NOSE GEAR.
NOSE GEAR OLEO.
DISASSEMBLY OF NOSE GEAR OLEO. (Refer to Figure 32-5.)
The nose gear oleo assembly may be removed and disassembled from the gear oleo housing with the gear
removed from or installed on the airplane.
1. Place the airplane on jacks. (Refer to Chapter 7.)
2. Place a drip pan under the nose gear to catch spillage.
3. Remove air and fluid from the oleo strut. Depress the air valve core pin until strut chamber pressure has
diminished, remove the filler plug and with a small hose siphon as much hydraulic fluid from the strut as
possible.
4. To remove the complete cylinder and fork assembly from the oleo housing, cut safety wire at the top of the
unit and remove cap bolts that attach steering arm and aligner guide bracket to the top of the oleo cylinder.
5. Disconnect the shimmy dampener by removing each cotter pin, nut, washer and bolt that connects the
dampner 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
cylinder and fork assembly from the bottom of the housing. The upper and lower housing bushings should
remain pressed in the housing.
7. To remove the piston tube and fork from the cylinder, first separate the upper and lower torque links by
removing the link connecting bolt assembly and then separate the two links. Note spacer washer between
the two links.
8. Compress the piston tube, reach up along the tube and release the snap ring from the annular slot at the
bottom of the oleo housing.
9. Pull the piston tube with components parts from the cylinder.
10. The piston tube components may be removed by reaching in the tube and pushing out the upper bearing
retainer pins. Slide from the tube, the upper bearing, lower bearing with outer and inner “O” rings, wiper
strip, washer and snap ring.
11. To remove the orifice tube, remove the large lock nut and lock washer from the top of the cylinder. Pull the
tube from the cylinder.
12. The orifice plate is removed from the bottom of the orifice tube by releasing the snap ring that holds the
parts in position.
13. To remove the piston tube plug with“O” ring, located in the lower end of the tube, remove the bolt assembly
and insert a rod up through the hole in the body of the fork. Push the plug out through the top of the tube.
CLEANING, INSPECTION AND REPAIR OF NOSE GEAR OLEO.
1. Clean all parts with a suitable dry type cleaning solvent.
2. Inspect the landing gear oleo assembly component for the following:
A.
Bearings and bushings for excess wear, corrosion, scratches and overall damage.
B.
Retaining pins for wear and damage.
C.
Lock rings for cracks, burrs, etc.
D.
Cylinder and orifice tube for corrosion, scratches, nicks and excess wear.
E.
Upper and lower cylinder bushings loose or turning in cylinder.
F.
Orifice plate for hole restriction.
G.
Fork tube for corrosion, scratches, nicks, dents and misalignment.
H.
Air valve general condition.
3. Repair of the oleo is limited to smoothing out minor scratches, nicks and dents and replacement of parts.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
3 2 - 2 1 - 0 2
Page 32-22
Revised: May 15, 1989
2G14
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...