(c)
Loosen the nut to 10-50 pound-feet.
(d)
While you turn the wheel again, tighten the nut to 110 pound-feet.
(e)
If the holes in the axle for the lockbolt are not aligned with the slots in the nut, do these steps: 1) Tighten the nut more, if necessary, to align the lockbolt
holes. Do not tighten the nut to more than 160 pound-feet.
2) Do not loosen the nut to align the lockbolt holes. If the lockbolt holes are not aligned at the maximum permitted torque, fully loosen the nut and do steps (a) thru (d) again.
S 424-037
(18)
Install the two lockbolts (8) through the retention nut (3), the axle, and the antiskid transducer support and attach with the washers (7) and the nuts (6).
S 424-038
(19)
Install the bolts (8) with the heads of the bolts on the inside of the axle.
(20)
Tighten the bolts (8).
(21)
Install the hubcap (4) and the antiskid transducer drive.
S 424-039
S 434-040
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757 MAINTENANCE MANUAL
S 824-041
(22) Make sure the coupling halves for the antikid transducer are aligned.
S 434-065
CAUTION:_______DO NOT OVERTIGHTEN THE HUBCAP BOLTS. IF THE BOLTS ARE OVERTIGHTENED, IT WILL CAUSE DAMAGE TO THE BOLTS.
(23)
Install the hubcap (4) with the bolts (5), the washers (9), and the nuts (10). Tighten the bolts to 50-80 inch-pounds.
S 614-043
(24)
Do a check for correct tire pressure and inflate the tire to the correct pressure if it is necessary (AMM 12-15-03/301).
S 584-044
(25)
Lower the main gear with the jack (AMM 07-11-03/201).
S 584-045
(26)
Remove the jack (AMM 07-11-03/201).
S 844-064
(27)
Remove electrical power if it is no longer necessary (AMM 24-22-00/201).
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MAINTENANCE MANUAL
1. WHEEL AND TIRE
FWD
WHEEL CHANGE DOLLY
BRAKE
SEE A
A
AXLE 2. TANG WASHER 11. WHEEL SPACER 3. WHEEL RETENTION NUT GREASE SEAL 7. WASHER
6. NUT 4. HUBCAP WHEEL (METAL) 1 SEE B
10. NUT
9. WASHER A
8. LOCKBOLT
(2 LOCATIONS)
5. BOLT (3 LOCATIONS)
4.
HUBCAP (PLASTIC) 1
5.
BOLT (3 LOCATIONS)
1 AIRPLANE CAN USE EITHER A
PLASTIC OR METAL HUBCAP ASSEMBLY
Main Gear Wheel and Tire Installation
Figure 401 (Sheet 1)
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A 757 MAINTENANCE MANUAL ASSEMBLY BRAKE
TRANSDUCER
TRANSDUCER DRIVE COUPLING
AXLE
HUBCAP
WHEEL
TIRE
(9 LOCATIONS) DRIVE KEY BRAKE ROTOR WHEEL (TIRE NOT SHOWN) A-A WHEEL (TIRE NOT SHOWN)
(2 LOCATIONS) BEARING
(2 LOCATIONS) BEARING
DUNLOP WHEEL B BF GOODRICH WHEEL B ROTOR TORQUE BAR (8 LOCATIONS)
Main Gear Wheel and Tire Installation Figure 401 (Sheet 2)
G61207
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NOSE GEAR WHEEL AND TIRE - REMOVAL/INSTALLATION
_______________________________________________
1. General_______
A. This procedure contains two tasks. The first task is a removal of the wheel and tire assembly for the nose gear. The second task is an installation of the wheel and tire asembly for the nose gear.
B. When you replace a nose wheel and tire assembly, you can replace the wheel and tire assembly on the other side. Differences in the diameter between new and worn tires can contribute to nose landing gear vibration. You can decrease this if you install tires that have equal pressures, nearly the same inflated diameters, and matching supplier part numbers.
TASK 32-45-02-024-001
2. Remove the Nose Gear Wheel and Tire (Fig. 401)___________________________________
A. Equipment
(1)
Dolly - Wheel Change - commercially available
(2)
Protector - Nose Landing Gear Axle - B32021-1
(3)
Wrench - NLG Wheel Retaining Nut -(Commercially Available)
(4)
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本文链接地址：757 AMM 飞机维护手册 起落架 CHAPTER 32 - LANDING GEAR 3(76)
