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

(8)  
For the area in the No. 2 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 on the right wing (AMM 28-11-11/401).

(b)  
Go into the opening for access panel No. 8 (AMM 28-10-0/201).

(c)  
Do this task for all bonding jumpers between rib No. 12 and rib No. 13: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48406 for bonding jumper locations.

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

500
Sep 01/02 28-00 Page 207

(9)  
For the area in the No. 2 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 on the right wing (AMM 28-11-11/401).

(b)  
Go into the opening for access panel No. 9 (AMM 28-10-0/201).

(c)  
Do this task for all bonding jumpers between rib No. 13 and rib No. 14: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48406 for bonding jumper locations.

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

(10)
For the area in the No. 2 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 on the right wing (AMM 28-11-11/401).

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

(c)  
Do this task for all bonding jumpers between rib No. 14 and rib No. 15: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48406 for bonding jumper locations.

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

(11)
For the area in the No. 2 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 on the right 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 bonding jumpers between rib No. 15 and rib No. 16: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48406 for bonding jumper 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. 2 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 right 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 bonding jumpers between rib No. 16 and rib No. 17: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48406 for bonding jumper locations.

(d)  
If access is not necessary for subsequent tasks, install access panel No. 12   (AMM 28-11-11/401).

500 28-00    Sep 01/02 Page 208

6.  Fuel System Static Ground Path, Center Tank - Inspection
A.  References
(1)  
AMM 28-10-0/201, Fuel Tanks

(2)  
AMM 28-11-31/401, Integral Center Tank Access Panel

(3)  
DWG 65-48411, WING CENTER SECTION STA 540 - 663.76

B.  Procedure
(1)  For the center fuel tank, do these steps:
(a)  
Remove the access panel for the center tank (AMM 28-11-31/401).

(b)  
Go into the center tank (AMM 28-10-0/201).

(c)  
Do this task for all bonding jumpers in the center tank: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48411 for bonding jumper locations.

7.  Fuel System Fault Current, No. 1 Tank - Inspection
A.  References
(1)  
AMM 27-81-0/201, Leading Edge Flaps and Slats

(2)  
SWPM 20-20-00, Electrical Bonds and Grounds

B.  Procedure
(1)
Do these steps to do an inspection of the left boost pump for the center tank:

(a)  
Remove the access panel 7201 in the bottom wing skin to get access to the left boost pump for the center tank.

(b)  
Do a check of the electrical bond between the left fuel boost pump for the center tank and the airplane structure (SWPM 20-20-00). 1) Make sure the resistance is not more than 0.0002 ohm.
　
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