(b)
Make sure the resistance is not more than 0.10 ohms.
TASK 28-00-00-282-029
4. Fuel System Static Bond Path, No. 1 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 65-48403, L.H. INBD. INSPAR AREA, W.B.L. 72.24 - 227
(4)
DWG 65-48405, L.H. OUTBD. INSPAR AREA, W.B.L. 227 TO TIP
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28-00-00
ALL ú ú 01 Page 206 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
B. Access
(1) Location Zones
305 Left Fuel Tank
C. Procedure (Fig. 201)
S 282-032
(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 bonding jumpers between rib No. 1 and rib No. 5: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48403 for bonding jumper locations.
(d)
If access is not necessary for subsequent tasks, install access panel No. 1 (AMM 28-11-11/401).
S 282-033
(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 bonding jumpers between rib No. 5 and rib No. 7: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48403 for bonding jumper locations.
(d)
If access is not necessary for subsequent tasks, install access panel No. 2 (AMM 28-11-11/401).
S 282-034
(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 bonding jumpers between rib No. 7 and rib No. 8: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48403 for bonding jumper locations.
(d)
If access is not necessary for subsequent tasks, install access panel No. 3 (AMM 28-11-11/401).
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28-00-00
ALL ú ú 01 Page 207 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 282-035
(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 bonding jumpers between rib No. 8 and rib No. 9: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48405 for bonding jumper locations.
(d)
If access is not necessary for subsequent tasks, install access panel No. 4 (AMM 28-11-11/401).
S 282-036
(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).
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