4. Extend the landing gear and connect both doors.
5. Retract the landing gear fully and ascertain the doors close properly and do not bind.
WHEELS AND BRAKES.
NOSE WHEEL.
REMOVAL AND DISASSEMBLY OF NOSE WHEEL. (Refer to Figure 32-13.
1. Jack the airplane enough to raise the nose wheel clear of the ground. (Refer to Chapter 7.)
2. Remove wheel by the following procedure:
A.
Remove the nut and washer from one end of the axle rod and slide out the rod and axle plugs.
B.
Lightly tap the axle tube out from the center of the wheel assembly by use of an object of near equal
diameter.
— Note —
Be certain not to damage the axle tube end in any way. This will make removal and
installation extremely difficult.
C.
Remove the spacer tubes and the wheel assembly.
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
secures the grease seal retainers and then the retainers, grease seals and bearing cones. The bearing cups
should be removed only for replacement, by tappipng out evenly from the inside.
INSPECTION OF NOSE WHEEL.
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 for distortion or wear. Replace the felt grease seal if surface is
hard or gritty. Lightly coat felt grease seals with SAE 10 oil. (Do not soak felts in oil.)
4. Check tire for cuts, internal bruises and deterioration.
5. Check bearing cones and cups for wear and pitting and relubricate.
6. Replace any wheel casting having visible cracks.
ASSEMBLY AND INSTALLATION OF NOSE WHEEL. (Refer to Figure 32-13.)
1. Ascertain that the bearing cup for each wheel half is properly installed. Install the tire with tube on the
wheel half with the valve stem hole and then join the two wheel halves. Install the through bolts with the
washers and nuts to the valve stem side.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
3 2 - 4 1 - 0 3
Page 32-39
Revised: May 15, 1989
2H7
PIPER AIRCRAFT
Summary of Contents for SEMINOLE PA-44-180
Page 38: ...CHAPTER DIMENSIONS AND AREAS 1B14...
Page 49: ...CHAPTER LIFTING AND SHORING 1C1...
Page 53: ...CHAPTER LEVELING AND WEIGHING 1C5...
Page 58: ...CHAPTER TOWING AND TAXIING 1C10...
Page 62: ...CHAPTER PARKING AND MOORING 1C14...
Page 65: ...CHAPTER REQUIRED PLACARDS 1C17...
Page 70: ...CHAPTER SERVICING 1C22...
Page 98: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E2...
Page 108: ...CHAPTER ENVIRONMENTAL SYSTEM 1E12...
Page 189: ...CHAPTER AUTOFLIGHT 1H21...
Page 192: ...CHAPTER COMMUNICATIONS 1H24...
Page 202: ...CHAPTER ELECTRICAL POWER 1I10...
Page 228: ...CHAPTER EQUIPMENT FURNISHINGS 1J12...
Page 233: ...CHAPTER FIRE PROTECTION 1J17...
Page 238: ...CHAPTER FLIGHT CONTROLS 1J24...
Page 304: ...2A18 CHAPTER FUEL...
Page 325: ...2B17 CHAPTER HYDRAULIC POWER...
Page 357: ...2D1 CHAPTER ICE AND RAIN PROTECTION...
Page 414: ...CHAPTER LANDING GEAR 2F13...
Page 479: ...2I6 CHAPTER LIGHTS...
Page 488: ...2I16 CHAPTER NAVIGATION AND PITOT STATIC...
Page 503: ...2J7 CHAPTER OXYGEN...
Page 524: ...2K6 CHAPTER VACUUM...
Page 535: ...2K19 CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTIPURPOSE PARTS...
Page 546: ...INTENTIONALLY LEFT BLANK PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 2L6 PIPER AIRCRAFT...
Page 547: ...2L7 CHAPTER STRUCTURES...
Page 582: ...CHAPTER DOORS 3A18...
Page 593: ...CHAPTER STABILIZERS 3B8...
Page 604: ...CHAPTER WINDOWS 3B22...
Page 611: ...CHAPTER WINGS 3C10...
Page 624: ...CHAPTER PROPELLER 3D1...
Page 643: ...CHAPTER POWER PLANT 3D21...
Page 667: ...CHAPTER ENGINE FUEL SYSTEM 3F1...
Page 681: ...CHAPTER IGNITION 3F16...
Page 712: ...CHAPTER ENGINE INDICATING 3H1...
Page 730: ...CHAPTER EXHAUST 3H19...
Page 734: ...CHAPTER OIL 3I1...
Page 743: ...CHAPTER STARTING 3I11...
Page 755: ...CHAPTER TURBINES 3J1...