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 28-41-44
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 ú  01  Page 603
 ú  Jul 12/01 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
M10408
A
737-300/400/500MAINTENANCE MANUAL
 C. Procedure
 S 286-002
 (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 FQIS wiring and components between rib No. 1 and rib No. 5: FQIS Wiring and Component Visual Inspection. 1) Refer to drawing 65-48303 for wiring and component

 locations.

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

 S 286-003
 (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 FQIS wiring and components between rib No. 5 and rib No. 7: FQIS Wiring and Component Visual Inspection. 1) Refer to drawing 65-48303 for wiring and component

 locations.

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

 S 286-004
 (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 FQIS wiring and components between rib No. 7 and rib No. 8: FQIS Wiring and Component Visual Inspection. 1) Refer to drawing 65-48303 for wiring and component

 locations.

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

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-41-44
 ALL  ú ú 01 Page 604 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 286-005
 (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 FQIS wiring and components between rib No. 8 and rib No. 9: 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. 4 (AMM 28-11-11/401).

 S 286-006
 (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).

 (c)  
Do this task for all FQIS wiring and components between rib No. 9 and rib No. 10: 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. 5 (AMM 28-11-11/401).

 S 286-007
 (6)  For the area in the No. 1 fuel tank between rib No. 10 (rib at WBL 279.25) and rib No. 11 (rib at WBL 304.50), do these steps:
 (a)  
Remove access panel No. 6 (7208) on the left wing
　
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