it is found that only with a steady pressure can the override be activated After gear does re...

Страница 336: ...ff light actuator out of adjustment mounting bracket at attach fails to operate ment slot Adjust switch until actuator is closed when emergency gear handle is in override posi tion and open when handl...

Страница 337: ...ire from the battery shelf 2 Disconnect the hydraulic lines from the pump Cap the line ends to prevent contamination 3 Remove the pump by removing the pump attaching bolts DISASSEMBLY OF HYDRAULIC PUM...

Страница 338: ...aterials are prevented from entering the system and that no parts are damaged 3 Inspect pump components for scratches scores chips cracks and wear 4 Inspect motor for worn brushes minimum 218 brush re...

Страница 339: ...Figure 29 5 Hydraulic Pump Reservoir Exploded View 29 10 05 Page 29 18 Revised November 6 1979 2C12 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 340: ...Figure 29 6 Test and Adjustment of Hydraulic Pump 29 10 05 Page 29 19 Revised November 6 1979 2C13 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 341: ...ect a 0 to 1000 psi gauge to the low pressure port port No 3 of the pump base The low pressure port No 3 is located nearest to the pipe plug installed in the base B Connect a 0 to 3000 psi gauge to th...

Страница 342: ...the electrical circuit with the positive terminal of the meter to the black lead and the negative terminal of the meter to negative terminal of the DC power supply I Connect the blue lead to the posit...

Страница 343: ...d be tagged for ease of reassembly 3 Place a shop cloth under the actuator hydraulic valve to absorb fluid and then disconnect the hydraulic lines from the elbows of the hydraulic valve Cover the line...

Страница 344: ...thus causing friction in movement 3 Connect the hydraulic lines to the elbows of the actuator hydraulic valve NOTE A special fitting with a restriction orifice of 063 of an inch is installed in the s...

Страница 345: ...Figure 29 8 Gear Back Up Extender Actuator 29 10 10 Page 29 24 Revised November 6 1979 2C18 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 346: ...he actuator with adjustment screw as follows NOTE The airspeed at which the hydraulic valve of the actuator opens was preset at the factory under ideal conditions There could be some variations at dif...

Страница 347: ...ck adjustment of electrical switch the following procedure may be used A Place the airplane on jacks Refer to Jacking Chapter 7 B Move the mixture control back to idle cutoff and the throttle to full...

Страница 348: ...aximum climb power Maintain approximately 70 KIAS for PA 28RT 201T or 65 KIAS for PA 28RT 201 for approximately 15 seconds Move the gear selector up The gear should stay down and locked Increase the a...

Страница 349: ...olt 4 Disconnect the cylinder from its attachment fitting by removing nut and bolt 5 Remove the cylinder from the wheel well DlSASSEMBLY OF NOSE GEAR ACTUATING CYLINDER Refer to Figure 29 9 1 With the...

Страница 350: ...itting in the piston rod end of the cylinder 8 Check smoothness of operation of the piston INSTALLATION OF NOSE GEAR ACTUATING CYLINDER 1 Attach the cylinder to its attachment fitting using bolt and n...

Страница 351: ...st to start out of the slot If so insert a strong wire pick or other available tool in the slot to lift up the end of the ring and then rotate gland 5 Pull the piston and end gland from the cylinder 6...

Страница 352: ...Figure 29 11 Main Gear Actuating Cylinder 29 10 22 Page 29 31 Revised August 8 1984 2D1 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 353: ...in swivel fitting is free to rotate 3 Connect the downlock spring to the swivel fitting 4 Check the adjustment of the cylinder rod end Refer to Adjustment of Main Landing Gear Chapter 32 5 Operate pum...

Страница 354: ...ed This will indicate the landing gear is down and locked 5 To check operation of gear back up extender actuator refer to Check and Adjustment of Gear Back Up Extender Actuator for Check and Adjustmen...

Страница 355: ...CHAPTER LANDING GEAR 2D4...

Страница 356: ...justment of Main Gear Door Assembly 2E5 32 20 00 NOSE GEAR 2E5 32 20 01 Disassembly of Nose Gear Oleo 2E5 32 20 02 Cleaning Inspection and Repair of Nose Gear Oleo 2E6 32 20 03 Assembly of Nose Gear O...

Страница 357: ...Brake 2F10 32 40 18 Removal of Brake Cylinder 2F10 32 40 19 Disassembly of Brake Cylinder 2F10 A 11 79 32 40 20 Cleaning Inspection and Repair of Brake Cylinder 2F12 32 40 21 Assembly of Brake Cylinde...

Страница 358: ...D WARNING cont 32 60 10 Removal of Landing Gear Up Power Reduced Warning Switch 2F18 32 60 11 Installation of Landing Gear Up Power Reduced Warning Switch 2F18 32 60 12 Adjustment of Landing Gear Up P...

Страница 359: ...of the safety switch squat switch located on the left gear and the up position of the selector lever Should the airplane be raised from the ground such as in flight far enough to move the safety swit...

Страница 360: ...other ground steering possible The two main wheels are equipped with self adjusting single disc hydraulic brake assemblies Toe brakes are standard on both the pilots and copilot s rudder pedals A park...

Страница 361: ...ugh gear has retracted switches failed Nose gear up limit switch Check gear up adjustment out of adjustment and readjust up limit switch Main gear not retracting Check gear up adjustment far enough to...

Страница 362: ...k wiring Ascertain navigation lights are off daytime Red gear unsafe light and Indicator lights circuit Reset circuit breaker and all green lights out breaker open determine cause for open circuit bre...

Страница 363: ...h Replace switch to go out with gear in transit failed or retracted Green gear down lights will Green light ground dimming Replace resistor go out and not dim when resistor open position light switch...

Страница 364: ...hment plate Steering bellcrank bearing Replace bearing and or bolt and or bolt worn Shimmy dampener galling Replace or binding Nose gear fails to straighten Steering arm roller sheared Replace defecti...

Страница 365: ...ly close completely gear Door retraction mechanism Check adjustment out of adjustment Red gear unsafe light and Gear selector handle in up Place handle in down position fail to stop when position tion...

Страница 366: ...ns Slide off the upper bearing lower bearing with O rings wiper washer and snap ring 9 To remove the orifice tube from the oleo housing remove the lock nut and washer from the top of the housing Draw...

Страница 367: ...Figure 32 1 Main Gear Oleo Strut Assembly 32 10 02 Page 32 09 Revised July 13 1983 2D16 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 368: ...Figure 32 2 Main Gear Installation 32 10 02 Page 32 10 Revised August 18 1980 2D17 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 369: ...Figure 32 2 Main Gear Installation cont 32 10 02 Page 32 11 Added August 17 1982 2D18 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 370: ...Figure 32 3 Main Gear Service Tolerances 32 10 02 Page 32 12 Revised August 17 1982 2D19 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 371: ...CHART 3202 MAIN GEAR SERVICE TOLERANCES 32 10 02 Page 32 13 Revised August 17 1982 2D20 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 372: ...CHART 3202 MAIN GEAR SERVICE TOLERANCES cont 32 10 02 Page 32 14 Revised August 17 1982 2D21 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 373: ...upper and lower torque links and then install links The torque link bolt assemblies should be lubricated and installed with the flat of the bolt head hex adjacent to the milled stop of the wide end o...

Страница 374: ...ment plates for cracks bends or misalignment C Downlock hook for excessive wear of the bearing surfaces 3 Inspect the gear downlock spring for the following A Excessive wear or corrosion expecially ar...

Страница 375: ...s freely in its support fittings and recheck thrust G Connect the brake line to its mating line in the wheel well and bleed brakes as given in Bleeding of the Brakes After A Unit Has Been Changed 3 Th...

Страница 376: ...binding of the gear assembly 9 The gear should be adjusted in the up position to allow the gear fork to press lightly into the rubber bumper pad on the wing The adjustment may be accomplished as follo...

Страница 377: ...further in or out then it will be necessary to turn the torque link assembly over This will put the link connecting point on the opposite side allowing the use of spacers to go in the same direction...

Страница 378: ...Figure 32 3a Aligning Main Gear 32 10 09 Page 32 20 Revised August 17 1982 2E3 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 379: ...r damage and corrosion 4 Repairs to a door may be replacement of hinge repair of fiberglass and painting INSTALLATION OF MAIN GEAR DOOR ASSEMBLY 1 Install the door by positioning the hinge halves of t...

Страница 380: ...r pin nut washer and bolt that connects the dampener to the oleo cylinder and housing 6 Release and remove the snap ring and washer s if installed at the top of the housing and pull the complete cylin...

Страница 381: ...washer and insert roll pin through the lock washer into the piston Install the tube lock nut finger tight at this time 6 The fork and tube assembly may be assembled by installing the tube components o...

Страница 382: ...Figure 32 4 Nose Gear Oleo Strut Assembly 32 20 03 Page 32 24 December 1 1978 2E7 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 383: ...gear oleo housing the housing may be removed by removing cotter pins nuts washers and bolts at the attachment points on each side of the housing at the engine mount 7 The steering bellcrank may be re...

Страница 384: ...Figure 32 5 Nose Gear Installation 32 20 05 Page 32 26 Interim Revision February 27 1995 2E9 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 385: ...Figure 32 5a Nose Gear Service Tolerances 32 20 05 Page 32 27 Revised August 17 1982 2E10 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 386: ...lower ID 3120 ID 3120 002 3130 3140 7 44386 03 Steering arm ID 4370 ID 4370 0015 4385 4385 8 14976 11 Bushing steering arm ID 312 ID 312 002 Press Fit 313 314 9 67054 03 Trunnion housing drag ID 4415...

Страница 387: ...my damper fitting ID 249 ID 249 003 bearing 251 252 19 20735 05 Torque link ID 312 ID 3155 0025 314 3130 20 20735 05 Torque link ID 377 ID 377 002 3785 3790 21 452 366 Bearing torque link ID 2495 ID 2...

Страница 388: ...fore and aft of the bellcrank may be made after the gear has been installed and rigged and adjusted 2 To install the gear housing assembly position the gear so that the bolt attachment points on the...

Страница 389: ...6 Carefully retract the landing gear by turning the master switch on raising the emergency gear extension lever and moving the gear selector handle to the UP position Retain the emergency extension le...

