— WARNING —
DO NOT RELEASE AIR BY REMOVING THE STRUT VA LVE CORE OR
FILLER PLUG. DEPRESS THE VA LVE CORE PIN UNTIL THE STRUT
CHAMBER PRESSURE HAS DIMINISHED.
— CAUTION —
CLEAN ALL DIRT AND FOREIGN PA RTICLES FROM AROUND THE
FILLER PLUGS WITH COMPRESSED AIR AND/OR WITH A QUICK
DRYING SOLVENT.
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. 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. For repair
procedures of the landing gear and/ or oleo struts, refer to Chapter 32 of this manual.
FILLING NOSE GEAR OLEO STRUT.
The nose gear should be serviced with MIL-H-5606 hydraulic fluid only. The nose gear is filled as follows:
1. Raise the airplane on jacks as explained in Chapter 7, and place a pan under the gear to catch spillage.
2. Remove the cap from the air valve and release the air pressure by depressing the valve core.
3. Remove the valve from the filler plug at the top of the strut housing.
4. Fully compress the piston tube and fill the strut with hydraulic fluid to the level of the hole for the valve .
5. Remove the core from the valve and install the valve back in the filler plug. Torque valve 350 to 400
inch-pounds.
6. Attach one end of a clean plastic hose to the valve and submerge the other end in a container of clean
hydraulic fluid, making sure the end of the hose is below the surface of the fluid
— Note —
An air tight connection is necessary between the plastic tube and the valve stem.
Without such a connection, a small amount of air will be sucked into the oleo strut
during each sequence, resulting in an inordinate amount of air bubbles and prolonged
filling operations.
7. Fully compress and extend the piston tube, thus expelling any air trapped within the strut chamber. 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.
8. When air bubbles cease to flow through the hose, compress the piston fully and remove the hose from the
valve stem.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
1 2 - 2 1 - 0 2
Page 12-05
Revised: May 15, 1989
1D5
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...