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SCHEDULED SERVICING.

LANDING GEAR.

The landing gear consists of tires, brakes and oleo strut assemblies. These should be inspected for proper

gear extension, scored piston tubes, possible hydraulic fluid leakage and security and condition of all
connection points. Check the brake linings for wear and frayed edges, and brake discs for scoring. Replace if
found necessary. Checked for proper adjustment of downlock hooks, looseness of drag links and side brace
links. Minor servicing is described in the following paragraphs, and for detailed service and overhaul
instructions refer to Chapter 32.

OLEO STRUTS.

The air-oil type oleo strut should be maintained at proper strut tube exposures for best oleo action. The

nose gear strut must have approximately 2.75 inches of piston tube exposed, while the main gear strut requires
approximately 2.0 inches of tube exposure. These measurements are taken with the airplane sitting on level
surface under normal static load. (Empty weight of airplane plus full fuel and oil.) If the strut has less tube
exposure than prescribed, 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
or two cycles after the rocking force is removed, the oleo strut requires inflating. Check the valve core and
filler plug for air leaks, correct if required, and add air as described in Inflating Oleo Struts. If the oleo strut
oscillates with long strokes (approximately three inches) and the airplane continues to oscillate after the
rocking force is removed, the oleo struts require fluid. Check the oleo for indications of oil leaks, correct if
required and add fluid as described in Filling Oleo Struts. For repair procedures of the landing gear and/or oleo
struts, refer to Chapter 32.

—WARNING—

Do not release air by removing the strut valve core or filler plug.
Depress the valve core pin until strut chamber pressure has
diminished.

—CAUTION—

Dirt and foreign particles form around the filler plugs of the
landing gear struts, therefore, before attempting to remove these
plugs, the tops of the struts should be cleaned with compressed
air and/or with a dry solvent.

12-20-03

Page 12-07

December 1, 1978

1D14

PIPER AIRCRAFT

PA-28RT-201 / 201T

*MAINTENANCE MANUAL

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Summary of Contents for Arrow IV

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

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

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

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

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

Page 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...

Page 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...

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

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

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

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

Page 77: ...CHAPTER SERVICING 1D5...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

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

Page 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...

Page 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...

Page 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...

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

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

Page 176: ...CHAPTER COMMUNICATIONS 1H8...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 297: ...CHAPTER FUEL 2A18...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 418: ...CHAPTER LIGHTS 2F19...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

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

Page 477: ...CHAPTER STRUCTURES 2I6...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 496: ...CHAPTER DOORS 2J1...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 505: ...CHAPTER STABILIZERS 2J10...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 514: ...CHAPTER WINDOWS 2J19...

Page 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...

Page 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...

Page 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...

Page 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...

Page 519: ...CHAPTER WINGS 2J24...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 550: ...CHAPTER PROPELLER 3A18...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 611: ...CHAPTER IGNITION 3D7...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

Page 664: ...CHAPTER EXHAUST 3G1...

Page 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...

Page 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...

Page 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...

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

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

Page 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...

Page 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...

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

Page 673: ...CHAPTER STARTING 3G10...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

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

Page 688: ...CHAPTER TURBINES 3H1...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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