(2)
AMM 20-11-19/401, O-Ring
(3)
AMM 20-11-28/401, Lockwire
(4)
AMM 24-22-00/201, Manual Control
(5)
AMM 29-11-00/201, Main Hydraulic Supply System
(6)
AMM 32-00-30/201, Landing Gear Door Locks
C. Access
(1) Location Zone
135 Left Wing Landing Gear Well
D. Prepare for Removal
S 482-083
WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK 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.
(1) Do this task: "Install the Door Locks on the Wing and Body Landing Gear" (AMM 32-00-30/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-13-02
ALL ú ú 01 Page 201 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
LAS
SEE A
4. GASKET PLATE
6. O-RING
2. SOLENOID VALVE 2 (ENGAGE)
6. O-RING
3. ELECTROHYDRAULIC SERVOVALVE
5. SCREWS
CONTROL (4 EACHROD VALVE)
4. GASKET PLATE
6. O-RING
1. SERVO
ASSEMBLY
4. GASKET PLATE
2. SOLENOID VALVE 1 (ARM)
A
LAS Electrohydraulic Servovalve and Solenoid Valves Installation Figure 201
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-13-02
ALL ú ú 01 Page 202 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 492-049
(2)
Make sure the ground lockpins, for the landing gear, are installed (AMM 09-11-00/201).
S 862-068
(3)
Supply electrical power (AMM 24-22-00/201).
S 862-069
(4)
Remove hydraulic pressure from hydraulic system number 1.
S 862-070
(5)
Put the FLT CONTROL HYD POWER WING 1 switch to the SHUTOFF position. The switches are found on the Pilots Overhead Maintenace Panel (P461).
S 862-071
(6)
Open the circuit breakers shown below and attach DO-NOT-CLOSE tags:
(a)
P7, Overhead Circuit Breaker Panel
1) 7D12, FLT CONT CMPTR SERVO C
2) 7D13, FLT CONT CMPTR PWR C
3) 7E9, MCP L
4) 7E18, MCP R
(b)
P180, DC Power Distribution Panel
1) 180H7, LATERAL CONT VLV SYS 1
E. Valve Removal
S 162-051
CAUTION: DO NOT LET CONTAMINATION GET INTO THE LAS, EHSV OR SOLENOID
_______ VALVES. THE CONTAMINATION CAN CAUSE DAMAGE AND/OR FAILURE TO THE EQUIPMENT
(1) Clean the surface of the valve with a clean rag.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-13-02
ALL ú ú 01 Page 203 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 032-052
(2) Do these steps to remove the valve:
(a)
Remove the lockwire (AMM 20-11-28/401).
(b)
Hold the valve and remove the mounting bolts and washers.
(c)
Remove the valve from the LAS.
(d)
A gasket plate is installed between the valve and the LAS. Make sure you remove the gasket plate when you remove the valve.
(e)
Remove the O-ring from the valve (AMM 20-11-19/401).
(f)
Put covers on the valve openings to prevent contamination.
TASK 22-13-02-422-063
3. Lateral Autopilot Servo Electrohydraulic Servovalve and Solenoid Valve______________________________________________________________________ Installation (Fig. 201)____________
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 空調 AUTO FLIGHT(116)
