(2)
25-51-25/401, Aft Cargo Loader Telescoping Baggage Modules

 B. Access
 (1)  
Location Zones
 153 Aft Cargo Compartment (Left)
 154 Aft Cargo Compartment (Right)

 (2)  
Access Panel
 822 No. 2 Cargo Door

 C. Procedure
 S 424-006
 (1)
Put the tracks in position and install the fasteners.

 (2)
For the floor roller tracks, install the track retainers.

 S 434-007
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THE CARGO LOADER SYSTEM ú

 25-51-24
 ú ú 03 Page 402 ú Sep 20/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 (3)  S 414-008Install the modules (Ref 25-51-25).
 (4)  S 864-009Supply electrical power (Ref 24-22-00).
 (5)  S 864-010Hold the cargo loader control switch in the LOAD position until modules are fully extended.
 (6)  S 754-011Make sure the modules move smoothly. Make sure the modules do not make too much noise when the modules move. Make sure the modules do not shake when the modules move.
 (7)  S 864-012Hold the cargo loader control switch in the UNLOAD position until modules are fully retracted.
 (8)  S 754-013Make sure the modules move smoothly. Make sure the modules do not make too much noise when the modules move. Make sure the modules do not shake when the modules move.
 (9)  S 864-014Remove electrical power if it is not necessary (Ref 24-22-00).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THE CARGO LOADER SYSTEM ú

 25-51-24
 ú ú 03 Page 403 ú Sep 20/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 AFT CARGO LOADER TELESCOPING BAGGAGE MODULES - REMOVAL/INSTALLATION
___________________________________________________________________
 1.  General
_______
 A.  This procedure contains two tasks. The first task is the instructions to remove the baggage modules from the aft cargo compartment. The second task is the instructions to install the baggage modules into the aft cargo compartment.
 TASK 25-51-25-004-001
 2.  Remove the Baggage Modules (Fig. 401)
__________________________
 A.  References
 (1)  
24-22-00/201, Electrical Power - Control

 (2)  
25-51-00/201, Cargo Loader Systems

 (3)  
25-51-00/501, Cargo Loader Systems

 (4)  
25-51-23/401, Aft Cargo Loader Rollers

 B.  Access
 (1)  
Location Zones
 153 Aft Cargo Compartment (Left)
 154 Aft Cargo Compartment (Right)

 (2)  
Access Panel
 822 No. 2 Cargo Door

 C.  Procedure
 S 864-002
 (1)  Put the CARGO LOADER CONTROL SWITCH in the LOAD position until the modules are fully extended.
 NOTE: For an inoperative cargo loader, do the Deactivate the Cargo
____ Loader procedure (Ref 25-51-00/201).
 S 864-003
 (2)  
Open this circuit breaker on the APU external power panel, P34, and attach a DO-NOT-CLOSE tag:

 (a)  34B16, AFT CARGO LOADER DRIVE

 (3)  
Remove electrical power (Ref 24-22-00).

 S 034-005

 (4)  
Remove the ball lockpins to disconnect module 2 from the drive screw.

 S 864-004
 NOTE: If the cargo loader is deactivated, this will separate
____
 module 2 from the pin block.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THE CARGO LOADER SYSTEM ú

 25-51-25
 ú ú 03 Page 401 ú Sep 20/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 EQUIPMENT/FURNISHINGS 2(59)