2..............…..................…............................…................1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-15-00
ALL ú ú 01 Page 113 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
HYDRAULIC SYSTEMS A, B, AND STANDBY - MAINTENANCE PRACTICES
___________________________________________________________
1. General_______
A. When it is necessary to open a hydraulic line, you must release the pressure from the reservoir for the applicable hydraulic system (AMM 29-09-00/201).
B. If hydraulic fluid gets on the airplane, then refer to 12-40-00/201 to clean it up.
TASK 29-15-00-862-001
2. Pressurize the A, B, or Standby Hydraulic System________________________________________________
A. General
(1)
Hydraulic systems A and B are almost the same, thus the same procedure is used for the two systems. The standby hydraulic system has a different procedure.
(2)
If you pressurize the A hydraulic system, these parts will get hydraulic power:
(a)
The ground spoilers (0, 1, 4, 5, 8, 9)
(b)
Through the alternate (brake) source selector valve (alternate source) 1) Deleted. 2) The alternate brakes
(c)
The left thrust reverser (primary source)
(d)
The landing gear transfer valve (primary source landing gear operation)
(e)
Through the system A flight control module 1) The flight spoilers 3, 6 2) The lower aileron power control unit 3) The right auto-pilot actuator 4) The rudder 5) The left elevator power control unit 6) The lower auto-pilot actuator 7) The left elevator feel
(3)
If you pressurize the B hydraulic system, these parts will get hydraulic power:
(a)
The leading edge flaps and slats
(b)
The trailing edge flaps
(c)
The primary brakes
1) Deleted.
(d)
The right thrust reverser (primary source)
(e)
The landing gear transfer valve (alternate source landing gear operation)
(f)
Through the system B flight control module 1) The flight spoilers 2, 7
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-15-00
ALL ú ú 01 Page 201 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
2) The upper aileron power control unit 3) The left auto-pilot actuator 4) The rudder 5) The right elevator power control unit 6) The upper auto-pilot actuator 7) The right elevator feel
(4) If you pressurize the standby hydraulic system, these parts will get hydraulic power.
(a)
The standby rudder
(b)
The standby leading edge flaps and slats (extend only)
(c)
The left and right thrust reversers (alternate source)
B. Standard Tools and Equipment
(1)
Hydraulic test stand - 0 to 3000 psi, with Hydraulic Fluid BMS 3-11 (AMM 20-30-21/201)
(2)
Ground Lock Assembly (AMM 32-00-01/201)
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 液壓 HYDRAULIC POWER(68)
