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时间:2011-04-02 05:47来源:蓝天飞行翻译 作者:航空
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 S 282-042
 (11) For the area in the No. 1 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 (7213) on the left 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 65-48405 for bonding jumper locations.

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


 S 282-043
 (12) For the area in the No. 1 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 (7214) on the left 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 65-48405 for bonding jumper locations.

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


 TASK 28-00-00-282-044
 5. Fuel System Static Bond Path, No. 2 Tank - Inspection
_____________________________________________________
 A. References
 (1)  
AMM 28-10-00/201, Fuel Tanks

 (2)  
AMM 28-11-11/401, Wing Fuel Tank Access Panels

 (3)  
DWG 65-48404, R.H. INBD. INSPAR AREA, W.B.L. 72.24 - 227

 (4)  
DWG 65-48406, R.H. OUTBD. INSPAR AREA, W.B.L. 227 TO TIP


 B. Access
 (1)  Location Zones
 405 Right Fuel Tank

 C. Procedure (Fig. 201)
 S 282-045
 (1)  For the area in the No. 2 fuel tank between rib No. 1 (side of body rib at WBL 71.24) and rib No. 5 (at WBL 157.00), do these steps:
 (a)  
Remove access panel No. 1 (7402) on the right wing (AMM 28-11-11/401).

 (b)  
Go into the opening for access panel No. 1 (AMM 28-10-00/201).


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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (c)  
Do this task for all bonding jumpers between rib No. 1 and rib No. 5: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48404 for bonding jumper locations.

 (d)  
If access is not necessary for subsequent tasks, install access panel No. 1 (AMM 28-11-11/401).


 S 282-046
 (2)  For the area in the No. 2 fuel tank between rib No. 5 (rib at WBL 157.00) and rib No. 7 (rib at WBL 198.60), do these steps:
 (a)  
Remove access panel No. 2 (7404) on the right wing
 (AMM 28-11-11/401).


 (b)  
Go into the opening for access panel No. 2 (AMM 28-10-00/201).

 (c)  
Do this task for all bonding jumpers between rib No. 5 and rib No. 7: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48404 for bonding jumper locations.

 (d)  
If access is not necessary for subsequent tasks, install access panel No. 2 (AMM 28-11-11/401).


 S 282-047
 (3)  For the area in the No. 2 fuel tank between rib No. 7 (rib at WBL 198.60) and rib No. 8 (rib at WBL 227.00), do these steps:
 (a)  
Remove access panel No. 3 (7405) on the right wing
 (AMM 28-11-11/401).


 (b)  
Go into the opening for access panel No. 3 (AMM 28-10-00/201).

 (c)  
Do this task for all bonding jumpers between rib No. 7 and rib No. 8: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48404 for bonding jumper locations.

 (d)  
If access is not necessary for subsequent tasks, install access panel No. 3 (AMM 28-11-11/401).


 S 282-048
 (4)  For the area in the No. 2 fuel tank between rib No. 8 (rib at WBL 227.00) and rib No. 9 (rib at WBL 254.00), do these steps:
 (a)  
Remove access panel No. 4 (7406) on the right wing
 (AMM 28-11-11/401).
 
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本文链接地址:737-300 400 500 AMM 飞机维护手册 燃油 FUEL 1(10)