S 426-004
(3) Install the outboard door of the shock strut for the body landing gear (Ref 32-14-06/401).
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MAINTENANCE MANUAL
Outboard Door Wear Limits of the Shock Strut for the Body Landing Gear
Figure 601 (Sheet 1)
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MAINTENANCE MANUAL
2.
BUSHING FLANGE (8 LOCATIONS)
3.
BEARING/BOLT 3. BEARING/BOLT
A-A A-A (ALTERNATE) (PREFERRED)
Outboard Door Wear Limits of the Shock Strut for the Body Landing Gear
Figure 601 (Sheet 2)
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MAINTENANCE MANUAL
NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS REPLACE WORN PART PART WORN REPAIR INSTR REPAIR
DIAMETER MITTED PER-WEAR DIM. 7 DIA ANCE MAX CLEAR-
MIN MAX
1 BUSHING ID 0.2515 0.2555 0.2695 0.020 1
BOLT OD 0.2490 0.2495 0.2315 X
2 BUSHING 2 0.030 1
3 BEARING ID 0.2495 0.2500 0.2695 OR 0.020 3 4
BOLT OD 0.2490 0.2495 0.2295 X
4 BUSHING ID 0.2500 0.2515 0.2695 0.020 5
BOLT OD 0.2490 0.2495 0.2300 X
5 BUSHING ID 0.4375 0.4390 0.4455 0.010 6
BUSHING OD 0.4335 0.4355 0.4245 X
GET BUSHING. INSTALL BUSHING PER 20-11-01 WITH INTERFERENCE FIT OF 0.0004-0.0023 INCH. MINIMUM FLANGE THICKNESS FOR FLANGED BUSHINGS.
0.010 INCH BETWEEN BALL AND RACE.
GET BEARING. INSTALL BEARING PER 20-11-01 WITH INTERFERENCE FIT OF 0.0005-0.0017 INCH.
GET BUSHING. INSTALL BUSHING PER 20-11-01 WITH INTERFERENCE FIT OF 0.0003-0.0013 INCH.
MAXIMUM OVERSIZE BUSHING AND HOLE IN FITTING IS 0.0625 INCH, IF IT IS NECESSARY.
GET BUSHING. INSTALL BUSHING PER 20-11-01 WITH INTERFERENCE FIT OF 0.0003-0.0016 INCH.
MAXIMUM OVERSIZE BUSHING AND HOLE IN FITTING IS 0.0625 INCH, IF IT IS NECESSARY.
YOU CAN HAVE MORE THAN THE LIMITS SHOWN IF YOU DO NOT HAVE MORE THAN THE MAXIMUM CLEARANCE.
Outboard Door Wear Limits of the Shock Strut For the Body Landing Gear
Figure 601 (Sheet 3)
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NOSE GEAR AND DOORS - DESCRIPTION AND OPERATION
_______________________________________________
1. General_______
A. The nose gear supports the forward end of the fuselage and controls the direction of the airplane while it is moving on the ground. The nose gear is hydraulically operated to retract forward and up into a wheel well, a recess in the lower nose compartment. Shocks from the impact of landing and rolling over bumps on the ground are absorbed by a shock strut. The shock strut contains oil and is charged with compressed air or nitrogen. For steering, the shock strut inner cylinder turns inside the outer cylinder.
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本文鏈接地址：747-400 AMM 飛機維護手冊 起落架 LANDING GEAR 3(96)
