locations.

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

 S 286-013
 (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 FQIS wiring and components between rib No. 16 and rib No. 17: 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. 12 (AMM 28-11-11/401).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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A
737-300/400/500MAINTENANCE MANUAL
 TASK 28-41-44-286-014
 4.  FQIS, 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 65-48304 Wire Bundle Instl - Sec. 20, RH Inboard Inspar, WBL

 71.24 - WBL 227.

 (4)  
DWG 65-48306 Wire Bundle Instl - Sec 20 RH Inspar WBL 227 to Wingtip

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

 C. Procedure
 S 286-015
 (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).

 (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 65-48304 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 286-016
 (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 FQIS wiring and components between rib No. 5 and rib No. 7: FQIS Wiring and Component Visual Inspection. 1) Refer to drawing 65-48304 for wiring and component

 locations.

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

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-41-44
 ALL  ú ú 01 Page 608 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 286-017
 (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 FQIS wiring and components between rib No. 7 and rib No. 8: FQIS Wiring and Component Visual Inspection. 1) Refer to drawing 65-48304 for wiring and component

 locations.

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

 S 286-018
 (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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