S 864-003
(2)
Remove the pressure from hydraulic system 1 (AMM 29-11-00/201).
S 494-004
WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASKS BELOW TO INSTALL
_______ THE DOOR LOCKS ON THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT INSTALL THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(3)
Do this task: "Wing Landing Gear Door Lock Installation"
(AMM 32-00-30/201).
S 494-033
(4)
Do this task: "Body Landing Gear Door Lock Installation"
(AMM 32-00-30/201).
S 864-005
(5)
Open these circuit breakers and attach DO-NOT-CLOSE tags:
(a)
P6, Main Power Distribution Panel
1) 6C28, ALT LG EXT NOSE
2) 6C31, ALT LG EXT BODY L
3) 6C32, ALT LG EXT BODY R
E.
Remove the Uplock Mechanism.
S 034-006
(1) Disconnect each end of the uplock actuator and hold the actuator to one side (AMM 32-33-14/401).
NOTE:____The uplock actuator is part of the assembly. It is not necessary to fully remove it when you remove the uplock mechanism. Do not disconnect the actuator hoses unless you must install a new actuator.
S 034-007
(2) Disconnect the forward end of the rod that operates the sequence valve from the uplock assembly (AMM 32-33-07/401).
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A 747-400 MAINTENANCE MANUAL
SEE A
ELECTRICAL ACTUATOR
HYDRAULIC UPLOCK ACTUATOR
FWD LGDR1B LEFT LGDR2B RIGHT
TURNBUCKLE
LGDR1A LEFT LGDR2A RIGHT
UPLOCK ATTACH BOLT
UPLOCK-OPERATED SEQUENCE VALVE
RIGGING PIN AE/GD-9 LEFT
UPLOCK
ATTACH BOLT
(2 LOCATIONS)
UPLOCK BOLT
ASSEMBLY
A
Body Landing Gear Uplock Mechanism Installation
Figure 401
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
RUBBER SLEEVE
(1/2 INCH ID X 1/8 INCH THK)
CAUTION:DO NOT USE THIS TOOL IF THE RUBBER SLEEVE IS DAMAGED. EXAMINE THE SLEEVE FOR DAMAGE BEFORE AND AFTER USE. INSTALL A NEW SLEEVE IF IT IS DAMAGED. THE TOOL CAN CAUSE DAMAGE TO THE UPLOCK MECHANISM.
ACTUATING TOOL
LOCK CLOSED LOCK OPEN
Uplock Actuating Tool
Figure 402
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A
747-400 MAINTENANCE MANUAL
(3) S 034-008Remove the two bolts that attach the forward end of the sequence valve bracket to the uplock assembly.
(4) S 034-009Remove the four bolts that attach the sequence valve bracket to the structure.
(5) S 014-034Move the valve and the bracket away to get to the mounting bolt.
(6) S 014-010Disconnect the uplock sensor (AMM 32-61-11/201).
(7) S 014-035Remove the clamps that attach the sensor conduit.
(8) S 034-036Loosen the conduit nut at the junction box.
(9) S 014-037Move the conduit away from the mechanism to permit the removal of the mechanism.
S 034-011
(10) 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：747-400 AMM 飛機維護手冊 起落架 LANDING GEAR 4(141)