Страница 390: ...m contacts adjacent parts Place a carpenters square with the longest end along the bottom of the fuselage and the shortest end running up through the centerline of the wheel axle At this time measure...

Страница 391: ...Figure 32 6 Nose Gear Adjustment PA 28RT 201 32 20 08 Page 32 33 Revised July 13 1983 2E16 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 392: ...Figure 32 7 Nose Gear Adjustment PA 28RT 201T 32 20 08 Page 32 34 December 1 1978 2E17 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 393: ...Allow the line to pass under the wheel at the center line of the tire Snap the chalk line 8 Clamp the rudder pedals to align them in a lateral position Ascertain that the rudder pedals are in their n...

Страница 394: ...ion and not enough in the other direction check for possible damage to the gear fork or torque links REMOVAL OF NOSE GEAR DOOR ASSEMBLY Refer to Figure 32 10 or 32 11 1 The nose gear door assembly on...

Страница 395: ...Figure 32 10 Nose Gear Door Retraction Mechanism PA 28RT 201 32 20 10 Page 32 37 December 1 1978 2E20 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 396: ...Figure 32 11 Nose Gear Door Retraction Mechanism PA 28RT 201T 32 20 10 Page 32 38 December 1 1978 2E21 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 397: ...manner A The roller assembly of the retraction mechanism may be installed by first assembling the roller threaded link and roller links and then installing this assembly on its mounting bracket Ascert...

Страница 398: ...cks WHEELS AND BRAKES REMOVAL AND DISASSEMBLY OF NOSE WHEEL Refer to Figure 32 12 1 Jack the airplane enough to raise the nose wheel clear off the ground Refer to Jacking Chapter 7 2 To remove the nos...

Страница 399: ...pounds NOTE On McCauley Nose Wheel Assemblies only bushing is required to prevent tube movement 2 Position the tire and tube so the index mark on the tire is aligned with the index mark on the tube T...

Страница 400: ...tire sufficiently deflated remove the wheel through bolts Pull the wheel halves from the tire by removing the inner half from the tire first and then the outer half The brake disc may be removed at t...

Страница 401: ...the wheel to rotate freely Safety the nut with a cotter pin and install dust cover 4 Position the brake lining back plates between the wheel and brake disc and the brake cylinder on the torque plate I...

Страница 402: ...thinnest point A single groove or isolated grooves up to 0 031 of an inch deep would not necessitate replacement but a grooving of the entire surface would reduce lining life and should be replaced S...

Страница 403: ...Figure 32 15 Removal of Anchor Bolt 32 40 10 Page 32 45 December 1 1978 2F4 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 404: ...Figure 32 16 Installation of Anchor Bolt 32 40 10 Page 32 46 December 1 1978 2F5 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 405: ...on rod assembly from the cylinder 3 The piston rod assembly may be disassembled by first removing the small snap ring securing the retainer bushing spring piston seal gland and if desired the large re...

Страница 406: ...Figure 32 17 Brake System Installation 32 40 15 Page 32 48 December 1 1978 2F7 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 407: ...ing bracket and secure with bolt washers nut and cotter pin Washers should be placed on each side of the handle between the bracket and under the nut 2 Place the cylinder between the mounting bracket...

Страница 408: ...Figure 32 19 Toe Brake Installation 32 40 16 Page 32 50 December 1 1978 2F9 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 409: ...o Figure 32 20 1 Gar Kenyon cylinder number 17000 Refer to Figure 32 20 a Remove the cylinder from its mounting bracket as per Removal of Brake Cylinder b To disassemble the cylinder first remove the...

Страница 410: ...Figure 32 21 Brake Cylinder 10 30 Toe Brake INTENTIONALLY LEFT BLANK 32 40 19 Page 32 52 Added November 6 1979 2F11 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 411: ...1 Gar Kenyon cylinder number 17000 Refer to Figure 32 20 a Install new O rings on the inside and outside of the packing gland and on the outside of the piston b To assemble the piston rod assembly ins...

Страница 412: ...the brake reservoir and place a second small clear plastic hose on the bleeder fitting on one main landing gear Place the open ends of these tubes in a suitable container to collect the fluid overflo...

Страница 413: ...ak may appear at any one of the connections throughout the system or internally in the master brake cylinder or wheel brake assemblies BLEEDING OF THE BRAKES AFTER A UNIT HAS BEEN CHANGED 1 Actuate th...

Страница 414: ...emergency extension lever in the up position and turn the master switch off 3 Block the nose gear in the up position and then slowly release the emergency extension lever This will relieve hydraulic...

Страница 415: ...e switches other than check that the gear when retracting will actuate the switch within 88 of an inch of full up Switch operation turns the red gear unsafe light out ADJUSTMENT OF MAIN GEAR DOWN LIMI...

Страница 416: ...til 7 875 inches is obtained between the top of the gear fork and the bottom of the gear housing Hold the gear at this measurement 2 Adjust the switch down until it actuates at this point Secure the s...

Страница 417: ...vers aft slide the quadrant cover into position around the controls far enough to allow the cover reinforcement clip to be installed to the top underside of the cover and secure with screws 5 Install...

Страница 418: ...CHAPTER LIGHTS 2F19...

Страница 419: ...07 Replacement of Annunciator Panel Light Bulbs 2G2 A 7 81 33 10 08 Removal and Installation of Vacuum Sensor Switch 2G2 A 7 81 33 10 09 Removal and Installation of Oil Pressure Sensor Switch 2G2 A 7...

Страница 420: ...f the rudder Strobe lights can also be incorporated in the wing tips for better recognition and are incorporated with the nav lights installation To aid in taxi and landing operations in low visibilit...

Страница 421: ...panel The VAC warning light is controlled by a vacuum sensor switch located at the firewall and is attached to the vacuum regulator The sensor switch will activate when the differential pressure is be...

Страница 422: ...rrent from bus Check all wire segments connections and the re ceptacle at the left side of the annunciator panel All the warning lights fail to Test switch grounded out Check terminals and replace ext...

Страница 423: ...s to Check all wire segments and resistor connections ALT warning light fails to Blown fuse Replace 5 amp fuse near the extinguish diode heat sink No current from the fuse to Check all wire segments a...

Страница 424: ...Figure 33 1 Annunciator Panel 33 10 06 Page 33 05 Added July 24 1981 2G1 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 425: ...tained in one light bulb It is a 100 watt unit located within the nose cowl section The light is controlled by a switch to a l0 amp circuit breaker The three navigation lights are controlled by a sing...

Страница 426: ...tive lamp 5 Remove and discard the plug with the cut wires from its electrical socket INSTALLATION OF WING TIP STROBE LIGHT 1 Route the wires from the new lamp down through the hole in the navigation...

Страница 427: ...Figure 33 2 Strobe Light Connections 33 40 06 Page 33 08 December 1 1978 2G4 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 428: ...ls of approximately 50 flashes per minute The condenser is parallel across the Xenon flash tube which is designated to hold off the 450 volts DC applied until the flash tube is triggered by an externa...

Страница 429: ...checks can be made with an ohmmeter C Check for continuity between the connectors of each interconnecting cable by checking from Pin 1 to Pin l Pin 2 to Pin 2 and Pin 3 to Pin 3 When making these che...

Страница 430: ...CHAPTER NAVIGATION AND PITOT STATIC 2G7...

Страница 431: ...nted Instruments 2G11 34 00 04 Gyro Fitting Installation Procedure Edo Aire 2G11 11 79 34 10 00 FLIGHT 2G12 11 79 34 10 01 Rate of Climb Indicator 2G12 11 79 34 10 02 Sensitive Altimeter 2G13 11 79 34...

Страница 432: ...stem and has a shutoff valve which closes the port when it is not needed A placard giving instructions for use is located on the instrument panel Pitot and static lines can be drained through separate...

Страница 433: ...Figure 34 1 Pitot Static System Installation 34 00 02 Page 34 02 Revised February 23 1979 2G10 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 434: ...l air lines are clean and free of foreign particles and or residue before connecting lines to gyro DO NOT USE THREAD LUBE ON FITTINGS OR IN PORTS The use of thread lube can cause contamination shorten...

Страница 435: ...aft has assumed level flight In rough air this should not be considered a malfunction CHART 3401 TROUBLESHOOTING RATE OF CLIMB INDICATOR Trouble Cause Remedy Pointer does not set on zero Aging of diap...

Страница 436: ...system must be rechecked per F A R 23 1325 SENSITIVE ALTIMETER The altimeter indicates pressure altitude in feet above seal level The indicator has three pointers and a dial scale the long pointer is...

Страница 437: ...g knob is rotated Setting knob set screw Not tight when altimeter Tighten instrument screw loose or missing was reset if loose Replace instrument if screw is missing Cracked or loose cover Case gasket...

Страница 438: ...the diaphragm vented to the pitot air source and the case is vented to the static air system As the airplane increases speed the pitot air pressure increases causing the diaphragm to expand A mechanic...

Страница 439: ...tia the spin axis continues to point in the vertical direction providing a constant visual reference to the attitude of the airplane relative to pitch and roll axis A bar across the face of the indica...

Страница 440: ...continues to point in the same direction even though the aircraft yaws to the right or left This relative motion between the gyro and the instrument case is shown on the instrument dial which is simil...

Страница 441: ...The compass correction card is located in the card holder mounted on the instrument The compass should be swung whenever instruments or radios are changed and at least once a year ADJUSTMENT OF COMPAS...

Страница 442: ...cate magnetic inter ference ference and eliminate if possible Excessive card oscillation Insufficient liquid Replace instrument Card sluggish Weak card magnet Replace instrument Excessive pivot fricti...

Страница 443: ...raft is held in a bank and rudder is applied the indicator will come back to zero indicating no turn CHART 3407 TROUBLESHOOTING TURN AND BANK INDICATOR Trouble Cause Remedy Pointer fails to respond Fo...

Страница 444: ...CHAPTER OXYGEN SYSTEM 2G21...

Страница 445: ...ent Handling 2H10 35 10 08 Removal of Oxygen Cylinder 2H10 35 10 09 Removal of Recharge Valve 2H11 35 10 10 Installation of Recharge Valve 2H11 35 10 11 Installation of Oxygen Cylinder 2H12 35 10 12 R...

