ASSEMBLY OF NOSE GEAR OLEO. (Refer to Figure 32-5.)
1. Ascertain that parts are cleaned and inspected.
2. To install the piston tube plug, first lubricate the tube plug and “O” ring with hydraulic fluid (MIL-H-5606)
and install the “0” ring on the plug. Lubricate the inside wall of the tube, insert the plug into the top of the
tube and push it to the fork end. Align the bolt holes of the fork, tube and plug, and install bolt assembly.
3. If desired, cement a cork in the hole in the bottom of the fork body to prevent dirt from entering between the
fork and tube.
4. To assemble the components of the orifice tube, insert the orifice plate into the bottom of the tube, with the
countersunk side of the orifice hole exposed. Secure the plate with the snap ring, lubricate and install the
“O” ring on the upper end of the tube.
5. Insert the orifice tube up through the bottom of the cylinder. With the tube exposed through the top of the
cylinder, install the lock washer and insert roll pin through the lock washer into the piston. Install the tube
lock nut finger tight at this time.
6. The fork and tube assembly may be assembled by installing the tube components on the tube. In order slide
onto the tube, the snap ring, washer, lower bearing with outer and inner “O” rings and upper bearing. Align
the lock pin holes in the upper bearing with the pin holes in the piston tube and install pins.
7. Lubricate the inner wall of the cylinder with hydraulic fluid. Carefully insert the piston tube assembly into
the bottom of the cylinder, allowing the orifice tube to guide itself into the fork tube, until the snap ring can
be installed in the annular slot at the bottom of the cylinder. Install wiper strip, slide washer into position
and secure assembly with snap ring.
8. At the top of the cylinder, tighten (torque) the orifice tube lock nut to 500 (min.) 600 (max.) inch pounds.
9. Ascertain that bushings are installed in the upper and lower torque links and then install both links. The
torque link bolt assemblies should be lubricated and installed with the flat of the bolt head hex adjacent to
the milled stop on the wide end of the link. Tighten the bolts only tight enough to allow no side play in the
link, yet be free enough to rotate.
10. Ascertain that the upper and lower oleo housing bushings are installed. Install the cylinder into the oleo
housing, position spacer washer(s) over the top of the cylinder and secure with snap ring. Install spacer
washers as required to obtain .0 to .015 of an inch thrust of the cylinder within the housing.
11. At the top of the oleo housing, install on the cylinder the aligner guide bracket and steering arm. Install cap
bolts, tighten 20 to 25 inch-pounds torque and safety with MS33540 wire.
12. Install the shimmy dampener and safety.
13. Lubricate the gear assembly. (Refer to Chapter 12.)
14. Compress and extend the strut several times to ascertain that the strut will operate freely. Weight of the gear
wheel and form should allow the strut to extend.
15. Service the oleo strut with fluid and air. (Refer to Chapter 12.)
16. Check nose gear for alignment and gear operation.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
3 2 - 2 1 - 0 3
Page 32-24
Revised: May 15, 1989
2G16
PIPER AIRCRAFT
Содержание SEMINOLE PA-44-180
Страница 18: ...CHAPTER AIRWORTHINESS LIMITATIONS PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 1A18 PIPER AIRCRAFT...
Страница 21: ...CHAPTER TIME LIMITS MAINTENANCE CHECKS PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 1A21 PIPER AIRCRAFT...
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Страница 38: ...CHAPTER DIMENSIONS AND AREAS 1B14...
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Страница 49: ...CHAPTER LIFTING AND SHORING 1C1...
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Страница 53: ...CHAPTER LEVELING AND WEIGHING 1C5...
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Страница 58: ...CHAPTER TOWING AND TAXIING 1C10...
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Страница 62: ...CHAPTER PARKING AND MOORING 1C14...
Страница 65: ...CHAPTER REQUIRED PLACARDS 1C17...
Страница 70: ...CHAPTER SERVICING 1C22...
Страница 98: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E2...
Страница 108: ...CHAPTER ENVIRONMENTAL SYSTEM 1E12...
Страница 189: ...CHAPTER AUTOFLIGHT 1H21...
Страница 192: ...CHAPTER COMMUNICATIONS 1H24...
Страница 202: ...CHAPTER ELECTRICAL POWER 1I10...
Страница 228: ...CHAPTER EQUIPMENT FURNISHINGS 1J12...
Страница 233: ...CHAPTER FIRE PROTECTION 1J17...
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Страница 238: ...CHAPTER FLIGHT CONTROLS 1J24...
Страница 304: ...2A18 CHAPTER FUEL...
Страница 325: ...2B17 CHAPTER HYDRAULIC POWER...
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Страница 357: ...2D1 CHAPTER ICE AND RAIN PROTECTION...
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Страница 414: ...CHAPTER LANDING GEAR 2F13...
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Страница 479: ...2I6 CHAPTER LIGHTS...
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Страница 488: ...2I16 CHAPTER NAVIGATION AND PITOT STATIC...
Страница 503: ...2J7 CHAPTER OXYGEN...
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Страница 524: ...2K6 CHAPTER VACUUM...
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Страница 535: ...2K19 CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTIPURPOSE PARTS...
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Страница 547: ...2L7 CHAPTER STRUCTURES...
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Страница 582: ...CHAPTER DOORS 3A18...
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Страница 593: ...CHAPTER STABILIZERS 3B8...
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Страница 604: ...CHAPTER WINDOWS 3B22...
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Страница 611: ...CHAPTER WINGS 3C10...
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Страница 624: ...CHAPTER PROPELLER 3D1...
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Страница 643: ...CHAPTER POWER PLANT 3D21...
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Страница 667: ...CHAPTER ENGINE FUEL SYSTEM 3F1...
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Страница 681: ...CHAPTER IGNITION 3F16...
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Страница 712: ...CHAPTER ENGINE INDICATING 3H1...
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Страница 730: ...CHAPTER EXHAUST 3H19...
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Страница 734: ...CHAPTER OIL 3I1...
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Страница 743: ...CHAPTER STARTING 3I11...
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Страница 755: ...CHAPTER TURBINES 3J1...
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Страница 787: ...CHAPTER CHARTS AND WIRING DIAGRAMS 4A18...
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