(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).
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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)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 燃油 FUEL 1(12)