Страница 446: ...or the outlets is set up such that the main feed line for the overhead outlets is connected to the left rear passenger outlet from which the right rear and pilot outlets are connected The copilot outl...

Страница 447: ...Figure 35 1 Fixed Oxygen System 35 00 01 Page 35 02 Added November 6 1979 2G24 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 448: ...s exhausted pressure system for leaks 1 Refer to appropriate section of this chapter for effective Charge bottle and check system maintenance for leaks 2 Pressure gauge defective Replace pressure gaug...

Страница 449: ...ated to 5 psi for a significant length of time or those that do not produce an audible hissing sound when the valve is cracked should be removed and hydrostatically tested If either of these condition...

Страница 450: ...llows Refer to Figure 35 3 A Interconnect a sensitive pressure gauge of a range of 0 to 100 psi with a Scott Aviation 8570 00 plug in and connect the apparatus to the pilots outlet in the overhead pan...

Страница 451: ...Figure 35 3 Test Apparatus For Testing Oxygen System 35 10 02 Page 35 06 Added November 6 1979 2H4 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 452: ...Figure 35 4 Oxygen Tubing Installations 35 10 02 Page 35 07 Added November 6 1979 2H5 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 453: ...ausing them to come in contact with other parts of the aircraft With this in mind low pressure tubing that is supported well enough to prevent relative motion must have at least a minimum clearance of...

Страница 454: ...threads are in good condition and that the cones do not exhibit pitting or disfigurement SWAGELOC FITTING INSTALLATIONS Refer to Figure 35 5 NOTE The high pressure line fitting at the regulator shoul...

Страница 455: ...Figure 35 5 Installation of Swageloc Fittings 35 10 04 Page 35 10 Added November 6 1979 2H8 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 456: ...8 teflon tape Teflon tape should not be used on straight threads Do not use any other lubricants in place of the teflon or on any other threads 1 Wrap tape on the threads starting with those farthest...

Страница 457: ...clean plastic bags Temporarily support lines as needed to prevent damage Make sure caps and coverings are as clean as possible OXYGEN SYSTEM COMPONENT HANDLING Keeping in mind the effect of compresse...

Страница 458: ...alve is interconnected with the gauge line as well as the regulator control valve and is constantly under cylinder pressure as long as the high pressure line is attached to the regulator NOTE The reco...

Страница 459: ...alve through a tee fitting at the tank regulator control valve The high pressure line connects into the valve such that it actuates a check valve permitting pressure to the line Disconnect the high pr...

Страница 460: ...e make sure new cable shield is cut to 84 0 inches long and that the core has sufficient material to make a twin loop two inches from the end of the shield Install as follows A Rout cable through the...

Страница 461: ...rature after filling before checking against the valves in Chart 3503 B When using a recharge unit consisting of one supply cylinder slowly open the valve of the supply unit and allow the oxygen to tr...

Страница 462: ...haul service or hydrostatic tests be conducted by an FAA DOT or manufacturer Scott Aviation approved shop The following material gives recommended inspection and maintenance information for the variou...

Страница 463: ...nsion with a suitable spanner wrench 3 Torque the fittings into the outlets approximately 30 inch pounds Do not over torque as this could damage the outlet PURGING OXYGEN SYSTEM The system should be p...

Страница 464: ...CHAPTER VACUUM SYSTEM 2H17...

Страница 465: ...37 10 04 Replacing Pump Fittings 2H23 37 10 05 Installation of Vacuum Pump 2H23 37 10 06 Vacuum Regulator Valve 2H24 37 10 07 Adjustment of Vacuum Regulator Valve 2H24 7 81 37 10 08 Adjustment of Vacu...

Страница 466: ...d to assist in locating and correcting possible malfunctions in the system CHART 3701 TROUBLESHOOTING VACUUM SYSTEM Trouble Cause Remedy No vacuum gauge indica Filter clogged or dirty Clean or replace...

Страница 467: ...lace pump functioning Vacuum correct on ground Vacuum pump mal Replace pump but will not maintain pres functioning sure at altitude Regulator sticky Clean regulator Vacuum correct but pilot Regulator...

Страница 468: ...is to protect the pump from ingesting any foreign materials that could cause premature service 2 Vacuum Gauges A Vacuum gauges seldom require service and usually are replaced when malfunctions occur N...

Страница 469: ...is not suspect or has been checked against a known test gauge cruise RPM only B All modes of regulator malfunction tend to increase the vacuum power applied to the gyros Thus although excess vacuum i...

Страница 470: ...m lubricant and the AIRBORNE fittings are cadmium plated thus eliminating any need for thread lubricants If thread lubricant is required use a powdered moly sulfide or graphite in dry form or in an ev...

Страница 471: ...e engine and adjust the regulator valve by moving the valve adjustment screw clockwise to increase the pressure and counterclockwise to decrease the pressure Start the engine and repeat the check With...

Страница 472: ...INDICATING VACUUM GAUGE The suction gauge is mounted in the right side of the instrument panel This gauge is calibrated in inches of mercury and indicates the amount of vacuum created by the engine dr...

Страница 473: ...CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTI PURPOSE PARTS 2I2...

Страница 474: ...Horn Indicator and Detector 2I4 D 7 83 Removal of Lift Detector 2I4 D 7 83 Installation of Lift Detector 2I4 D 7 83 Adjustment of Lift Detector 2I4 D 7 83 39 40 01 Electrical Switches and Circuit Bre...

Страница 475: ...r panel on the lower right hand corner of the instrument panel REMOVAL OF ELECTRICAL SWITCHES 1 For a particular switch removal remove the screw above the screw below the switch on the front of the in...

Страница 476: ...THIS PAGE INTENTIONALLY LEFT BLANK 2I5 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 477: ...CHAPTER STRUCTURES 2I6...

Страница 478: ...Repairs 2I13 51 10 03 Fiberglas Fracture and Patch Repairs 2I13 51 10 04 Thermoplastic Repairs 2I14 51 10 05 Safety Walk Repair 2I21 51 10 06 Surface Preparation 2I21 51 10 07 Product Listing for Liq...

Страница 479: ...ure 51 1 identifies the type and thickness of various skin material used WARNING No access holes are permitted in any control surfaces The use of patch plates for repairs of all movable tail surfaces...

Страница 480: ...Figure 51 1 Skin Materials and Thickness 51 10 01 Page 51 02 Reissued August 1 1987 2I9 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 481: ...Figure 51 1 Skin Materials and Thickness cont 51 10 01 Page 51 03 Reissued August 1 1987 2I10 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 482: ...two 10 98 points so that the resulting lines cross the centerline of each hole g Using the intersection of the lines constructed in step f with each hole s centerline as the center scribe an arc havin...

Страница 483: ...3b Interim Revision February 27 1995 2I12 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL C L FORWARD AFT 14 99 2 50 8 48 30 TYP 2 28 R TYP 2 00 R TYP M 0 120 HOLE THRU N0 8 X 38 CRES TRUSS RECESSE...

Страница 484: ...ir to cut off air and start the cure of gel mixture 6 Allow the gel to cure 10 to 15 minutes until it feels rubbery to the touch Remove the cellophane and trim flush with the surface using a sharp raz...

Страница 485: ...e Brush catalyzed resin over hole lay mat over hole and wet out with catalyzed resin Use a daubing action with brush Then apply additional layer or layers of fiberglas cloth to build up patch to the s...

Страница 486: ...chlorethylene VM P Naptha Lighter Fluid ABS Solvent Cements Solarite 11 Series Solar Compounds Corp Linden N J 07036 Solvents Methylethylketone Obtain From Local Suppliers Methylene Chloride Acetone E...

Страница 487: ...nozzle of the gun about 1 4 of an inch away from the surface and apply heat with a circular motion until the area is sufficiently soft to remove the dirt particles C The thermoplastic will return to i...

Страница 488: ...Figure 51 3 Deep Scratches Shallow Nicks and Small Holes Figure 51 4 Mixing of Epoxy Patching Compound 51 10 04 Page 51 08 December 1 1978 2I17 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 489: ...end of the crack C If possible a double plate should be bonded to the reverse side of the crack to provide extra strength to the part D The crack should be V grooved and filled with repair material s...

Страница 490: ...Figure 51 5 Welding Repair Method Figure 51 6 Repairing of Cracks 51 10 04 Page 51 10 Revised August 17 1982 2I19 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 491: ...Figure 51 7 Various Repairs 51 10 04 Page 51 11 Revised August 17 1982 2I20 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 492: ...ittle coatings that are usually best for abrasion resistance should not be used in areas which incur high stress flexing or impact Such coating may crack thus creating a weak area SAFETY WALK REPAIR S...

Страница 493: ...Figure 51 8 Repair of Stress Lines Figure 51 9 Repair of Impacted Damage 51 10 07 Page 51 13 Revised August 17 1982 2I22 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 494: ...iquid safety walk is installed the area must be prepared as follows 1 Area must be masked off to protect painted surfaces 2 Apply suitable stripper MEK Federal Spec TT M 261 U S Rubber No 3339 to wing...

Страница 495: ...THIS PAGE INTENTIONALLY LEFT BLANK 2I24 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 496: ...CHAPTER DOORS 2J1...

Страница 497: ...08 Installation of Door Lock Assembly 2J4 52 10 09 Removal of Door Safety Latch 2J4 52 10 10 Installation of Door Safety Latch 2J4 52 10 11 Adjustment of Door Safety Latch 2J4 52 10 12 Removal and Ins...

Страница 498: ...R 1 To acquire the proper vertical adjustment of the door insert the necessary washer combination between the cabin door hinge and fuselage bracket assembly 2 Additional adjustments may be made by tap...

Страница 499: ...ut on the back of the lock assembly and tighten 3 Replace the door trim upholstery and secure with the attachment screws REMOVAL OF DOOR SAFETY LATCH 1 Remove the two handles and the five screws holdi...

Страница 500: ...ive C With the snubber removed use a clean cloth and mineral spirits to removal all excess adhesive 2 If the door jamb is flaking or excessively scuffed proceed as follows A Rub down and feather the f...

Страница 501: ...entrapped air and to insure an effective bond NOTE Do not pre stretch the snubber as this may induce cracks in the snubber D Allow the adhesive to cure at least 24 hours with the door left open It is...

