(a)  
P180 DC Power Distribution Panel
 1) 180H7 LATERAL CONT VALV SYS 1
 2) 180E6 LATERAL CONT VALV SYS 2
 3) 180H22 LATERAL CONT VALV SYS 3
 4) 180E21 LATERAL CONT VALV SYS 4

 S 714-015
 (6)  
Do a test of the shutoff valve (3) (Ref 27-13-01/501).

 S 794-016

 (7)  
Examine the valve and the connections for leaks.

 F.
Put the Airplane Back To Its Usual Condition

 S 864-017
 (1)  
Remove hydraulic power (Ref 29-11-00/201).

 S 864-018

 (2)  
Remove electrical power (Ref 24-22-00/201).

 S 414-019

 (3)  
If it is open, close the access panels of the outboard aileron (Ref 06-09-08/201).

 (4)  
Service the hydraulic reservoir (Ref 12-12-01/301).

 S 614-020
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-13-01
 ALL  ú ú 01 Page 405 ú Feb 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 HYDRAULIC SHUTOFF WING VALVE - ADJUSTMENT/TEST
______________________________________________
 1.  General_______
 A.  This procedure contains a test of the hydraulic shutoff wing valve for all four hydraulic systems. Each system supplies hydraulic pressure to a different group of surfaces. These are the four hydraulic systems:
 (1)  
SYS 1 controls the central lateral control package (CLCP)-right autopilot, and left outboard and inboard ailerons.

 (2)  
SYS 2 controls the CLCP-right autopilot, left outboard aileron, right inboard aileron, and No. 2, 3, 10 and 11 spoilers.

 (3)  
SYS 3 controls the CLCP-left autopilot, left inboard aileron, right outboard aileron, and No. 1, 4, 9 and 12 spoilers.

 (4)  
SYS 4 controls the CLCP-left autopilot, right inboard and outboard aileron, and No. 5, 6, 7 and 8 spoilers.

 TASK 27-13-01-705-001
 2.  The Hydraulic Shutoff Wing Valve Test_____________________________________
 A.  References
 (1)  
AMM 06-09-08/201, Wing Access Doors and Panels

 (2)  
AMM 24-22-00/201, Manual Control

 (3)  
AMM 29-11-00/201, Main Hydraulic Supply System

 (4)  
AIPC 27-13-01 Fig. 1

 (5)  
SSM 27-13-01

 (6)  
WDM 27-13-11

 B.  
Access

 (1)  
Location Zone 592 Outboard Aileron, LH 692 Outboard Aileron, RH 571 Rear Spar to Landing Gear Support Beam, LH 671 Rear Spar to Landing Gear Support Beam, RH

 (2)  
Access Panel Gain access to rear spar through wing gear wheel well door: 591BB Outboard Aileron, LH 691BB Outboard Aileron, RH

 C.  
Procedure

 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 865-002
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-13-01
 ALL  ú ú 01 Page 501 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (2)  S 865-003Make sure the FLT CONTROL HYD POWER - WING VALVE switch on the P461 Pilot's Overhead Maintenance Panel is in NORM.
 (3)  S 715-005Make sure the VALVE CLOSED indicator light is off.
 S 865-006

 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. THIS CAN PREVENT POSSIBLE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (4)  
Supply hydraulic power on the system with the shutoff wing valve replaced (AMM 29-11-00/201).

 S 715-014

 (5)  
Operate the control wheel.

 (a)  
Make sure the surfaces operate smoothly through the full range of travel.

 NOTE: The outboard ailerons will move only when trailing edge
____ flaps extend between the 1 degree detent and the full down position.
 S 865-008
 (6)  
Set the FLT CONTROL HYD POWER - WING VALVE switch on the P461 Pilot's Overhead Maintenance Panel to SHUTOFF.
　
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 飛行操縱 FLIGHT CONTROLS 2(30)