(c)  
Put the HYD PUMPS ENGINE switch in the ON position.

 (5)  S 614-027Do this task:  "Hydraulic Reservoir Servicing" (AMM 12-12-01/301).
 (6)  S 864-028Do this task:  "Pneumatic System Pressurization" (AMM 36-00-00/201).
 S 794-055

 S 414-032
 (9)  
Close the thrust reverser on the right side of the engine (AMM 78-31-00/201).

 S 794-059

 (10)
 Do the Ground Test Idle Leak Check, Test No. 3 (AMM 71-00-00/501).

 S 864-035

 (11)
 Remove the electrical power if it is not necessary for other operations (AMM 24-22-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-05
 ALL  ú ú 04 Page 410 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 ENGINE-DRIVEN HYDRAULIC PUMP - ADJUSTMENT/TEST
______________________________________________
 1.  General________
 A.  This procedure contains a task to an operational test of the
 engine-driven pump (EDP).

 B.  It is necessary to operate an engine to do this task.
 TASK 29-11-05-715-001
 2.  Engine-Driven Hydraulic Pump (EDP) Operational Test___________________________________________________
 A.  References
 (1)  
AMM 71-00-00/201, Power Plant

 B.  
Procedure

 S 865-002
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE FLIGHT
_______ CONTROL SURFACES BEFORE YOU OPEN THE SHUTOFF VALVES. THE FLIGHT CONTROL SURFACES CAN MOVE WHEN YOU OPEN THE SHUTOFF VALVES FOR THE FLIGHT CONTROLS. A MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN CAUSE INJURY TO PERSONS AND DAMAGE TO THE EQUIPMENT.
 (1)  
Put the eight FLT CONTROL SHUTOFF valve switches on the P461 overhead panel in the ON position.

 S 865-003

 (2)  
Close these circuit breakers:

 (a)  
P7 Overhead Circuit Breaker Panel
 1) 7F2 HYDRAULICS EDP DEPRESS 4
 2) 7G2 HYDRAULICS EDP DEPRESS 3
 3) 7H2 HYDRAULICS EDP DEPRESS 2
 4) 7J2 HYDRAULICS EDP DEPRESS 1
 5) 7J4 HYDRAULICS EDP SUPPLY 1
 6) 7J5 HYDRAULICS EDP SUPPLY 2
 7) 7J6 HYDRAULICS EDP SUPPLY 3
 8) 7J7 HYDRAULICS EDP SUPPLY 4

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-05
 ALL  ú ú 01 Page 501 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 715-020
 (3)  
Do the operational test of the EDP:

 (a)  
Put the HYD PUMP DEMAND switch, for the applicable system, in the OFF position.

 NOTE: The switch is on the P5 panel.
____
 (b)  
Put the HYD PUMP ENGINE switch, for the applicable system, in the ON position. 1) Make sure the ENGINE PRESS and SYS FAULT lights, for the

 applicable system, are on.

 (c)  
Start the applicable engine (AMM 71-00-00/201).

 (d)  
Increase the engine speed to ground idle. 1) Make sure the applicable system pressure on the EICAS STATUS display becomes stable between 2800-3200 psig.

 2)  Make sure the applicable system ENGINE PRESS and SYS FAULT lights go off.

 (e)  
Put the HYD PUMP ENGINE switch, for the applicable system, in the OFF position. 1) Make sure the applicable system pressure on the EICAS

 STATUS display decreases to less than 160 psig.
 NOTE: You can operate the rudder to decrease the
____
 pressure faster.

 2)  Make sure the applicable system ENGINE PRESS and SYS FAULT lights are on.
 (f)  
Push the HYD switch on the EICAS select panel on the pilots glare shield. 1) Make sure the HYD synoptic shows the applicable EDP is not

 in operation.

 (g)  
Put the applicable system HYD PUMP ENGINE switch in the ON position. 1) Make sure the applicable system pressure on the EICAS
　
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊(cè) 液壓 HYDRAULIC 1(106)