Страница 502: ...Figure 52 1 Installation of Door Snubber 52 10 12 Page 52 05 Revised July 24 1981 2J7 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 503: ...e door INSTALLATION OF BAGGAGE DOOR LOCK ASSEMBLY 1 Place the lock into position for installation 2 Install the nut on the lock assembly and tighten with the use of a special wrench REMOVAL OF BAGGAGE...

Страница 504: ...THIS PAGE INTENTIONALLY LEFT BLANK 2J9 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 505: ...CHAPTER STABILIZERS 2J10...

Страница 506: ...and Installation of Stabilator Trim Tab 2J12 55 20 03 Balancing Equipment 2J12 55 20 04 Balancing Stabilator 2J12 2 79 55 30 00 VERTICAL STABILIZER 2J14 55 30 01 Removal and Installation of Vertical...

Страница 507: ...ed by placing it on the control surface to be balanced with the balance points over the control surface hinge center line and balance bar parallel to the chord line Position the trailing edge support...

Страница 508: ...Figure 55 1 Stabilator Installation 55 20 04 Page 55 02 Revised February 23 1979 2J13 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 509: ...TICAL STABILIZER REMOVAL AND INSTALLATION OF VERTICAL FIN Refer to Figure 55 3 1 Remove the fin tip and dorsal fin at the forward edge of the fin Disconnect upper tail light at the quick disconnect 2...

Страница 510: ...Figure 55 3 Vertical Fin Installation 55 30 01 Page 55 04 Revised February 23 1979 2J15 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 511: ...5 To balance the rudder the assembly must be complete including the rudder lower fairing assembly and all attaching screws and the position light wiring Place the complete assembly horizontally on kni...

Страница 512: ...Figure 55 4 Rudder Installation 55 40 03 Page 55 06 Revised July 13 1983 2J17 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 513: ...Figure 55 5 Rudder Balancing END 55 40 03 Page 55 07 Revised August 17 1982 2J18 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 514: ...CHAPTER WINDOWS 2J19...

Страница 515: ...IGHT COMPARTMENT 2J21 56 10 01 Removal of Windshield 2J21 56 10 02 Installation of Windshield 2J21 7 81 56 20 00 CABIN 2J21 56 20 01 Removal of Side Windows 2J21 7 81 56 20 02 Installation of Side Win...

Страница 516: ...ehr Manning sealant number PRC 5000 or equivalent under the edge of the moldings and trim strips 4 Place the windshield in position for installation and slide the windshield aft and up into place usin...

Страница 517: ...Figure 56 1 Windshield Installation Typical 56 20 01 Page 56 02 Revised July 24 1981 2J22 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 518: ...2 Apply Behr Manning vinyl foam tape number 560 or equivalent on both sides of the window around the outer edges 3 Apply Behr Manning Sealant number PRC 5000 or equivalent completely around the outer...

Страница 519: ...CHAPTER WINGS 2J24...

Страница 520: ...Wing Tip 2K2 57 40 00 ATTACH FITTINGS 2K6 57 40 01 Removal of Wing 2K6 2 79 57 40 02 Installation of Wing 2K7 2R 8 80 57 50 00 FLIGHT SURFACES 2K10 57 50 01 Removal of Aileron 2K10 57 50 02 Installat...

Страница 521: ...nect the position and strobe light wire assembly The ground lead may be disconnected at the point of connection on the wing rib and the positive lead may be disconnected at the wire terminal or unscre...

Страница 522: ...Figure 57 1 Wing Installation 57 20 03 Page 57 02 Revised February 23 1979 2K3 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 523: ...Figure 57 1 Wing Installation cont 57 20 03 Page 57 03 Revised August 18 1980 2K4 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 524: ...Figure 57 1 Wing Installation cont 57 20 03 Page 57 04 Revised August 18 1980 2K5 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 525: ...y and bracket 9 Disconnect the flap from the torque tube by extending the flap to its fullest degree and removing the bolt and bushing from the bearing at the aft end of the control rod 10 Disconnect...

Страница 526: ...e forward face of the wing fitting and the aft face of the fuselage fitting Refer to Figure 57 1 Sketch B Notes 1 2 and 3 8 Install the correct bolt washers and nut which attach the rear spar to the f...

Страница 527: ...Figure 57 2 Aileron and Flap Installation 57 40 02 Page 57 07 Revised February 23 1979 2K8 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 528: ...Figure 57 2 Aileron and Flap Installation cont 57 40 02 Page 57 08 December 1 1978 2K9 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 529: ...f all electrical equipment and pitot static system 21 Remove the airplane from the jacks 22 Install the cockpit trim panel assembly spar box carpet the front and back seats and wing butt rubber moldin...

Страница 530: ...ree area and in a manner which allows unrestricted movement of the aileron Place the tool on the aileron avoid rivets and keep the beam perpendicular to the hinge centerline Read the scale when the bu...

Страница 531: ...ack off the wing INSTALLATION OF WING FLAP Refer to Figure 57 2 1 Replace the wing flap by placing the flap onto its proper position and inserting the hinge bolts bushings washers and nuts 2 With the...

Страница 532: ...2K13 THRU 2L24 INTENTIONALLY LEFT BLANK 2K13 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 533: ...ARROW IV MAINTENANCE MANUAL CARD 3 OF 3 PA 28RT 201 ARROW IV PA 28RT 201T TURBO ARROW IV PIPER AIRCRAFT CORPORATION PART NUMBER 761 694 3A1 Courtesy of Bomar Flying Service www bomar biz...

Страница 534: ...he major System Chapters are then broken down into Sub System Sections These sections are identified by the second element of the standardized numbering system The number 40 of the basic number series...

Страница 535: ...inental Motors Aircraft Products Division Mobile Alabama 36601 Operators Handbook CONTINENTAL Form No X 30512 Teledyne Continental Motors Aircraft Products Division Mobile Alabama 36601 PROPELLER Over...

Страница 536: ...753 502 Altimatic III C Service Manual Piper P N 761 602 79 Vero Beach Avionics Wiring Diagrams Manual Piper P N 761 713 AEROFICHE PA 28RT 201 201T Parts Catalog Piper P N 761 693 INSPECTION PA 28 RT...

Страница 537: ...t following list of Illustrations 4 A complete list of paragraphs titles and appropriate Grid location numbers is given at the beginning of each Chapter relating to the information within that Chapter...

Страница 538: ...R 8018001 to 28R 8018106 inclusive PA 28RT 201 Arrow IV 1981 Serial Numbers 28R 8118001 to 28R 8118082 inclusive PA 28RT 201 Arrow IV 1982 Serial Numbers 28R 8218001 to 28R 8218026 inclusive PA 28RT 2...

Страница 539: ...ARKING AND MOORING 1C18 11 REQUIRED PLACARDS 1C22 12 SERVICING 1D5 20 STANDARD PRACT AIRFRAME 1E14 21 ENVIRONMENTAL SYSTEM 1E21 22 AUTOFLIGHT 1H1 23 COMMUNICATIONS 1H8 24 ELECTRICAL POWER 1H17 27 FLIG...

Страница 540: ...WS 2J19 57 WINGS 2J24 61 PROPELLER 3A18 70 STANDARD PRACTICES ENGINE 3B9 71 POWER PLANT 3B12 73 ENGINE FUEL AND CONTROL 3C12 74 IGNITION 3D7 77 ENGINE INDICATING 3F16 78 EXHAUST 3G1 79 OIL SYSTEM 3G6...

Страница 541: ...12 10 Lubrication Chart Back Up Extender 1E11 12 11 Lubrication Chart Air Conditioning Condenser 1E12 20 1 Torque Wrench Extension 1E16 20 2 Method of Installing Rod End Bearings 1E17 21 1 Cabin Heat...

Страница 542: ...eld Assembly 1I14 24 12 Testing Stator 1I16 24 13 Removal of Pulley 1I16 24 14 Removal of Bearing 1I16 24 15 Removal of Rectifier End Shield Bearing 1I16 24 16 Testing Rotor for Ground 1I17 24 17 Test...

Страница 543: ...1L1 27 17 Methods of Securing Trim Cables 1L4 27 18 Stabilator Trim Control 1L5 27 19 Flap Controls 1L9 27 20 Flap Step Adjustment 1L11 27 21 Flap Rigging Tool 1L11 27 22 Flap Rigging 1L14 28 1 Fuel S...

Страница 544: ...rake 2F8 32 19 Toe Brake Installation 2F9 32 20 Brake Cylinder 17000 Toe Brake 2F10 32 21 Brake Cylinder 10 30 Toe Brake 2F11 32 22 Adjustment of Nose Gear Down Limit Switch 2F15 32 23 Adjustment of M...

Страница 545: ...stallation PA 28RT 201 3C7 71 4 Engine Cowling Installation PA 28RT 201 3C11 73 1 Schematic Diagram of Fuel Injection System 3C15 73 2 Fuel Injector Nozzle Assembly 3C17 73 3 Engine Controls 3C17 73 4...

Страница 546: ...32 Assembly Tool 3E16 74 33 Using Assembly Tool 3E16 74 34 Measuring Lead Assembly Length 3E17 74 35 Cutting Metallic Braid From End of Lead 3E17 74 36 Unbraiding Metallic Shielding 3E17 74 37 Forming...

Страница 547: ...ing Stand 3K7 95 7 York Compressor and Fabricated Oil Dipstick PA 28RT 201 3K7 95 8 Fabricated Gear Back Up Extender Actuator Aligning Tool 3K8 95 9 Fabricated Stabilator Rigging Tool 3K9 95 10 Fabric...

Страница 548: ...ading Particulars Hydraulic System 2C10 2903 Characteristics Hydraulic Pump Motor 2C15 3201 Troubleshooting Landing Gear 2D10 3202 Main Gear Service Tolerances 2D20 3203 Toe In Toe Out Correction Char...

Страница 549: ...0 7704 Troubleshooting Oil Temperature Indicators 3F20 7705 Troubleshooting Exhaust Gas Temperature Gauge Alcor 3F22 7706 Troubleshooting Cylinder Head Temperature Gauge 3F22 8001 Troubleshooting Star...

Страница 550: ...CHAPTER PROPELLER 3A18...

