(2)
Union - MS21902-20 (used to open the EDP supply hose self-sealing coupling)
B.
References
(1)
AMM 29-11-00/201, Main Hydraulic Supply System
(2)
AMM 29-11-05/401, Engine Driven Pump
(3)
AMM 36-00-00/201, Pneumatic System
(4)
AMM 78-31-00/201, Thrust Reverser System
C.
Access
(1)
Location Zone 412 Engine 1 - The 2:00 Face of the Engine Nacelle Firewall 422 Engine 2 - The 2:00 Face of the Engine Nacelle Firewall 412 Engine 3 - The 2:00 Face of the Engine Nacelle Firewall 422 Engine 4 - The 2:00 Face of the Engine Nacelle Firewall
(2)
Access Panel 416 Engine 1 - Right Half of the Thrust Reverser 426 Engine 2 - Right Half of the Thrust Reverser 436 Engine 3 - Right Half of the Thrust Reverser 446 Engine 4 - Right Half of the Thrust Reverser
D.
Procedure
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A
747-400 MAINTENANCE MANUAL
SEE A
SUPPLY HOSE SELF-SEALING DISCONNECT
COVER PLATE
HYDRAULIC PRESSURE HOSE
FUEL HOSE
HYDRAULIC
SUPPLY HOSE
HYDRAULIC CASE DRAIN HOSE
FWD
A
Supply Hose Self-Sealing Disconnect (Firewall Mounted) Installation Figure 401
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 864-001
WARNING:_______ DO NOT OPEN THE HYDRAULIC SYSTEM BEFORE RELEASE THE PRESSURE IN
THE PNEUMATIC SYSTEM. THE PNEUMATIC SYSTEM PRESSURIZES THE
HYDRAULIC RESERVOIR. PRESSURIZED HYDRAULIC FLUID CAN CAUSE
INJURY.
(1)
Release the pressure in the pneumatic system (AMM 36-00-00/201).
(a)
Operate the bleed valve on the pressurization module to release the pressure in the reservoir (AMM 29-11-00/201).
S 014-003
(2)
Open the right half of the thrust reverser for the applicable engine (AMM 78-31-00/201).
S 684-024
(3)
Drain the hydraulic reservoir:
(a)
Disconnect the hydraulic supply hose from the EDP (AMM 29-11-05/401).
(b)
Put a container below the EDP.
(c)
Install the MS21902-20 union in the self-sealing disconnect.
(d)
Drain the hydraulic reservoir.
(e)
Remove the union from the self-sealing disconnect.
S 684-006
(4)
Connect the hydraulic supply hose to the EDP.
(a)
Tighten the supply hose connection to 855-945 pound-inches (95-105 N.m).
S 034-007
(5)
Disconnect the hydraulic supply hose below the firewall.
S 014-008
(6)
Remove the cover plate:
(a)
Remove the sealant from the edges of the cover plate.
(b)
Remove the mounting screws and remove the cover plate.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 024-010
(7)
Remove the self-sealing disconnect:
(a)
Remove the sealant from the mounting bolts and the edges of the mounting flange.
(b)
Remove the bolts and remove the self-sealing disconnect.
TASK 29-11-32-404-025
3. Supply Hose Self-Sealing Disconnect Installation (Fig. 401)________________________________________________
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