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时间:2011-04-11 09:19来源:蓝天飞行翻译 作者:航空
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 C.  
Access

 (1)  
Location Zone
 221,222 Control Cabin
 464 System 2 - Strut Aft Fairing
 474 System 3 - Strut Aft Fairing


 (2)  
Access Panel
 464A Trailing Edge Fairing Doors - System 2
 474A Trailing Edge Fairing Doors - System 3


 D.  
Procedure


 S 865-002
 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 015-003

 (2)
Open the doors on the trailing edge fairing (AMM 54-62-00/201).

 (3)
Release the pressure in the hydraulic system (AMM 29-11-00/201).

 S 035-005

 (4)  
Disconnect the pressure hose from the engine-driven pump (EDP) in the applicable hydraulic system (AMM 29-11-05/401).

 S 435-006

 (5)  
Connect the pressure hose from a hydraulic service cart to the pressure hose of the engine-driven pump.


 S 865-004
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 29-11-19
 ALL  ú ú 02 Page 501 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (6)  S 865-036Disconnect connector DM3108 or DM7202 (as applicable) from the fuel metering unit on the applicable engine (AMM 73-21-01/401).
 (7)  S 865-009Put the applicable HYD DEMAND PUMPS switch, on the overhead panel, P5, in the OFF position.
 (8)  S 215-010Make sure the PRESS light, for the applicable demand pump, is on.
 S 865-011

 CAUTION: OPERATE ONLY THE SYSTEMS WITH HYDRAULIC POWER WHICH THIS TEST
_______ PROCEDURE TELLS YOU TO OPERATE. KEEP THE TEST TIME TO A MINIMUM. MONITOR THE FLUID LEVEL IN THE HYDRAULIC RESERVOIR CONTINUOUSLY. BECAUSE THE HYDRAULIC FLUID CAN NOT GO BACK TO THE HYDRAULIC SERVICE CART, THE HYDRAULIC RESERVOIR CAN BECOME TOO FULL.
 (9)  
Set the hydraulic service cart to pressurize the applicable hydraulic system to 2950 to 3050 psig.

 S 215-012

 (10)
 Make sure the hydraulic pressure indication, for the applicable system, on the EICAS display is between 2900 and 3150 psig.

 S 865-013

 (11)
 Put the applicable HYD DEMAND PUMPS switch, on the overhead panel P5, in the AUTO position.

 S 215-014

 (12)
 Make sure the ACMP did not start.

 S 215-015

 (13)
 Make sure the PRESS light, for the applicable demand pump, is off.

 S 865-016

 (14)
 Slowly decrease the pressure from the hydraulic service cart to 1350 psig.

 S 215-017

 (15)
 Make sure the ACMP operates continuously for 30 seconds.

 S 865-018

 (16)
 Slowly increase the pressure from the hydraulic service cart to 1650 psig, while the ACMP is in operation.


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 29-11-19
 ALL  ú ú 02 Page 502 ú Oct 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 215-019
 (17)
 Monitor the PRESS light for the engine-driven pump (EDP) until this light goes off.

 S 215-020

 (18)
 Make sure the ACMP stops approximately 15 seconds after the PRESS light for the EDP goes off.

 S 485-041

 (19)
 Install a jumper between pins 13 and 14 of connector DM3108 or DM7202 (as applicable) on the applicable engine.

 S 215-022

 (20)
 Make sure the ACMP, in the applicable system, starts immediately.

 S 085-046

 (21)
 Remove the jumper from connector DM3108 or DM7202 (as applicabe) on the applicable engine.

 S 215-024

 (22)
 Make sure the ACMP, in the applicable system, stops immediately.

 S 485-051

 (23)
 Install a jumper between pins 13 and 14 of connector DM3108 or DM7202 (as applicable) on the applicable engine.

 S 865-027

 (24)
 Put the applicable HYD DEMAND PUMPS switch, on the overhead panel, P5, in the ON position.
 
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本文链接地址:747-400 AMM 飞机维护手册 液压 HYDRAULIC 2(32)