29-11-03
 ALL  ú ú 01 Page 402 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 864-004
 (3)
Release the pressure in the pneumatic system (AMM 36-00-00/201).

 S 864-005

 (4)  
Operate the bleed valve on the reservoir pressurization module to release the pressure in the reservoir (AMM 29-17-01/201).

 S 494-020

 (5)  
Put the container below the reservoir drain valve.

 S 684-006

 (6)  
Drain the reservoir fluid into the container.

 S 024-021

 (7)  
Remove the reservoir drain valve:

 (a)  
Remove the four bolts and the washers that attach the reservoir drain valve to the hydraulic reservoir.

 (b)  
Remove the reservoir drain valve.
 1) Discard the packing.

 (c)  
Install a cap on the reservoir port to prevent contamination.

 TASK 29-11-03-404-009
 3.  Reservoir Drain Valve Installation (Fig. 401)__________________________________
 A. Consumable Materials
 (1)  
D00153 Fluid - Hydraulic, Fire-Resistant, BMS 3-11

 B.
References

 (1)  
AMM 12-12-01/301, Hydraulic Systems

 (2)  
AMM 36-00-00/201, Pneumatic System

 (3)  
AMM 54-62-00/201, Nacelle Strut Access Panels

 (4)  
IPC 29-11-01 Fig. 1 (Outboard), IPC 29-11-01 Fig. 5 (Inboard)

 C.
Access

 (1)  
Location Zone
 454 System 1 - Strut Aft Fairing
 464 System 2 - Strut Aft Fairing
 474 System 3 - Strut Aft Fairing
 484 System 4 - Strut Aft Fairing

 (2)  
Access Panel
 454A Trailing Edge Fairing Doors - System 1
 464A Trailing Edge Fairing Doors - System 2
 474A Trailing Edge Fairing Doors - System 3
 484A Trailing Edge Fairing Doors - System 4

 D.
Procedure

 S 424-022
 (1)  
Install the reservoir drain valve:

 (a)
Remove the cap from the hydraulic reservoir port.

 (b)
Lubricate the new packing with hydraulic fluid.

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 29-11-03
 ALL  ú ú 05 Page 403 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (c) (d) (e)  Install the packing in the groove on the flange of the hydraulic drain valve.Install the hydraulic drain valve in the hydraulic reservoir with the four bolts and the washers. 1) Tighten the bolts. 2) Install a lockwire on the bolts.Make sure the drain valve handle is in the closed position. 1) Install a lockwire on the handle.
 (2)  S 614-015Do this task:  "Hydraulic Reservoir Servicing" (AMM 12-12-01/301).
 (3)  S 864-016Do this task:  "Pneumatic System Pressurization" (AMM 36-00-00/201).
 (4)  S 794-017Examine the reservoir drain valve for leakage. (a) If you find leakage, repair the cause of it.
 S 414-019

 CAUTION: MAKE SURE YOU LATCH THE FAIRING DOORS ON THE TRAILING EDGE
_______ CORRECTLY. DAMAGE CAN OCCUR IF THE DOORS OPEN DURING A FLIGHT.
 (5)  Close the fairing doors on the trailing edge of the strut (AMM 54-62-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-03
 ALL  ú ú 04 Page 404 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 HYDRAULIC SUPPLY SHUTOFF VALVE - REMOVAL/INSTALLATION
_____________________________________________________
 1.  General_______
 A.  This procedure contains the tasks to remove and install the hydraulic supply shutoff valve. The installation task contains a test of the installation of the hydraulic supply shutoff valve. During this procedure the hydraulic supply shutoff valve is referred to as the hydraulic shutoff valve.
 B.  The hydraulic shutoff valve is installed in the strut. You can get access to the valve through the pressure relief door on the forward upper midspar.
　
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