(2)
A00249 - sealant, BMS 5-26 Type II
C. References
(1)
AMM 27-81-00/201, Leading Edge Flaps
(2)
AMM 28-10-00/201, Fuel Storage
(3)
AMM 28-41-00/501, Fuel Quantity Indicating System
(4)
AMM 28-41-02/501, Fuel Quantity Indicating System
(5)
AMM 28-41-41/401, Tank and Compensator Unit Bussing Plug
(6)
AMM 51-31-00/201, Sealants
(7)
SWPM 20-10-11, Installation of Electrical Wires and Wire Harnesses
(8)
SWPM 20-10-12, Wire Harness Supports
(9)
SWPM 28-10-19, Wire Separation
(10)
DWG 65-48311 Wire Bundle Installation Wing Center Section STA 540-663.75
(11)
DWG 65-48303 Wire Bundle Instl - Sec. 20, LH Inboard Inspar WBL
71.24 to WBL 227
(12)
DWG 65-48304 Wire Bundle Instl - Sec. 20, RH Inboard Inspar, WBL
71.24 - WBL 227.
(13)
DWG 65-48305 Wire Bundle Instl - Sec 20 LH Inspar WBL 227 to Wingtip
(14)
DWG 65-48306 Wire Bundle Instl - Sec 20 RH Inspar WBL 227 to Wingtip
D. Access
(1)
Location Zones
221 Center Section Fuel Tank
305 Left Fuel Tank
405 Right Fuel Tank
(2)
Access Panels
7202 Fuel Tank Access Door
7402 Fuel Tank Access Door
E. Procedure
S 864-002
(1) Open these circuit breakers and attach DO-NOT-ClOSE tags:
(a) P6 Main Power Distribution Panel
1) EP GND FUELING
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-41-44
ALL ú ú 02 Page 401 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
2) QTY
S 864-030
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LE AND TE
_______ FLAPS AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAPS. THE FLAPS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) If you are scheduled to replace the wire bundle for the receptacle in the No. 1 tank or the No. 2 tank, extend the leading edge flaps (AMM 27-81-00/201).
S 494-004
WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO
_______ INSTALL THE LE FLAP SAFETY LOCKS. THE LE FLAPS CAN MOVE QUICKLY IF YOU DO NOT INSTALL THE SAFETY LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(3) If you are scheduled to replace the wire bundle in the No. 1 tank or the No. 2 tank, install the flap locks on the leading edge flaps (AMM 27-81-00/201).
S 654-005
WARNING: YOU MUST CAREFULLY DO ALL OF THE SAFETY PROCEDURES TO PREPARE
_______ TO GO INTO THE APPLICABLE TANK. AN EXPLOSION, BAD INJURY TO PERSONS, AND DAMAGE TO EQUIPMENT CAN OCCUR.
(4)
Do this task: "Fuel Tank Purging and Entry" for the applicable fuel tank (AMM 28-10-00/201).
S 014-006
(5)
Remove the bussing plug for the tank unit and the compensator unit (AMM 28-41-41/401).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 燃油 FUEL 3(122)