Страница 551: ...G 3B1 61 20 01 Removal of Propeller Governor 3B1 61 20 02 Installation of Propeller Governor 3B1 61 20 03 Rigging and Adjustment of Propeller Governor 3B1 2 79 61 00 00 GENERAL PA 28RT 201 3B3 61 10 0...

Страница 552: ...Certified Repair Station 1 Check for oil and grease leaks 2 Clean the spinner propeller hub and blades with a non corrosive solvent 3 Inspect the hub parts for cracks 4 Steel hub parts should not be...

Страница 553: ...Figure 61 1 Propeller Installation Hartzell Effectivity 61 10 02 PA 28RT 201T Page 61 02 Revised August 17 1982 3A21 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 554: ...e mounting nuts a few threads at a time until all are tight Torque the nuts 60 to 70 foot pounds 4 Safety the propeller mounting nuts 5 Install spinner if removed and torque screws 35 to 40 inch pound...

Страница 555: ...red at 30 inch station Propeller RPM Setting Engine Static High RPM 2575 RPM Max Propeller Torque Limits Description Required Torque Dry Spinner Bulkhead Aft 20 22 foot pounds Propeller Mounting 60 70...

Страница 556: ...king small marks with a pencil at each position Then center the tip between these marks and scribe a line on the board for the full width of the tip 2 Carefully rotate propeller by hand to bring the o...

Страница 557: ...wind direction and warm in normal manner 2 To check high RPM low pitch setting move the propeller control all the way forward At this position the governor speed control arm should be against the high...

Страница 558: ...nd from the control arm loosen the cable end jam nut and rotate the end to obtain the desired level clearance Reconnect the cable end and tighten jam nut Lower cowl must be removed to accomplish this...

Страница 559: ...ler assembly with a non corrosive solvent 3 Inspect spinner and propeller hub components for cracks 4 Check all visible components for wear and safety 5 Inspect blades for nicks and cracks Refer to Fi...

Страница 560: ...Figure 61 5 Propeller Installation Hartzell Effectivity PA 28RT 201 61 10 02 Page 61 09 December 1 1978 3B4 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 561: ...Static High RPM 2700 RPM Max Propeller Torque Limits Description Required Torque Dry Propeller Mounting Nuts 60 70 foot pounds Hartzell 55 65 foot pounds McCauley Forward Bulkhead Attach ment Bolts 30...

Страница 562: ...e in blade track more than 0625 inch may be an indication of bent blades or improper propeller installation Check blade track as follows 1 With the engine shut down and blades vertical secure to the a...

Страница 563: ...l cable end to the governor control arm The ball stud is installed in the inner hole of the control arm 6 Adjust governor control per Rigging and Adjustment of Propeller Governor 7 Install engine cowl...

Страница 564: ...against the base projection to lock E Ascertain that the governor control arm is adjusted to the proper angle on the control wheel as shown in Figure 61 7 4 With the high RPM adjustment complete the...

Страница 565: ...CHAPTER STANDARD PRACTICES ENGINE 3B9...

Страница 566: ...INES TABLE OF CONTENTS EFFECTIVITY CHAPTER SECTION GRID SUBJECT SUBJECT NO EFFECTIVITY 70 00 00 STANDARD PRACTICES ENGINE 3B11 A 11 79 70 Cont Effec Page 1 Added November 6 1979 3B10 PIPER AIRCRAFT PA...

Страница 567: ...re lockwashers tablocks tabwashers or cotter pins All lockwire and cotter pins must fit snugly in holes drilled in studs and bolts for locking purposes Cotter pins should be installed so the head fits...

Страница 568: ...CHAPTER POWER PLANT 3B12...

Страница 569: ...0 MOUNTS 3B24 71 20 01 Replacement of Engine Shock Mounts 3B24 71 00 00 GENERAL PA 28RT 201 LYCOMING 3C1 8 82 71 00 01 Description 3C1 71 00 02 Troubleshooting 3C1 71 00 03 Removal of Engine 3C6 71 00...

Страница 570: ...he blades into low pitch Refer to Chapter 28 for description of fuel system and primer operation TROUBLESHOOTING Troubles peculiar to the power plant are listed in Chart 7101 along with the probable c...

Страница 571: ...to lean mixture and counter clockwise to richen mixture Fouled spark plugs Remove and clean plugs ad just gaps Replace defective plugs Discharge nozzle air vent Check for bent or loose con manifold r...

Страница 572: ...ement of linkage tion in maximum manifold control sticky linkage or by moving control from idle pressure or critical altitude dirty air cleaner to full throttle Make proper adjustments and replace wor...

Страница 573: ...con nections and check rotor assembly for possible rub bing in housing damaged rotor or defective bearings Replace turbocharger if damage is noted Exhaust system gas leakage Inspect exhaust system fo...

Страница 574: ...e Defective relief valve opera Check fuel injector pump tion in fuel injector control line from turbo charger for loose connec tions and defects Tighten connections replace dam aged line Restricted re...

Страница 575: ...ns Clean parts tighten connections and replace defective parts Leaking oil seal in turbo Check for oil in turbo charger charger exhaust outlet Re place turbocharger Defective check valve in Disassembl...

Страница 576: ...ds at the magnetos 13 Disconnect the engine vent tube at the engine 14 Disconnect the engine oil temperature lead at the aft end of the engine 15 Untie the ignition harness hoses and lines at the aft...

Страница 577: ...Figure 71 1 Engine Installation PA 28RT 201T Effectivity 71 00 03 PA 28RT 201T Page 71 08 Revised December 21 1981 3B21 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 578: ...on the mount 2 Install the lower shock mount assemblies and mounting bolts Torque the bolts 450 to 500 inch pounds 3 Route and connect the throttle and mixture control cables and adjust 4 Route and co...

Страница 579: ...cowl and then remove the upper cowl 2 Disconnect fuel drain flex line from the drain valve assembly 3 Disconnect the nose gear door rods 4 Support the bottom cowl and remove the screws that attach the...

Страница 580: ...res and cables for interference Disconnect any lines and cables if necessary 5 Check all components for wear damage or cracks and install new mounting kit 6 Lower the engine slowly and use mounting bo...

Страница 581: ...er or may be operated manually with the use of a control in the cockpit is provided in the induction system The exhaust system is constructed of stainless steel directing gases inboard to a muffler lo...

Страница 582: ...e in idle cutoff Incorrect throttle setting Open throttle to one eighth of its range Defective spark plugs Clean and adjust or replace spark plugs Defective ignition wire Check with electric tester an...

Страница 583: ...ssure Lower power and uneven Mixture too rich indicated Readjustment of fuel in running by sluggish engine opera jector by authorized person tion red exhaust flame at nel is indicated night Extreme ca...

Страница 584: ...n air scoop Examine air scoop and re move restrictions Improper fuel Drain and refill tank with recommended fuel Faulty ignition Tighten all connections Check system with tester Check ignition timing...

Страница 585: ...ve and clean oil strainers Excessive blow by Usually caused by worn or stuck rings Failing or failed bearing Examine sump for metal par ticles If found overhaul of engine is indicated Defective temper...

Страница 586: ...ct both lines from the oil cooler 12 Disconnect the magneto P leads at the magnetos 13 Disconnect the engine vent tube at the engine 14 Disconnect the engine oil temperature lead at the aft end of the...

Страница 587: ...Figure 71 3 Engine Installation PA 28RT 201 Effectivity 71 00 03 PA 28RT 201 Page 71 18 Revised December 21 1981 3C7 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 588: ...Figure 71 3 Engine Installation PA 28RT 201 cont Effectivity 71 00 03 PA 28RT 201 Page 71 19 Revised August 17 1982 3C8 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 589: ...Connect the engine vent tube 14 Connect the oil cooler 15 Connect the magneto P leads Check that magneto switch is OFF 16 Connect the fuel pump supply and vent line 17 Install the injector 18 Connect...

Страница 590: ...otching or cutting of the pin requires replacement e If it is necessary to remove the pins appropriate tools should be used to remove the fiberglas resin from around the pin and plate assembly A templ...

Страница 591: ...gine mounting bolts and the lower half of the mount assemblies 4 Carefully raise the engine just enough to remove the shock mounts Check all lines wires and cables for interference Disconnect any line...

Страница 592: ...CHAPTER ENGINE FUEL AND CONTROL 3C12...

Страница 593: ...r Nozzles 3C16 73 20 00 CONTROLLING 3C16 73 20 01 Rigging Throttle and Mixture Controls 3C16 73 20 02 Engine Setup Procedures 3C16 73 00 00 GENERAL PA 28RT 201 3C24 73 10 00 DISTRIBUTION 3C24 73 10 01...

Страница 594: ...for each cylinder FUEL INJECTION SYSTEM MAINTENANCE 1 Check all attaching parts for tightness 2 Check all fuel lines for leaks evidence of damage or chafing by metal to metal contact 3 Check control c...

Страница 595: ...Figure 73 1 Schematic Diagram of Fuel Injection System Effectivity 73 10 03 PA 28RT 201T Page 73 02 Revised August 17 1982 3C15 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 596: ...trol arm at the idle stop the quadrant throttle lever must have a minimum clearance of 032 inches from the aft stop 2 Rig the mixture control as follows A Place the mixture control lever full forward...

Страница 597: ...Figure 73 2 Fuel Injector Nozzle Assembly Figure 73 3 Engine Controls Effectivity 73 20 02 PA 28RT 201T Page 73 04 Revised August 17 1982 3C17 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 598: ...f gasoline then reconnect the line G Using the electric fuel boost pump purge the air from the fuel flow gauge line at the back of the instrument then reconnect the line 2 Exhaust Bypass Check Ascerta...

Страница 599: ...ed and Mixture Adjustment Points Figure 73 5 Sectional View of Altitude Compensating Fuel Pump Assembly Effectivity 73 20 02 PA 28RT 201T Page 73 06 December 1 1978 3C19 PIPER AIRCRAFT PA 28RT 201 201...

Страница 600: ...r cowling removed D If the engine speed increase is less than 75 RPM adjust the idle mixture adjustment to enrich the mixture counterclockwise If the engine speed increase is more than 100 RPM adjust...

Страница 601: ...turn will cause a 1 0 to 1 5 gph change Use CAUTION when loosening and tightening the jam nut so as not to change settings or over torque the jam nut NOTE If other than minor adjustments are required...

