S 032-054
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-13-03
 ALL  ú ú 01 Page 202 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (e)  Install the covers on the CLCP openings to prevent contamination.
 TASK 22-13-03-402-060
 3.  Central Lateral Control Package Electrohydraulic Servovalve and Solenoid________________________________________________________________________ Valve Installation__________________
 A.  Standard Tools and Equipment
 (1)  
Bonding Meter - Autron T477W or equivalent

 (2)  
O-Ring Installation Tool - ST848

 (3)  
Torque Wrench - Commercially available

 B.  Consumable Material
 (1)  
G00062 Fluid - Hydraulic, Fire Resistant, BMS 10-11

 (2)  
D00013 Lubricant - Grease, MIL-G-23827

 (3)  
D00054 Lubricant - Assembly, Skydrol, MCS352

 C.  References
 (1)  
AMM 09-11-00/201 Towing

 (2)  
AMM 20-11-19/401, O-Ring

 (3)  
AMM 20-11-28/401, Lockwire

 (4)  
AMM 20-22-01/601, Electrical Bonding

 (5)  
AMM 24-22-00/201, Manual Control

 (6)  
AMM 29-11-00/201, Main Hydraulic Supply System

 (7)  
AMM 32-00-30/201, Landing Gear Door Locks

 D.  Access
 (1)  Location Zone
 135 Wing Landing Gear Well - LH
 136 Wing Landing Gear Well - RH
 137 Body Landing Gear Well - LH
 138 Body Landing Gear Well - RH

 E.  Prepare for the Installation
 S 862-061
 (1)  
Remove the hydraulic pressure from the applicable system (AMM 29-11-00/201).

 S 862-062

 (2)  
Put the FLT CONTROL HYD POWER WING 1, 2, 3, and 4 switches in the SHUTOFF position. The switches are on the Pilot's Overhead Maintenance Panel, P461.

 S 862-063

 (3)
Open these circuit breakers and attach the DO-NOT-CLOSE tags:

 (a)  P7, Overhead Circuit Breaker Panel 1) 7D7, FLT CONT CMPTR L SERVO 2) 7D8, FLT CONT CMPTR L PWR 3) 7D14, FLT CONT CMPTR R SERVO 4) 7D15, FLT CONT CMPTR R PWR 5) 7E9, MCP L 6) 7E18, MCP R
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-13-03
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
 (b)  P180, CD Power Distribution Panel
 1) 180E6, LATERAL CONT VALV SYS 2
 2) 180E22, LATERAL CONT VALV SYS 4
 3) 180H7, LATERAL CONT VALV SYS 1
 4) 180H23, LATERAL CONT VALV SYS 3

 F.  Procedure
 S 162-064
 CAUTION:_______DO NOT LET HYDRAULIC FLUID GET INTO THE ELECTRICAL CONNECTOR. CONTAMINATION BY HYDRAULIC FLUID CAN CAUSE DAMAGE AND FAILURE OF THE ELECTRICAL DEVICE.
 (1)  
Remove the covers from the electrical and hydraulic openings. Clean the mating surfaces of the valve, gasket plate and CLCP with clean hydraulic fluid.

 S 622-065

 (2)  
Apply a thin layer of MCS352 lubricant on the new seal plate and O-ring.

 S 432-066

 (3)  
Install the new O-ring on the valve (AMM 20-11-19/401).

 S 642-067

 (4)  
Apply a thin layer of grease (MIL-G-23927) on the mounting screws.

 S 432-068

 (5)  
Install the gasket plate on the CLCP.

 S 422-069

 (6)  
Install the valve on the CLCP with the mounting screws and washers.

 S 432-070

 (7)  
Tighten the mounting screws to 50-70 pound-inches.

 S 762-071

 (8)  
Use a bonding meter to measure the resistance between the valve and the CLCP body. The resistance must be 5.0 milliohms (0.005 ohms) or less (AMM 20-22-01/601).

 (9)
Put lockwire through the mounting screws (AMM 20-11-28/401).

 S 432-072
 TASK 22-13-03-702-073
　
中國航空網 m.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(120)