(a)  
Remove access panel No. 11 on the left wing (AMM 28-11-11/401).

(b)  
Go into the opening for access panel No. 11 (AMM 28-10-0/201).

(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 locations.

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

(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 on the left wing (AMM 28-11-11/401).

(b)  
Go into the opening for access panel No. 12 (AMM 28-10-0/201).

(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).

Sep 01/02 28-41-101 Page 603

4.  FQIS, No. 2 Tank - Inspection
A.  References
(1)  
AMM 28-10-0/201, 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 to WBL 227

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

B.  Procedure
(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 (rib at WBL 157.00), do these steps:

(a)  
Remove access panel No. 1 on the right wing (AMM 28-11-11/401).

(b)  
Go into the opening for access panel No. 1 (AMM 28-10-0/201).

(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).

(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 on the right wing (AMM 28-11-11/401).

(b)  
Go into the opening for access panel No. 2 (AMM 28-10-0/201).

(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).

28-41-101 Sep 01/02 Page 604

(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 on the right wing (AMM 28-11-11/401).

(b)  
Go into the opening for access panel No. 3 (AMM 28-10-0/201).

(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).

(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 on the right wing (AMM 28-11-11/401).

(b)  
Go into the opening for access panel No. 4 (AMM 28-10-0/201).

(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).

(5)  
For the area in the No. 2 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 on the right wing (AMM 28-11-11/401).

(b)  
Go into the opening for access panel No. 5 (AMM 28-10-0/201).

(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.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737 AMM 飛機(jī)維護(hù)手冊 燃油 FUEL(185)