(b)
Go into the opening for access panel No. 6 (AMM 28-10-00/201).
(c)
Do this task for all FQIS wiring and components between rib No. 10 and rib No. 11: 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. 6 (AMM 28-11-11/401).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-41-44
ALL ú ú 01 Page 605 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 286-008
(7) For the area in the No. 1 fuel tank between rib No. 11 (rib at WBL 304.50) and rib No. 12 (rib at WBL 329.75), do these steps:
(a)
Remove access panel No. 7 (7209) on the left wing
(AMM 28-11-11/401).
(b)
Go into the opening for access panel No. 7 (AMM 28-10-00/201).
(c)
Do this task for all FQIS wiring and components between rib No. 11 and rib No. 12: 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. 7 (AMM 28-11-11/401).
S 286-009
(8) For the area in the No. 1 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 (7210) on the left wing
(AMM 28-11-11/401).
(b)
Go into the opening for access panel No. 8 (AMM 28-10-00/201).
(c)
Do this task for all FQIS wiring and components between rib No. 12 and rib No. 13: 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. 8 (AMM 28-11-11/401).
S 286-010
(9) For the area in the No. 1 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 (7211) on the left wing
(AMM 28-11-11/401).
(b)
Go into the opening for access panel No. 9 (AMM 28-10-00/201).
(c)
Do this task for all FQIS wiring and components between rib No. 13 and rib No. 14: 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. 9 (AMM 28-11-11/401).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-41-44
ALL ú ú 01 Page 606 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 286-011
(10) For the area in the No. 1 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 (7212) on the left wing
(AMM 28-11-11/401).
(b)
Go into the opening for access panel No. 10 (AMM 28-10-00/201).
(c)
Do this task for all FQIS wiring and components between rib No. 14 and rib No. 15: 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. 10 (AMM 28-11-11/401).
S 286-012
(11) For the area in the No. 1 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 (7213) on the left wing
(AMM 28-11-11/401).
(b)
Go into the opening for access panel No. 11 (AMM 28-10-00/201).
(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
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