ADJUSTMENT OF NOSE LANDING GEAR. (Refer to Figure 32-9.)
The gear up stop is located on the steering bellcrank.
1. Place the airplane on jacks. (Refer to Chapter 7.)
— CAUTION —
WHENEVER AIRCRAFT IS PLACED ON JACKS FOR THE PURPOSE OF
M A N U A L LY RETRACTING THE NOSE GEAR ASSEMBLY, INSURE THE
NOSE GEAR DOWNLOCK IS FULLY DISENGAGED BEFORE RELEASING
THE NOSE GEAR DRAG LINKS DAMAGE COULD OCCUR TO THE
DOWNLOCK IF NOT FULLY DISENGAGED.
2. Disconnect both nose gear door actuation rods.
3. Turn master switch OFF, pull out Free Fall Control.
4. Disconnect the aft end of the cylinder from its attachment fitting by removing the connecting nut, bolt and
washer.
5. Pull out the cylinder rod to it full extended position. Measure and record the exposed length of the rod.
6. Retract the cylinder rod as required and reconnect aft end of the cylinder to its attachment fitting using nut,
bolt and washer.
7. Loosen jam nut on secondary up stop and turn in so it will not interfere with initial rigging.
8. Push in free fall control and retract the nose gear by turning the master switch ON and moving the gear
selector handle to the UP position. Check the adjustment of the cylinder rod end bearing by placing a
carpenters square with the longest end along the bottom of the fuselage, and the shortest end running up
through the centerline of the wheel axle. Measure up along the square from the bottom of the fuselage 8.25
inches, to determine if the center of the wheel axle meets this measurement. If this measurement is
incorrect, extend the gear, loosen the jam nut on the rod end bearing and make the required adjustment by
turning the bearing in to raise wheel, out to lower.
9. Turn secondary up stop out until finger tight against strut. Lower gear and turn stop out one additional turn
and tighten jam nut.
10. Tighten jam nut on rod end bearing and check that threads cover safety hole in actuator rod.
11. Measure length of exposed rod. Subtract from value obtained in Step 5 and determine that at least 0.06
inches of travel remains to full extension.
12. Adjust shimmy dampener by turning nose wheel stops and adjusting the rod ends of the dampener for 30°
travel to both extremes.
13. Reconnect both nose gear door actuation rods.
14. Push in Free Fall Control, turn master switch ON. Retract landing gear and check doors.
15. Lower gear. Turn master switch OFF. Ascertain that the landing gear is down and locked, then remove the
airplane from jacks.
ALIGNMENT OF NOSE LANDING GEAR.
1. Place the airplane on a smooth level floor that will accommodate the striking of a chalk line.
2. Ascertain that the nose gear is properly adjusted.
3. With the landing gear in the downlock position, weight proportionally on the nose gear and the nose wheel
facing forward, adjust the steering bellcrank. The bellcrank may be adjusted by loosening its attachment
bolt and sliding the bellcrank fore and aft until it clears each steering arm rollers by .031 of an inch.
Retighten the attachment bolt.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
3 2 - 2 2 - 0 8
Page 32-35
Revised: May 15, 1989
2H3
PIPER AIRCRAFT
Содержание SEMINOLE PA-44-180
Страница 18: ...CHAPTER AIRWORTHINESS LIMITATIONS PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 1A18 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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