(d)  
If access is not necessary for subsequent tasks, install access panel No. 9 (AMM 28-11-11/401).

 S 282-054
 (10) For the area in the No. 2 fuel tank between rib No. 14 (rib at WS 453.00) and rib No. 15 (rib at WS 479.00), do these steps:
 (a)  
Remove access panel No. 10 (7412) on the right wing
 (AMM 28-11-11/401).

 (b)  
Go into the opening for access panel No. 10 (AMM 28-10-00/201).

 (c)  
Do this task for all bonding jumpers between rib No. 14 and rib No. 15: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48406 for bonding jumper locations.

 (d)  
If access is not necessary for subsequent tasks, install access panel No. 10 (AMM 28-11-11/401).

 S 282-055
 (11) For the area in the No. 2 fuel tank between rib No. 15 (rib at WS 479.00) and rib No. 16 (rib at WS 505.00), do these steps:
 (a)  
Remove access panel No. 11 (7413) on the right wing
 (AMM 28-11-11/401).

 (b)  
Go into the opening for access panel No. 11 (AMM 28-10-00/201).

 (c)  
Do this task for all bonding jumpers between rib No. 15 and rib No. 16: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48406 for bonding jumper locations.

 (d)  
If access is not necessary for subsequent tasks, install access panel No. 11 (AMM 28-11-11/401).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 28-00-00
 ALL  ú ú 01 Page 213 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 282-056
 (12) For the area in the No. 2 fuel tank between rib No. 16 (rib at WS 505.00) and rib No. 17 (rib at WS 531.00), do these steps:
 (a)  
Remove access panel No. 12 (7414) on the right wing (AMM 28-11-11/401).

 (b)  
Go into the opening for access panel No. 12 (AMM 28-10-00/201).

 (c)  
Do this task for all bonding jumpers between rib No. 16 and rib No. 17: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48406 for bonding jumper locations.

 (d)  
If access is not necessary for subsequent tasks, install access panel No. 12 (AMM 28-11-11/401).

 TASK 28-00-00-282-057
 6.  Fuel System Static Bond Path, Center Tank - Inspection______________________________________________________
 A. References
 (1)  
AMM 28-10-00/201, Fuel Tanks

 (2)  
AMM 28-11-31/401, Center Tank Access Panel

 (3)  
DWG 65-48411, WING CENTER SECTION STA 540 - 663.76

 B. Access
 (1)  
Location Zones
 221 Center Section Fuel Tank

 (2)  
Access Panels
 3303 A/C Access Panel
 3304 A/C Access Panel

 C. Procedure
 S 282-058
 (1)  For the center fuel tank, do these steps:
 (a)  
Remove access panel for the center tank (AMM 28-11-31/401).

 (b)  
Go into the center tank (AMM 28-10-00/201).

 (c)  
Do this task for all bonding jumpers in the center tank: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48411 for bonding jumper locations.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 28-00-00
 ALL  ú ú 01 Page 214 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (d)  If access is not necessary for subsequent tasks, install the access panel for the the center tank (AMM 28-11-31/401).
 TASK 28-00-00-282-059
 7.  Fuel System Fault Current, No. 1 Tank - Inspection__________________________________________________
 A. References
 (1)  
AMM 27-81-00/201, Leading Edge Flap and Slat Control System

 (2)  
SWPM 20-20-00, Standard Wiring Practices Manual

 B. Access
 (1)  
　
中國航空網 m.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(12)