Страница 602: ...HART 7301 METERED FUEL ASSEMBLY CALIBRATION CHART 7302 LIMITS FUEL FLOW VS BRAKE H P Effectivity 73 20 02 PA 28RT 201T Page 73 09 December 1 1978 3C22 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUA...

Страница 603: ...the manifold pressure should decrease until the overboost lights go off 40 8 to 41 0 in Hg at some point between 11 500 feet minimum 12 500 feet maximum density altitude This point is known as the cri...

Страница 604: ...ed air Damaged strainer O rings should be replaced To install the screen assembly place the gasket on the screen assembly and install the assembly in the throttle body and tighten to 35 40 inch pounds...

Страница 605: ...Figure 73 7 Fuel Injector THIS SPACE INTENTIONALLY LEFT BLANK Effectivity 73 10 04 PA 28RT 201 Page 73 12 December 1 1978 3D1 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 606: ...Figure 73 8 Schematic Diagram of RSA Fuel Injection System 73 10 04 Effectivity Page 73 13 PA 28RT 201 December 1 1978 3D2 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 607: ...eed adjustment to obtain the desired idling RPM with closed throttle The above method aims at a setting that will obtain maximum RPM with minimum manifold pressure In case the setting does not remain...

Страница 608: ...Figure 73 9 Fuel Air Bleed Nozzle Figure 73 10 Adjustment of Engine Controls Effectivity PA 28RT 201 73 20 01 Page 73 15 December 1 1978 3D4 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 609: ...of cable casing attachments 4 Pull the throttle and mixture levers in the cockpit full aft to ascertain that the idle screw contacts its stop and the mixture control arm contacts its lean position A...

Страница 610: ...THIS PAGE INTENTIONALLY LEFT BLANK 3D6 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 611: ...CHAPTER IGNITION 3D7...

Страница 612: ...3D19 74 21 01 Removal of Harness 3D20 74 21 02 Maintenance of Harness 3D21 74 21 03 Installation of Harness 3E4 74 22 00 SPARK PLUGS 3E4 A 8 82 74 22 01 Removal of Spark Plugs 3E4 74 22 02 Inspection...

Страница 613: ...nance of Harness 3E18 74 21 03 Installation of Harness 3E20 74 22 00 SPARK PLUGS 3E22 A 8 82 74 22 01 Removal of Spark Plugs 3E22 74 22 02 Inspection and Cleaning of Spark Plug 3E23 74 22 03 Installat...

Страница 614: ...to start Defective spark plugs Clean and adjust or replace spark plugs Defective ignition wire Check with electric tester and replace defective wires Defective battery Replace with charged battery Imp...

Страница 615: ...the source of trouble Remove the harness outlet plate from the magneto Inspect for the presence of moisture and foreign matter on the rubber grommet and high tension outlet side of the distributor blo...

Страница 616: ...Figure 74 1 Magneto Assembly Effectivity 74 11 01 PA 28RT 201T Page 74 03 December 1 1978 3D12 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 617: ...s for felt to absorb the oil Blot off the excess with a clean cloth Too much oil may foul contact points and cause excessive burning 10 Inspect the felt washer in the distributor block for oil content...

Страница 618: ...long maximum B Hold magneto as shown in Figure 74 5 Pull heel of flyweight outward with the hooked wire and make certain that feeler gauge of 0 010 inch minimum thickness will pass between stop pin an...

Страница 619: ...74 5 Flyweight Clearance of Impulse Coupling Figure 74 6 Rotor Holding Tool Installed Figure 74 7 Timing Kit Installed Effectivity 74 11 01 PA 28RT 201T Page 74 06 December 1 1978 3D15 PIPER AIRCRAFT...

Страница 620: ...ug from the top of the magneto and turn the rotating magnet in the direction of normal rotation until the painted chamfered tooth on the distributor gear is approximately in the center of the inspecti...

Страница 621: ...Cast In Timing Marks Figure 74 9 Fabricated Pointer Figure 74 10 Engine Timing Marks Effectivity 74 11 03 PA 28RT 201T Page 74 08 Revised February 23 1979 3D17 PIPER AIRCRAFT PA 28RT 201 201T MAINTEN...

Страница 622: ...ry readjust breaker Check to be sure contacts open within E gap tolerance Replace breaker assembly if E gap tolerance and contact clearance cannot be obtained Tighten breaker screws to 20 to 25 inch p...

Страница 623: ...grommet for tears Check all the mounting brackets and clamps to see that they are secure and not cracked 2 Should a harness problem be suspected integrity of the harness wiring may be checked using a...

Страница 624: ...rrent tester such as the TAKK Model 86 or 86A or an equivalent direct current tester capable of delivering a test potential of 10 000 volts Connect ground lead of high voltage tester to outer shieldin...

Страница 625: ...bricate a tool as shown in Figure 74 12 for installing the insulating sleeves over the cable terminals 2 Push the tool through insulating sleeve and spring retainer assembly as shown in Figure 74 13 S...

Страница 626: ...d at outer surface of plate drive out tapered ferrule and remaining pieces of insulation and shielding E To determine what length the new lead assembly should be cut to proceed as follows 1 Measure th...

Страница 627: ...elets from the leads adjacent to the lead being replaced When splitting the eyelet make certain that the wire strands are not cut Removal of eyelets on adjacent leads will allow the grommet to be pull...

Страница 628: ...gure 74 16 Measuring Wire From Top of Ferrule Figure 74 17 Needle Figure 74 18 Installing Grommet Over Lead Assemblies Effectivity 74 21 02 PA 28RT 201T Page 74 16 December 1 1978 3D24 PIPER AIRCRAFT...

Страница 629: ...lead assembly through cable outlet plate until cleaned braid binds in the outlet well Position the Bendix ll 7074 Ferrule Seating Tool Figure 74 15 over the insulation and firmly seat the ferrule by t...

Страница 630: ...imping tool is not available a satisfactory connection can be made by soldering with Kester Flux 709 or equivalent and a non corrosive solder After soldering clean solder joints using denatured alcoho...

Страница 631: ...Figure 74 21 Ignition Schematic Effectivity 74 21 02 PA 28RT 201T Page 74 18 December 1 1978 3E3 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 632: ...nd connector If the lead cannot be removed easily in this manner the resisting contact between the neoprene collar and the barrel insulator will be broken by a rotary twisting of the collar Avoid undu...

Страница 633: ...ide is applied will aid in the removal of an excessively seized plug 5 Do not allow foreign objects to enter the spark plug hole INSPECTION AND CLEANING OF SPARK PLUG 1 Visually inspect each spark plu...

Страница 634: ...20 inch pounds CAUTION Make certain the deep socket is properly seated on the spark plug hexagon as damage to the plug could result if the wrench is cocked to one side when pressure is applied 2 Caref...

Страница 635: ...engine to start Defective spark plugs Clean and adjust or replace spark plugs Defective ignition wire Check with electric tester and replace defective wires Defective battery Replace with charged batt...

Страница 636: ...harness outlet plate from the magneto Inspect for the presence of moisture and foreign matter on the rubber grommet and high tension outlet side of the distributor block Check height of block contact...

Страница 637: ...l be at least 0 30 microfarads 9 Check magneto to engine timing as follows A Connect Scintilla 11 851 Timing Light or equivalent across the contact assembly B Slowly bring the engine up to number one...

Страница 638: ...gure 74 25 Timing Kit Installed Figure 74 26 Aligning Timing Marks Figure 74 27 Checking Flyweight Clearance of Impulse Coupling Effectivity 74 11 01 PA 28RT 201 Page 74 25 December 1 1978 3E10 PIPER...

Страница 639: ...Pointer Assembly of the 11 8150 Scintilla Timing Kit to breaker compartment of magneto Refer to Figure 74 25 Align pointer assembly with the 0 mark on timing plate Loosen adjusting knob of 11 8465 Ro...

Страница 640: ...gh timing hole in housing and against large distributor gear teeth Rock distributor gear back and forth slightly There must be perceptible backlash between teeth of large and small gears This check sh...

Страница 641: ...plug hole Continue rotating the crankshaft in direction of normal rotation until the advance timing mark 20 on the front face of the starter ring gear is in exact alignment with the small hole located...

Страница 642: ...on the engine Secure with washers and nuts tighten only finger tight NOTE The magnetos are held in place by clamps which allows them to be timed in several positions Since all positions will not give...

Страница 643: ...ter ON and apply 10 000 volts The insulation resistance should be 100 megohms minimum Proceed to check other leads of harness in same manner 4 Minor repair of the harness assembly such as replacement...

Страница 644: ...Figure 74 32 Assembly Tool Figure 74 33 Using Assembly Tool Effectivity 74 21 01 PA 28RT 201 Page 74 31 December 1 1978 3E16 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 645: ...Assembly Length Figure 74 35 Cutting Metallic Braid From End Figure 74 36 Unbraiding Metallic Shielding of Lead Effectivity 74 21 01 PA 28RT 201 Page 74 32 December 1 1978 3E17 PIPER AIRCRAFT PA 28RT...

Страница 646: ...ad flush with outer surface of cable outlet plate C Grip eyelet of lead with a pair of pliers and pull short length of conductor out of grommet and cable outlet plate D Using a 3 inch long 0 270 inch...

Страница 647: ...4 37 Forming Shielding Around Ferrule Figure 74 38 Ferrule Seating Tool Figure 74 39 Needle Effectivity 74 21 02 PA 28RT 201 Page 74 34 December 1 1978 3E19 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE...

Страница 648: ...f wire Refer to Figure 74 41 Slide grommet down needle until it seats tightly against the tapered ferrule N Cut wire 3 8 inch from top of grommet outlet Refer to Figure 74 42 Double wire over as shown...

Страница 649: ...ng Grommet Over Lead Ferrule Assemblies Figure 74 42 Lead Assembly Installed in Figure 74 43 Wire Doubled Over for Installation Grommet of Eyelet Effectivity 74 21 03 PA 28RT 201 Page 74 36 December 1...

Страница 650: ...with the center line of the plug barrel otherwise a side load will be applied which frequently results in damage to the barrel insulator and connector If the lead cannot be removed easily in this mann...

