(3)
Mallet - rubber
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28-11-11
ALL ú ú 02 Page 401 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
WING CENTER SECTION ACCESS PANEL
NO. 2 NO. 3 SEE A
NO. 5
NO. 7
NO. 9
NO. 11
NO. 12 NO. 14 NO. 13
(AIR VENT SCOOP) BOOST PUMP
SEE B
ACCESS PANEL NO. 1
FWD NO. 1
BOOST PUMP
INBD SEE C ACCESS PANEL NO. 4 NO. 6
NO. 2
NO. 8 NO. 10
SEE C SURGE
SEE D TANK
TANK NO. 2 SHOWN, TANK NO. 1 OPPOSITE
A
ACCESS DOOR
LOWER WING SKIN
INSIDE
MOLDED RUBBER SEAL TANK
ACCESS DOOR GASKET
28-11-10
LOWER WING SKIN
GASKET (KNITTED ALUMINUM) CLAMP RING LOWER SURFACE OF THE WING SKIN
MOUNTING BOLT CLAMP RING (23 LOCATIONS)
MIL-G-25537 MOUNTING BOLT (23 LOCATIONS)
CROSS SECTION OF THE A MAIN TANK ACCESS DOOR A-A
A
APPLY A THIN LAYER (APPROXIMATELY 0.010 TO 0.015 INCH) OF GREASE TO THE LOWER SURFACE OF THE WING SKIN THAT TOUCHES THE ALUMINUM GASKET. (REFER TO THE TEXT)
Fuel Tank Access Panel Installation Figure 401 (Sheet 1)
E35460
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-11-11
ALL ú ú 02 Page 402 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
WING LOWER SKIN
MOUNTING SCREW (17 LOCATIONS)
AIR VENT SCOOP ACCESS PANEL (NO. 14)
Fuel Tank Access Panel Installation
Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-11-11
ALL ú ú 01 Page 403 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
ACCESS DOOR LOWER WING SKIN
ALUMINUM) (KNITTED GASKET
FWD NO. 1, NO. 2, NO. 6, NO. 8 MOUNTING BOLT (23 LOCATIONS) RING CLAMP
C
ACCESS DOOR
LOWER WING SKIN
GASKET (KNITTED ALUMINUM)
FWD CLAMP RING
NO. 10
MOUNTING BOLT (21 LOCATIONS)
D
Main Tank Access Door Installation Figure 401 (Sheet 3)
E35771
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-11-11
ALL ú ú 01 Page 404 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
LOWER WING SKIN
Identification of Impact Resistant Access Doors
Figure 402
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28-11-11
("IMPACT RESISTANT DOOR" STENCIL) ú ú 02 Page 405 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E55033
A 737-300/400/500MAINTENANCE MANUAL
FWD
7 3 1 5 9
10 6 2 4 8
LOWER WING SKIN
NOTE: TORQUE THE MOUNT BOLTS IN THE SEQUENCE SHOWN BY THE NUMBERS. THIS WILL MAKE SURE FUEL DOES NOT LEAK AROUND THE ACCESS PANEL.
Access Panel Mount Bolt Torque Pattern
Figure 403
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú 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(112)
