9.
Reinstall the valve core in the filler plug
— Note —
A completely empty strut will take 21 +/- 1 ounces of MIL-H-5606 hydraulic fluid.
10.
With the airplane still on jacks, compress and extend the gear piston tube several times to ascertain that
the strut will operate freely. The weight of the gear, wheel, and fork should allow the piston tube to
extend.
11. Clean off any overflow of fluid and inflate the strut.
12.
Check that fluid is not leaking around the strut piston at the bottom of the housing.
13.
With the aircraft off the jacks, and the weight on the gear, visible strut extension should be 27 +/- .25
inches.
FILLING MAIN GEAR OLEO STRUTS.
To fill the main gear oleo struts with hydraulic fluid (MIL-H-5606) use the following procedure:
1.
Raise the airplane on jacks as explained in Chapter 7, and place a pan under the gear to catch any
spillage.
2.
Unless already done so, remove the cap from the air valve and by depressing the core, relieve the air
pressure.
3.
Remove the valve from the filler plug.
4.
Fully compress the piston and fill the strut with fluid until it comes level with the hole for the valve
5.
Remove the valve core and install the valve with a torque of 350 to 400 inch-pounds.
6.
Attach one end of a clean plastic hose to the valve and submerge the other end well into a container
of hydraulic 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 prolongs
filling operation.
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, fully compress the piston and remove the hose from the
valve stem.
9.
Reinstall the air valve core.
10.
With the airplane still on jacks, compress and extend the gear piston tube several times to ascertain that
the strut will operate freely. The weight of the gear, wheel, and fork should allow the piston tube to
extend.
11. Clean off any overflow of fluid and inflate the strut with air to 200 psi.
12.
Remove the aircraft from jacks and check strut exposure for 2.6 +/- .25 inches.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
1 2 - 2 1 - 0 3
Page 12-06
Revised: May 15, 1989
1D6
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...