(2)
AMM 32-00-30/201, Landing Gear Door Locks
(3)
AMM 32-11-14/601, Wing Gear Torsion Links
(4)
AMM 32-11-23/401, Wing Gear Truck Mechanical Lock
(5)
AMM 32-45-01/401, Main Gear Tire and Wheel
(6)
AMM 32-61-00/501, Landing Gear Position Indicating and Warning System
(7)
AIPC 32-11-02 Fig. 2
(8)
AIPC 32-11-14 Fig. 2
(9)
AIPC 32-11-21 Fig. 1
D.
Access
(1)
Location Zone
735 Wing Landing Gear, LH
745 Wing Landing Gear, RH
E.
Procedure
S 224-046
CAUTION: MAKE SURE THAT YOU DO NOT MOVE OR DAMAGE THE WING GEAR TRUCK
_______ SENSORS OR TARGET BRACKET. IF THE TARGET BRACKET OR SENSORS ARE MOVED, THEN THE AIRPLANE SYSTEMS MAY NOT RECOGNIZE AN IN-AIR CONDITION.
(1)
If the sensor or target bracket is moved or damaged, then do the task to measure the wing landing gear truck sensor clearance (AMM 32-61-22/201).
S 224-016
(2)
Examine the structural attach points for permitted worn areas (AMM 32-11-14/601).
S 424-017
(3)
Put the lower torsion link on the truck lugs until the apex will be inboard of the upper link (Fig. 401).
S 644-018
(4)
Lubricate the threads of the lower link attach bolt (16, Fig. 403), the nut (14), and the washer (13) with grease.
(5)
Install the bolt (16) from the inboard side as shown on Fig. 403.
S 434-020
(6)
Install the washer (13) and the nut (14).
(a)
Use the spanner wrench to tighten the nut (14) 960 to 1200 pound-inches.
(b)
Loosen the nut if it is necessary to align to the nearest castellation and install the lockbolt (15).
S 434-019
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-14
ALL ú ú 02 Page 410 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
S 624-021
(7) Apply the tamper-proof putty to the lockbolt nut.
NOTE: IF you move the lockbolt nut, the putty will break.
____
S 424-022
(8)
Align the holes and install the bolt (4, Fig. 401) to install the upper torsion link (3, Fig. 401) on the outer cylinder.
S 414-023
(9)
Install the truck lock assembly (5) on the upper torsion link (3) (AMM 32-11-23/401).
S 434-024
(10)
Install the shim (6, Fig. 401), the nut (7) on the bolt (4).
S 434-025
(11)
Tighten the nut (7) 980 to 1200 pound-inches.
(a)
Loosen the nut if it is necessary to align to the nearest castellation and install the lockbolt (8).
S 624-026
(12) Apply the tamper-proof putty to the lockbolt nut.
NOTE: If you move the lockbolt nut, the putty will break.
____
S 434-027
(13)
Align the top holes of the upper torsion link (3, Fig. 402), the lower torsion link, and the truck positioner bellcrank.
(a)
Install the bolt (13, Fig. 402) from the inboard side.
S 434-028
(14)
Install the through pin (7, Fig. 402) from the inboard side and align the lockbolt holes.
S 644-029
(15)
Lubricate the washer (8) and the threads of the bolt (13) and the nut (9) with grease.
(16)
Install the washer (8) and the nut (9).
S 434-030
NOTE: Temporarily tighten the nut with your hand.
____
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-14
ALL ú ú 02 Page 411 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：747-400 AMM 飞机维护手册 起落架 LANDING GEAR 2(18)