Страница 651: ...nel adapter with a hole at the apex just large enough to accommodate the funnel of a CO2 bottle Refer to Figure 74 44 When a seized spark plug cannot be removed by normal means the funnel adapter is p...

Страница 652: ...20 inch pounds CAUTION Make certain the deep socket is properly seated on the spark plug hexagon as damage to the plug could result if the wrench is cocked to one side when pressure is applied 2 Caref...

Страница 653: ...ation of the ignition switch as follows A Remove the P lead from the right magneto B Attach the P lead of the right magneto to an ohmmeter and to the airframe ground C With the switch in the OFF L or...

Страница 654: ...3F2 THRU 3F15 INTENTIONALLY LEFT BLANK 3F2 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 655: ...CHAPTER ENGINE INDICATING 3F16...

Страница 656: ...Engine Oil Pressure Gauge 3F20 77 20 00 TEMPERATURE 3F20 77 20 01 Oil Temperature Indicator 3F20 77 20 02 Exhaust Gas Temperature Gauge Alcor 3F21 77 20 03 Removal of EGT Probe and Gauge 3F21 77 20 04...

Страница 657: ...UBLESHOOTING MANIFOLD PRESSURE INDICATOR Trouble Cause Remedy Excessive error at existing Pointer shifted Replace instruments barometric pressure Excessive error when en Line leaking Tighten line conn...

Страница 658: ...ittent Loose cable connections Tighten cable Pointer oscillates ex Rough spot on or sharp Repair or replace cessively bend in shaft Excessive friction in Replace instrument instrument Indicator change...

Страница 659: ...eck pointer or pressure fails to build up TEMPERATURE OIL TEMPERATURE INDICATOR The oil temperature indicator is mounted in the instrument cluster on the instrument panel This instrument will provide...

Страница 660: ...ve the probe from the exhaust stack and check for a broken weld at tip end or a burnt off end The measured resistance of probe should be 8 ohms Clean the connections with steel wool before reassembly...

Страница 661: ...the instrument cluster on the instrument panel This instrument measures the cylinder head temperature using a sender located in a cylinder head The head location is determined by the engine manufactur...

Страница 662: ...THIS PAGE INTENTIONALLY LEFT BLANK 3F23 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 663: ...THIS PAGE INTENTIONALLY LEFT BLANK 3F24 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 664: ...CHAPTER EXHAUST 3G1...

Страница 665: ...ENTS EFFECTIVITY CHAPTER SECTION GRID SUBJECT SUBJECT NO EFFECTIVITY 78 00 00 GENERAL 3G3 78 00 01 Inspection of Exhaust System 3G3 78 Cont Effec Page 1 Revised December 21 1981 3G2 PIPER AIRCRAFT PA...

Страница 666: ...erform the necessary cleaning operations and inspect all external surfaces for dents cracks and missing parts Pay particular attention to welds clamps supports and support attachment lugs slip joints...

Страница 667: ...Figure 78 1 Exhaust System Inspection Points 78 00 01 Page 78 02 Revised February 23 1979 3G4 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 668: ...THIS PAGE INTENTIONALLY LEFT BLANK 3G5 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 669: ...CHAPTER OIL SYSTEM 3G6...

Страница 670: ...00 GENERAL 3G8 79 00 01 Installation of Oil Cooler 3G8 79 00 02 Engine Oil Quick Drain 3G8 79 30 00 INDICATING 3G8 79 30 01 Removal of Oil Pressure Sensor 3G8 79 30 02 Installation of Oil Pressure Se...

Страница 671: ...r distorted end cups 7 Run up engine After run up check for oil leaks ENGINE OIL QUICK DRAIN VALVE When replacing the engine oil quick drain refer to the Piper Parts Catalog for the correct replacemen...

Страница 672: ...THIS PAGE INTENTIONALLY LEFT BLANK 3G9 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 673: ...CHAPTER STARTING 3G10...

Страница 674: ...sembly of Starting Motor 3G16 80 10 05 Brushes 3G18 80 10 06 Armature 3G18 80 10 07 Field Coils 3G18 80 10 08 Brush Holders 3G18 80 10 09 Gear and Pinion H ousing 3G18 80 10 10 Bendix Drive 3G18 80 10...

Страница 675: ...ar mates with the teeth of the reduction gear that drives the bendix shaft The shaft is keyed to the reduction gear The Bendix drive is held in position on the shaft by a spiral pin The shaft is suppo...

Страница 676: ...sh boxes should be wiped clean with a gasoline undoped moist ened cloth A new brush should be run in until at least 50 percent seated however if facilities are not available for running in brushes the...

Страница 677: ...anking Worn rough or improp Disassemble clean in speed erly lubricated motor or spect and relubricate starter gearing replacing ball bearings if worn Same electrical causes as Same remedies listed for...

Страница 678: ...d water Be sure none of the solution enters the battery cells 2 The starting circuit wiring should be inspected to be sure that all connections are clean and tight and that the insulation is sound A v...

Страница 679: ...d cable from the battery post to prevent short circuiting Disconnect the lead from the starting motor terminal then take out the mounting bolts The motor can then be lifted off and taken to the bench...

Страница 680: ...rning Starting Figure 80 3 Testing Motor Armature Motor Commutator for Shorts Figure 80 4 Testing Motor Fields for Grounds 80 10 05 Page 80 06 December 1 1978 3G17 PIPER AIRCRAFT PA 28RT 201 201T MAIN...

Страница 681: ...e 4 A quick check for opens can be made by inspecting the trailing edge in direction of rotation of the commutator segments for excessive discoloration This condition indicates an open circuit FIELD C...

Страница 682: ...e out 1 1 4 to 1 1 2 times maximum Drop brushes on sandpaper covered commutator and turn the armature slowly in the direction of rotation Dust should be blown out of the motor after sanding NOTE The s...

Страница 683: ...connections for high resistance If these checks are made and found to be in good order replace frame and field assembly and retest starter STARTING MOTOR CONTROL CIRCUIT 1 Inspect the control circuit...

Страница 684: ...ing hole nearest the drive end head to the edge of the pinion STARTING THROUGH EXTERNAL POWER RECEPTACLE WITH AIRPLANE S BATTERY NEARLY DEPLETED When using a 12 volt battery for external power startin...

Страница 685: ...THIS PAGE INTENTIONALLY LEFT BLANK 3G22 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 686: ...THIS PAGE INTENTIONALLY LEFT BLANK 3G23 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 687: ...THIS PAGE INTENTIONALLY LEFT BLANK 3G24 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 688: ...CHAPTER TURBINES 3H1...

Страница 689: ...20 00 TURBOCHARGER 3H3 12 81 81 20 01 Removal of Turbocharger 3H3 81 20 02 Installation of Turbocharger 3H3 81 20 03 Adjustment of Turbocharger 3H5 7 81 81 20 04 Overboost Valve 3H5 81 20 05 Removal...

Страница 690: ...ystem from the turbine inlet and outlet C Remove safety wire securing the turbine insulation blanket and remove blanket D Remove the bolts that attach the turbocharger to the mounting bracket and remo...

Страница 691: ...Figure 81 1 Schematic Diagram of Turbocharger System 81 20 02 Page 81 02 December 1 1978 3H4 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 692: ...sconnected 9 Perform engine ground run up and check for normal engine functioning excessive exhaust manifold leakage and oil leaks Repair as necessary 10 Install the upper cowling ADJUSTMENT OF TURBOC...

Страница 693: ...THIS PAGE INTENTIONALLY LEFT BLANK 3H6 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 694: ...CHAPTER 91 CHARTS AND WIRING DIAGRAMS 3H7...

Страница 695: ...91 00 04 CONVERSION CHARTS 3H13 12 81 91 00 05 DECIMAL MILLIMETER EQUIVALENTS OF DRILL SIZES 3H19 12 81 91 00 06 TIRE BALANCER BUILDING INSTRUCTIONS D 12 81 91 00 07 SPECIAL TOOLS D 12 81 91 00 08 CO...

Страница 696: ...se the lower torque specified for the listed nut or bolt NOTE If normal operating requires movement between any of the components being clamped together tighten the nut or bolt only enough to insure i...

Страница 697: ...ascertain that the male threads are properly lubricated Torque the fittings in accordance with Chart 9101 FLARE FITTING TORQUES CHART 9101 FLARE FITTING TORQUES TORQUE INCH POUND TUBING ALUMINUM ALLO...

Страница 698: ...to FAA Manual AC 43 13 1A For thread sizes 10 through 7 16 the friction drag torque for selflocking fasteners shall be assumed to be as specified in Table II IIA and for non self locking fasteners sh...

Страница 699: ...CHART 9102 RECOMMENDED NUT TORQUES cont 91 00 03 Page 91 04 Revised December 21 1981 3H12 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 700: ...ng Inches to Millimeters A Example Convert 1 5 inches to millimeters 1 Read down inches column to 1 inches 2 Read across top inch column to 0 5 3 Read down and across to find millimeters 1 5 inches is...

Страница 701: ...CHART 9103 CONVERSION TABLES cont 91 00 04 Page 91 06 Added November 6 1979 3H14 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 702: ...CHART 9103 CONVERSION TABLES cont 91 00 04 Page 91 07 Added November 6 1979 3H15 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 703: ...CHART 9103 CONVERSION TABLES cont 91 00 04 Page 91 08 Added November 6 1979 3H16 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 704: ...THIS PAGE INTENTIONALLY LEFT BLANK 3H17 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 705: ...CHART 9103 CONVERSION TABLES cont 91 00 04 Page 91 09 Added November 6 1979 3H18 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 706: ...CIMAL MILLIMETER EQUIVALENTS OF DRILL SIZES CHART 9104 DECIMAL MILLIMETER EQUIVALENTS OF DRILL SIZES 91 00 05 Page 91 10 Revised December 21 1981 3H19 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUA...

Страница 707: ...lourocarbon Re MS 122 Purch lease Agent and Dry Lubricant Lubricating Oil Aero Lubriplate Fiske Bros Refining Co Purch MAG 1 Lubricating Grease MIL L 7711 Regal AFB2 Texaco Inc General Purpose 135 Eas...

Страница 708: ...th Street P O Box 95 New York N Y 07936 Lubricating Grease Texaco Marfak All All Purpose Purpose Grease or Mobile Mobilgrease 77 or Mobilux EP2 Grease or Shell Al vania EP Grease 2 Hydraulic Fluid MIL...

