S 494-065
(10)
Do this task: "Removal of the Door Locks from the Doors for the Body Landing Gear" (Ref 32-00-30/201).
S 864-067
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS, ELEVATORS, FLAPS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(11) Supply hydraulic power to system No. 1 (Ref 29-11-00/201).
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32-31-03
ALL ú ú 01 Page 414 ú Oct 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 874-029
(12)
Bleed air from the selector valve (1).
(a)
Move the control handle to the UP and DN position, two or three times.
NOTE:____This will open and close the wheel well doors. The correct operation of the wheel well doors shows the selector valve works correctly.
S 794-030
(13)
Do a check of the hydraulic connections for leaks.
S 864-031
(14)
Put the control handle in the DN position.
(15)
Remove hydraulic power if it is not necessary (Ref 29-11-00/201).
S 864-032
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32-31-03
ALL ú ú 01 Page 415 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
LANDING GEAR SELECTOR VALVE QUADRANTS - REMOVAL/INSTALLATION
____________________________________________________________
1. General_______
A. This procedure contains two tasks:
(1)
The removal of the selector valve quadrant for the wing landing gear
(2)
The removal of the selector valve quadrant for the body landing gear and nose landing gear
(3)
The installation of the selector valve quadrant for the wing landing gear
(4)
The installation of the selector valve quadrant for the body landing gear and the nose landing gear.
B.
To remove the selector valve quadrants these steps are necessary:
(1)
Disconnect the turnbuckles until the cables are loose at the quadrant.
(2)
Disconnect the control rod assembly from the quadrant clevis.
(3)
Disconnect the quadrant from the structure.
(4)
Disconnect the cables from the quadrant.
C.
To install the selector valve quadrants these steps are necessary:
(1)
Connect the cables to the quadrant.
(2)
Connect the quadrant to the structure.
(3)
Connect the control rod assembly to the quadrant clevis.
(4)
Adjust the control system for the landing gear.
(5)
Do the system test for the control system.
D.
There are two selector valves and two selector valve quadrants for the landing gear. One quadrant is for the selector valve for the wing landing gear. One quadrant is for the selector valve for the nose landing gear and the body landing gear.
TASK 32-31-04-004-001
2. Wing Landing Gear Selector Valve Quadrant Removal_________________________________________________
A. References
(1)
09-11-00/201, Towing
(2)
25-22-01/401, Main Passenger Cabin Ceiling Panels
(3)
29-11-00/201, Main Hydraulic Supply System
(4)
32-00-30/201, Landing Gear Door Locks
(5)
32-31-00/501, Landing Gear Control
(6)
IPC 32-31-63 Fig. 1
B.
Access
(1)
Location Zone
138 Body Landing Gear Wheel Well, Right
C.
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本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊 起落架 LANDING GEAR 4(38)
