28-11-00
ALL ú ú 02A Page 856 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
~.............................................................................. | TABLE I BMS 5-81 CURE RATES | ................................................................................ | | CURE CONDITIONS | | ................................................................. | | DRY HARD (HOURS) *[1] | DRY THROUGH (HOURS) *[2] | | ................................................................. | CURE | TYPE II, | TYPE II, | TYPE II, | TYPE II, | | TEMPERATURE | CLASS 1 | CLASS 2 | CLASS 1 | CLASS 2 | ................................................................................ | 75 |5°F | 50 | 8 | 96 | 24 | ................................................................................ | 100 |5°F | 18 | 2.5 | 36 | 3.5 | ................................................................................ | 125 |5°F | 7.5 | 1.5 | 15 | 2.5 | ................................................................................ | 150 |5°F | 2.5 | 1.5 | 5 | 2 | 2..............…...............…...............…...............…...............1
*[1] Condition where metal particles do not bond to the sealant.
*[2] Condition where sealant is sufficiently hard to prevent damage when
walked on with boot socks.
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28-11-00
ALL ú ú 02A Page 857 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
WING FUEL TANK ACCESS PANELS - REMOVAL/INSTALLATION
___________________________________________________
1. General_______
A. This procedure has these tasks:
(1)
The removal of access panels No. 1 thru 13.
(2)
The installation of access panels No. 1 thru 13.
(3)
The removal of access panel No. 14.
(4)
The installation of access panel No. 14.
(5)
The surge tank access door leak test
B. The access panels No. 1 thru 12 (Fig. 401) give access to the internal structure and the equipment in tanks No. 1 and No. 2.
C. Access panel No. 13 gives access to the inboard part of each surge tank and if installed, has a pressure relief valve mounted in the panel. The circular access panel No. 14 operates as the air vent scoop for the fuel vent system in each wing. Panel No. 14 also gives access to the outboard part of the surge tank in each wing.
D. The access panels No. 1 thru 13 are oblong, not circular. The installation procedure and the seals for these panels are different from those used with panel No. 14.
E. On the original design, No. 13 surge tank access doors, 10-60031, do not have a pressure relief valve installed in them. No. 14 vent scoop access doors, 65-68831, do not have a flame arrestor installed in them. These doors are replaced by SB 737-28-1026 and SB 737-28-1131.
F. The No. 14 access panels, 65C38139-1/-2, have a flame arrestor/vent scoop installed on them. The No. 13 access panels 65C15617-2 have a pressure relief valve installed on them.
G. The No. 14 surge tank access panels with the flame arrestor/vent scoop must be installed with the No. 13 surge tank access panels with the pressure relief valve. If the flame arrestor becomes clogged, and there is no pressure relief valve, the wing can be damaged by the pressure differences.
H. Remove the electrical power on the airplane before you remove an access panel.
I. Do not put back the electrical power on the airplane until the tank is closed and safe.
TASK 28-11-11-004-001
2. Access Panels 1 thru 13 Removal (Fig. 401)_______________________________
A. Equipment
(1)
Container - clean, flat, large enough to hold clamp ring and aluminum gasket
(2) 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 燃油 FUEL 1(111)