Страница 709: ...uppliers Methylene Chloride Acetone Epoxy Patching Solarite 400 Solar Compounds Corp Compound Linden N J 07036 Hot Melt Adhesives Stick Form 1 2 in dia Sears Roebuck Co or Polyamids and Hot 3 in long...

Страница 710: ...Wooster Products Inc sure Sensitive Loehr and Wyant Sts Wooster Ohio 44691 Leak Detector Solu MIL L 25567C Alpha 73 U S Gulf Corp tion For Oxygen P O Box 233 Oxygen Leak Detector Stoneybrook N Y Type...

Страница 711: ...ad Solon Ohio 44139 NOTES 1 If 100 Octane green fuel is not available use 100 octane low lead blue fuel 2 Precautions should be taken when using MIL G 23827 and MIL G 81322 since these greases contain...

Страница 712: ...ONTROL SURFACE E ENGINE INSTRUMENT F FLIGHT INSTRUMENT G LANDING GEAR H HEATER VENTILATION DEICING L LIGHTING P POWER Q FUEL OIL RP RADIO POWER RG RADIO GROUND RZ RADIO AUDIO INTERPHONE J IGNITION W W...

Страница 713: ...CHART 9107 ELECTRICAL SYMBOLS 91 00 09 Page 91 17 Revised August 17 1982 3I2 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 714: ...to 7931353 3I11 91 9 S N s 28R 8031001 to 8131005 3I12 91 10 S N s 28R 8131006 and up 3I13 Avionics Master Switching Emergency Bus 91 7 PA 28RT 201 S N s 28R 8031001 and up 3I10 91 7 PA 28RT 201T S N...

Страница 715: ...arly Models 3I20 91 23 PA 28 RT 201 201T Later Models 3I21 Turn and Bank 91 16 PA 28RT 201 201T 3I17 LANDING GEAR Landing Gear 91 22 PA 28RT 201 201T Early Models 3I20 91 23 PA 28RT 201 S N s 28R 7X37...

Страница 716: ...1 Early Models 3I23 Dimmer Instrument Lights Control 91 32 PA 28RT 201T Early Models 3I24 Dimmer Instrument Lights Control 91 33 PA 28RT 201T Later Models 3I24 Dimmer Control Assembly 91 34 PA 28RT 20...

Страница 717: ...Figure 91 1 Annunciator PA 28RT 201 Early Models 91 00 09 Page 91 18 Added August 17 1982 3I6 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 718: ...Figure 91 2 Annunciator PA 28RT 201 Later Models w Panel 91 00 09 Page 91 19 Added August 17 1982 3I7 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 719: ...Figure 91 3 Annunciator PA 28RT 201T Early Models 91 00 09 Page 91 20 Added August 17 1982 3I8 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 720: ...Figure 91 4 Annunciator PA 28RT 201T Later Models w Panel 91 00 09 Page 91 21 Added August 17 1982 3I9 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 721: ...K Figure 91 5 Cigar Lighter PA 28RT 201 201T Figure 91 6 Pitot Static PA 28R 201 and 201T Figure 91 7 Avionics Switching Emergency Bus 91 00 09 Page 91 22 Revised August 17 1982 3I10 PIPER AIRCRAFT PA...

Страница 722: ...lternator System External Power PA 28RT 201 S N s 28R 7918001 to 7918306 PA 28RT 201T S N s 28R 7931001 to 7931353 91 00 09 Page 91 23 Revised August 17 1982 3I11 PIPER AIRCRAFT PA 28RT 201 201T MAINT...

Страница 723: ...lternator System External Power PA 28RT 201 S N s 28R 8018001 to 8118005 PA 28RT 201T S N s 28R 8031001 to 813005 91 00 09 Page 91 24 Revised August 17 1982 3I12 PIPER AIRCRAFT PA 28RT 201 201T MAINTE...

Страница 724: ...10 Alternator System External Power PA 28RT 201 S N s 28R 8118006 and up PA 28RT 201T S N s 28R 8131006 and up 91 00 09 Page 91 25 Revised August 17 1982 3I13 PIPER AIRCRAFT PA 28RT 201 201T MAINTENAN...

Страница 725: ...001to8018116 PA 28RT 201T S N s 28R 7931001 to 8031188 Figure 91 12 Starter PA 28RT 201 S N s 28R 8118001 and up PA 28RT 201T S N s 28R 8131001 and up 91 00 09 Page 91 26 Added August 17 1982 3I14 PIP...

Страница 726: ...91 13 Air Conditioning PA 28RT 201 S N s 28R 7918001 to 8018116 PA 28RT 201T S N s 28R 7931001 to 8031188 91 00 09 Page 91 27 Revised August 17 1982 3I15 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE M...

Страница 727: ...igure 91 14 Air Conditioning PA 28RT 201 S N s 28R 8118001 and up PA 28RT 201T S N s 28R 8131001 and up 91 00 09 Page 91 28 Added August 17 1982 3I16 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 728: ...gure 91 16 Turn and Bank PA 28RT 201 and 201T Figure 91 17 Fuel Pump Prime Switch Diverter Valve and Manifold Pressure Switch PA 28RT 201T 91 00 09 Page 91 29 Revised August 17 1982 3I17 PIPER AIRCRAF...

Страница 729: ...lectric Clock Digital Clock and Hourmeter Installation Optional Figure 91 19 Engine Gauges and Senders PA 28RT 201 91 00 09 Page 91 30 Revised August 17 1982 3I18 PIPER AIRCRAFT PA 28RT 201 201T MAINT...

Страница 730: ...igure 91 20 Engine Gauges and Senders PA 28RT 201T Figure 91 21 Engine Gauges and Senders PA 28RT 201T 91 00 09 Page 91 31 Revised August 17 1982 3I19 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUA...

Страница 731: ...Figure 91 22 Landing Gear PA 28RT 201 201T Early Models 91 00 09 Page 91 32 Added August 17 1982 3I20 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 732: ...Figure 91 23 Landing Gear PA 28RT 201 S N s 28R 7837025 and up PA 28RT 201T S N s 28R 7803057 and up 91 00 09 Page 91 33 Revised August 17 1982 3I21 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 733: ...1 25 Anti Collision Strobe PA 28RT 201 only PA 28RT 201 and 201T Figure 91 26 Landing Light Figure 91 27 Navigation Lights PA 28RT 201 and 201T 91 00 09 Page 91 34 Revised August 17 1982 3I22 PIPER AI...

Страница 734: ...T 201 S N s 28R 8118040 and up PA 28RT 201T S N s 28R 8131042 and up Figure 91 30 Cabin Overhead Flood Lights Figure 91 31 Dimmer Switch and Radio Lights PA 28RT 201 Early Models 91 00 09 Page 91 35 R...

Страница 735: ...nstrument Lights Control PA 28RT 201T Early Models Figure 91 33 Dimmer Instrument Lights Control PA 28RT 201T Later Models 91 00 09 Page 91 36 Revised August 17 1982 3I24 PIPER AIRCRAFT PA 28RT 201 20...

Страница 736: ...Figure 91 34 Dimmer Control Assembly PA 28RT 201 201T 91 00 09 Page 91 37 Added August 17 1982 3J1 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 737: ...THIS SPACE INTENTIONALLY LEFT BLANK Figure 91 35 Stall Warning PA 28RT 201 and 201T END 91 00 09 Page 91 38 Revised August 17 1982 3J2 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 738: ...3J3 THRU 3J24 INTENTIONALLY LEFT BLANK 3J3 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 739: ...CHAPTER 95 SPECIAL PURPOSE EQUIPMENT 3K1...

Страница 740: ...SECTION GRID SUBJECT SUBJECT NO EFFECTIVITY 95 00 00 GENERAL 3K3 A 12 81 95 10 00 TOOLS AND TEST EQUIPMENT 3K3 A 12 81 95 10 01 Tire Balancer Building Instructions 3K4 A 12 81 95 Cont Effec Page 1 Rev...

Страница 741: ...ft An illustrated list of tools required follows NOTE Tools with Part Numbers given are available through the Piper Service Department Specifications for fabricated tools may be found by referring to...

Страница 742: ...um tubing The two lengths of spacers are suitable for balancing most any aircraft wheel 4 The 7 bushings may be made from one inch phenolic or aluminum using a 1 1 2 inch hole saw to cut out the small...

Страница 743: ...Figure 95 2 Control Surface Balancing Tool 95 10 01 Page 95 03 Added December 21 1981 3K5 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 744: ...arness Ferrule Figure 95 4 Needle Seating Tool Figure 95 5 Assembly Tool For Ignition Harness Insulating Sleeve Installation 95 10 01 Page 95 04 Added December 21 1981 3K6 PIPER AIRCRAFT PA 28RT 201 2...

Страница 745: ...Figure 95 6 Charging Stand Figure 95 7 York Compressor and Fabricated Oil Dipstick PA 28RT 201 95 10 01 Page 95 05 Added December 21 1981 3K7 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 746: ...Figure 95 8 Fabricated Gear Back Up Extender Actuator Aligning Tool 95 10 01 Page 95 06 Added December 21 1981 3K8 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 747: ...Figure 95 9 Fabricated Stabilator Rigging Tool 95 10 01 Page 95 07 Added December 21 1981 3K9 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 748: ...Figure 95 l0 Fabricated Aileron and Flap Rigging Tool 95 10 01 Page 95 08 Revised August 8 1984 3K10 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 749: ...Figure 95 11 Fabricated Aileron Bellcrank Rigging Tool Figure 95 12 Fabricated Rudder Rigging Tool 95 10 01 Page 95 09 Added December 21 1981 3K11 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 750: ...Figure 95 13 Fabricated Tool for Baggage Door Lock Figure 95 14 Retainer Ring Tool 95 10 01 Page 95 10 Added December 21 1981 3K12 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 751: ...Figure 95 15 Orifice Replacement Tool 95 10 01 Page 95 11 Added December 21 1981 3K13 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

Страница 752: ...3K14 THRU 3L24 INTENTIONALLY LEFT BLANK 3K14 PIPER AIRCRAFT PA 28RT 201 201T MAINTENANCE MANUAL...

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