28-13-05
ALL ú ú 04 Page 401 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
[2] SURGE TANK ACCESS DOOR SEE
FWD
SURGE TANK ACCESS DOOR
Wing Surge Tank Pressure Relief Valve Installation
Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-13-05
ALL ú ú 03 Page 402 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
L46265
A
747-400
MAINTENANCE MANUAL
OF THE ACCESS DOOR FOR AN ELECTRICAL SURFACE BOND (SWPM 20-20-20).
Wing Surge Tank Pressure Relief Valve Installation Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-13-05
ALL ú ú 01 Page 403 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
B. Consumable Materials
(1)
C00064 Coating - Alodine 600 Chemical conversion coating for aluminum or aluminum alloys, (MIL-C-5541)
(2)
C00307 Corrosion Resistant Finish - BMS 10-20 Type II
(3)
D00128 Petrolatum - Technical, VV-P-236
C.
Parts
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 | Pressure Relief Valve | 28-11-02 | 08 | 30 | | | 2 | Packing | | | 35 | 2......…........…...................................…..........….....….........1
D. References
(1)
AIPC 28-11-02 Fig. 8
(2)
AMM 28-11-00/801, Fuel Tank Repair
(3)
AMM 28-11-03/401, Wing Surge Tank Access Door
(4)
AMM 51-21-04/701, Alodine Coating
(5)
SWPM 20-20-00, Electrical Ground and Bond
E.
Access
(1)
Location Zones 555 Surge Tank, Front Spar to Rear Spar, Left 655 Surge Tank, Front Spar to Rear Spar, Right
(2)
Access Panels
555AB Surge Tank Access Door
655AB Surge Tank Access Door
F.
Procedure
S 034-015
WARNING:_______KEEP YOUR FINGERS AWAY FROM THE POPPET SPRING (VIEW A-A). THE
SPRING FORCE IS EXTREMELY STRONG AND CAN CAUSE INJURY TO YOUR
FINGERS.
(1) Keep your fingers away from the poppet spring when you do maintenance on the pressure relief valve.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-13-05
ALL ú ú 04 Page 404 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
(2) S 214-006Prepare the mating surfaces of the pressure relief valve (1) and the access door (3) for a faying surface bond (SWPM 20-20-00) (View A).
(3) S 434-007Install the new packing (2) on the pressure relief valve (1).
NOTE:____ Lubricate the packing with a thin coating of petrolatum.
(4) S 424-008Put the pressure relief valve (1) into the position on the access door (3).
(5) S 434-009Install and tighten the mounting bolts (4) (8 locations) that attach the valve to the access door (3).
(6) S 284-012Do these two bonding resistance checks (SWPM 20-20-00) (View A-A): (a) Measure the bonding resistance between the valve body and the access door.
NOTE:____ The bonding resistance must not be more than 0.010 ohm.
(b) Measure the bonding resistance between the valve poppet face and the access door.
NOTE:____ The bonding resistance must not be more than 1.00 ohm.
(7) S 624-016Apply these protective finishes to any exposed areas on the access door (3) at the mating surface of the valve body (1): (a) Alodine 600 (AMM 51-21-04/701).
中國航空網(wǎng) www.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) 燃油 FUEL 1(150)
