29-31-00
 ALL  ú ú 02 Page 503 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 2) 7G1 HYDRAULICS DEMAND 3 3) 7H1 HYDRAULICS DEMAND 2 4) 7J1 HYDRAULICS DEMAND 1
 S 865-005
 WARNING:_______ MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE FLIGHT
 CONTROL SURFACES.  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 DAMAGE TO

 EQUIPMENT AND INJURY TO PERSONS.
 (4)  Put the eight FLT CONTROL SHUTOFF switches in the ON position. NOTE: The switches are on the P461 panel.
____
 S 015-006
 (5)  Open the fairing doors on the trailing edge of the strut (AMM 54-62-00/201).
 S 865-007 WARNING: MAKE SURE YOU RELEASE THE PNEUMATIC SYSTEM PRESSURE BEFORE YOU
_______ OPEN THE HYDRAULIC SYSTEM. THE PNEUMATIC SYSTEM PRESSURIZES THE HYDRAULIC RESERVOIR. HYDRAULIC FLUID THAT HAS PRESSURE CAN CAUSE INJURY TO PERSONS.
 (6)  
Release the pressure in the pneumatic system (AMM 36-00-00/201). S 985-008

 (7)  
Operate the bleed valve on the reservoir pressurization module to decrease the system reservoir pressure to 0 psig (AMM 29-17-01/201).

 S 015-010

 (8)  
Open the right thrust reverser half (AMM 78-31-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-31-00
 ALL  ú ú 02 Page 504 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 865-012
 WARNING: MAKE SURE YOU RELEASE THE HYDRAULIC SYSTEM PRESSURE BEFORE YOU
_______ OPEN THE HYDRAULIC SYSTEM. HYDRAULIC FLUID THAT HAS PRESSURE CAN CAUSE INJURY.
 (9)  
Release the pressure in the hydraulic system (Ref 29-11-00/201).

 S 485-057

 (10)
 Connect the hydraulic test bench:

 (a)  
Disconnect the hose at the pressure port on the engine-driven pump (EDP) of the applicable system (AMM 29-11-05/401).

 (b)  
Connect the pressure hose from the test bench to the EDP pressure hose.

 (c)  
Connect the return hose from the test bench to the return-module-service disconnect for the applicable system.

 S 865-016
 (11) Put the HYD PUMPS DEMAND switch for the applicable system in the OFF position.
 NOTE: The switch is on the P5 panel.
____
 S 285-017
 (12)
 Make sure the reservoir quantity indication, on the EICAS status page for the applicable system, is between 0.7-1.1.

 S 285-053

 (13)
 Make sure the reservoir fluid temperature, on the EICAS status page for the applicable system, is less than 158°F (70°C).

 S 215-018

 (14)
 Make sure the PRESS light for the demand pump of the applicable system is on.

 NOTE: The light is on the P5 panel.
____
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-31-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 215-019
 (15)
 Make sure the HYD PRESS SYS display, for the applicable system, shows on the primary EICAS screen.

 S 215-020

 (16)
 Make sure the function display, for the applicable system, shows on the hydraulic synoptic page of the auxiliary EICAS screen.

 S 785-021

 (17)
 Do these steps while you monitor the applicable SYS FAULT light and the test bench pressure:

 (a)  
Slowly increase the test bench pressure to 1300 psig.

 (b)  
　
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