ADJUSTMENT OF NOSE GEAR DOORS.
1. Adjust PA-28RT-201 nose gear doors as follows:
A. Place the airplane on jacks. (Refer to Jacking, Chapter 7.)
B. Adjust the door retraction rods so that the gear will swing through the door opening with a .12 ±
.06 of an inch clearance between the gear and door at their closest point. This can best be done
with the nose gear down, tension springs disconnected and operating the nose gear manually.
C. With door clearance adjusted, adjust the link between the roller assembly and bellcrank assembly
so that the doors will pull up tightly when gear is full up. Over-tightening may result in door
buckling, however, if the link is too loose, doors will gap in flight.
D. Check all rod ends for adequate thread engagement, for safety and tightness of jam nuts.
E. Remove the airplane from jacks.
2. Adjust PA-28RT-201T nose gear doors as follows:
A. Place the airplane on jacks. (Refer to Jacking, Chapter 7.)
B. Gear up stop must be properly adjusted per Adjustment of Nose Landing Gear (PA-28RT-201T)
before rigging doors.
C. Adjust the door actuator rods to fully close doors in the gear up position.
D. Check all rod ends for adequate thread engagement, for safety and tightness of jam nuts.
E. Remove the airplane from jacks.
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 nose wheel, first remove the cotter pin and washer that secures the safety clevis pin of
the wheel nut. Next remove the clevis pin, wheel nut and then slide the wheel from the axle.
3. The wheel halves may be separated by first deflating the tire. With the tire sufficiently deflated,
remove the wheel through bolts. Pull the wheel halves from the tire by removing the wheel half opposite the
valve stem first and then the other half.
4. The wheel bearing assemblies may be removed from each wheel half by first removing the snap rings
that secure the grease seal retainers, and then the retainers, grease seals and bearing cones. The bearing cups
should be removed by tapping out evenly from the inside.
INSPECTION OF NOSE WHEEL ASSEMBLY.
1. Visually check all parts for cracks, distortion, defects and excess wear.
2. Check tie bolts for looseness or failure.
3. Check internal diameter of felt grease seals. Replace the felt grease seal if surface is hard or gritty.
4. Check tire for cuts, internal bruises and deterioration.
5. Check bearing cones and cups for wear and pitting and re-lubricate.
6. Replace any wheel casting having visible cracks.
32-40-02
Page 32-40
December 1, 1978
2E23
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
Summary of Contents for Arrow IV
Page 18: ...CHAPTER AIRWORTHINESS LIMITATIONS 1A18...
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Page 22: ...CHAPTER TIME LIMITS MAINT CHECKS 1A22...
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Page 40: ...CHAPTER DIMENSIONS AND AREAS 1B16...
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Page 53: ...CHAPTER LIFTING AND SHORING 1C5...
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Page 57: ...CHAPTER LEVELING AND WEIGHING 1C9...
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Page 62: ...CHAPTER TOWING AND TAXIING 1C14...
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Page 66: ...CHAPTER PARKING AND MOORING 1C18...
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Page 70: ...CHAPTER REQUIRED PLACARDS 1C22...
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Page 77: ...CHAPTER SERVICING 1D5...
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Page 110: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E14...
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Page 117: ...CHAPTER ENVIRONMENTAL SYSTEM 1E21...
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Page 169: ...CHAPTER AUTO FLIGHT 1H1...
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Page 176: ...CHAPTER COMMUNICATIONS 1H8...
Page 185: ...CHAPTER ELECTRICAL POWER 1H17...
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Page 233: ...CHAPTER FLIGHT CONTROLS 1J17...
Page 297: ...CHAPTER FUEL 2A18...
Page 320: ...CHAPTER HYDRAULIC POWER 2B17...
Page 355: ...CHAPTER LANDING GEAR 2D4...
Page 418: ...CHAPTER LIGHTS 2F19...
Page 430: ...CHAPTER NAVIGATION AND PITOT STATIC 2G7...
Page 444: ...CHAPTER OXYGEN SYSTEM 2G21...
Page 464: ...CHAPTER VACUUM SYSTEM 2H17...
Page 473: ...CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTI PURPOSE PARTS 2I2...
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Page 477: ...CHAPTER STRUCTURES 2I6...
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Page 496: ...CHAPTER DOORS 2J1...
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Page 505: ...CHAPTER STABILIZERS 2J10...
Page 514: ...CHAPTER WINDOWS 2J19...
Page 519: ...CHAPTER WINGS 2J24...
Page 550: ...CHAPTER PROPELLER 3A18...
Page 565: ...CHAPTER STANDARD PRACTICES ENGINE 3B9...
Page 568: ...CHAPTER POWER PLANT 3B12...
Page 592: ...CHAPTER ENGINE FUEL AND CONTROL 3C12...
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Page 611: ...CHAPTER IGNITION 3D7...
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Page 655: ...CHAPTER ENGINE INDICATING 3F16...
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Page 664: ...CHAPTER EXHAUST 3G1...
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Page 669: ...CHAPTER OIL SYSTEM 3G6...
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Page 673: ...CHAPTER STARTING 3G10...
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Page 688: ...CHAPTER TURBINES 3H1...
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Page 694: ...CHAPTER 91 CHARTS AND WIRING DIAGRAMS 3H7...
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