(b)
Go into the opening for access panel No. 11 (AMM 28-10-00/201).
(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 65-48405 for bonding jumper locations.
(d)
If access is not necessary for subsequent tasks, install access panel No. 11 (AMM 28-11-11/401).
S 282-043
(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 bonding jumpers between rib No. 16 and rib No. 17: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48405 for bonding jumper locations.
(d)
If access is not necessary for subsequent tasks, install access panel No. 12 (AMM 28-11-11/401).
TASK 28-00-00-282-044
5. Fuel System Static Bond Path, 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 65-48404, R.H. INBD. INSPAR AREA, W.B.L. 72.24 - 227
(4)
DWG 65-48406, R.H. OUTBD. INSPAR AREA, W.B.L. 227 TO TIP
B. Access
(1) Location Zones
405 Right Fuel Tank
C. Procedure (Fig. 201)
S 282-045
(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).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-00-00
ALL ú ú 01 Page 210 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
(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 65-48404 for bonding jumper locations.
(d)
If access is not necessary for subsequent tasks, install access panel No. 1 (AMM 28-11-11/401).
S 282-046
(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 bonding jumpers between rib No. 5 and rib No. 7: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48404 for bonding jumper locations.
(d)
If access is not necessary for subsequent tasks, install access panel No. 2 (AMM 28-11-11/401).
S 282-047
(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 bonding jumpers between rib No. 7 and rib No. 8: Inspection of the Electrical Bonding Jumpers in the Fuel System. 1) Refer to drawing 65-48404 for bonding jumper locations.
(d)
If access is not necessary for subsequent tasks, install access panel No. 3 (AMM 28-11-11/401).
S 282-048
(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).
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 燃油 FUEL 1(10)