(b)  
Go into the opening for access panel No. 6 (AMM 28-10-00/201).

 (c)  
Do this task for all FQIS wiring and components between rib No. 10 and rib No. 11: FQIS Wiring and Component Visual Inspection. 1) Refer to drawing 65-48305 for wiring and component

 locations.

 (d)  
If access is not necessary for subsequent tasks, install access panel No. 6 (AMM 28-11-11/401).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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737-300/400/500MAINTENANCE MANUAL
 S 286-008
 (7)  For the area in the No. 1 fuel tank between rib No. 11 (rib at WBL 304.50) and rib No. 12 (rib at WBL 329.75), do these steps:
 (a)  
Remove access panel No. 7 (7209) on the left wing
 (AMM 28-11-11/401).

 (b)  
Go into the opening for access panel No. 7 (AMM 28-10-00/201).

 (c)  
Do this task for all FQIS wiring and components between rib No. 11 and rib No. 12: FQIS Wiring and Component Visual Inspection. 1) Refer to drawing 65-48305 for wiring and component

 locations.

 (d)  
If access is not necessary for subsequent tasks, install access panel No. 7 (AMM 28-11-11/401).

 S 286-009
 (8)  For the area in the No. 1 fuel tank between rib No. 12 (rib at WBL 329.75) and rib No. 13 (rib at WBL 355.00), do these steps:
 (a)  
Remove access panel No. 8 (7210) on the left wing
 (AMM 28-11-11/401).

 (b)  
Go into the opening for access panel No. 8 (AMM 28-10-00/201).

 (c)  
Do this task for all FQIS wiring and components between rib No. 12 and rib No. 13: FQIS Wiring and Component Visual Inspection. 1) Refer to drawing 65-48305 for wiring and component

 locations.

 (d)  
If access is not necessary for subsequent tasks, install access panel No. 8 (AMM 28-11-11/401).

 S 286-010
 (9)  For the area in the No. 1 fuel tank between rib No. 13 (rib at WBL 355.00) and rib No. 14 (rib at WS 453.00), do these steps:
 (a)  
Remove access panel No. 9 (7211) on the left wing
 (AMM 28-11-11/401).

 (b)  
Go into the opening for access panel No. 9 (AMM 28-10-00/201).

 (c)  
Do this task for all FQIS wiring and components between rib No. 13 and rib No. 14: FQIS Wiring and Component Visual Inspection. 1) Refer to drawing 65-48305 for wiring and component

 locations.

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

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-41-44
 ALL  ú ú 01 Page 606 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 286-011
 (10) For the area in the No. 1 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 (7212) on the left 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 FQIS wiring and components between rib No. 14 and rib No. 15: FQIS Wiring and Component Visual Inspection. 1) Refer to drawing 65-48305 for wiring and component

 locations.

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

 S 286-012
 (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 FQIS wiring and components between rib No. 15 and rib No. 16: FQIS Wiring and Component Visual Inspection. 1) Refer to drawing 65-48305 for wiring and component
　
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