(b)  
Make sure the resistance is not more than 0.10 ohms.

 TASK 28-00-00-282-029
 4.  Fuel System Static Bond Path, No. 1 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 65-48403, L.H. INBD. INSPAR AREA, W.B.L. 72.24 - 227

 (4)  
DWG 65-48405, L.H. OUTBD. INSPAR AREA, W.B.L. 227 TO TIP

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 B. Access
 (1)  Location Zones
 305 Left Fuel Tank

 C. Procedure (Fig. 201)
 S 282-032
 (1)  For the area in the No. 1 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 (7202) on the left wing (AMM 28-11-11/401).

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

 (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 65-48403 for bonding jumper locations.

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

 S 282-033
 (2)  For the area in the No. 1 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 (7204) on the left 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 65-48403 for bonding jumper locations.

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

 S 282-034
 (3)  For the area in the No. 1 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 (7205) on the left 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 65-48403 for bonding jumper locations.

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

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 282-035
 (4)  For the area in the No. 1 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 (7206) on the left wing
 (AMM 28-11-11/401).

 (b)  
Go into the opening for access panel No. 4 (AMM 28-10-00/201).

 (c)  
Do this task for all bonding jumpers between rib No. 8 and rib No. 9: 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. 4 (AMM 28-11-11/401).

 S 282-036
 (5)  For the area in the No. 1 fuel tank between rib No. 9 (rib at WBL 254.00) and rib No. 10 (rib at WBL 279.25), do these steps:
 (a)  
Remove access panel No. 5 (7207) on the left wing
 (AMM 28-11-11/401).

 (b)  
Go into the opening for access panel No. 5 (AMM 28-10-00/201).
　
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