S 024-031
(5)
Remove the card assembly.
TASK 20-10-01-424-032
5. Install the Card Assembly
_________________________
A. Reference
(1) AMM 20-41-01/201, Electro-Static Sensitive Devices
B. Access
(1) Location Zone
100 Lower Half of Fuselage
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
20-10-01
ALL ú ú 01 Page 406 ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
C. Procedure
S 424-033
CAUTION:_______CARD ASSEMBLIES ARE STATIC SENSITIVE. TAKE THE NECESSARY PRECAUTIONS WHEN YOU ARE TO HOLD THE CARD ASSEMBLIES. READ THE PROCEDURE ON HOW TO HOLD ELECTROSTATIC-DISCHARGE SENSITIVE DEVICES (AMM 20-41-01/201). THE CARD ASSEMBLIES CONTAIN DEVICES THAT CAN BE DAMAGED BY STATIC DISCHARGE.
(1)
Install the card assembly in the guides. Carefully push the card in until the card is tightly engaged in the electrical connector.
S 214-034
(2)
Make sure that the ejectors are level against the card.
S 864-035
(3)
Close the applicable circuit breakers.
S 414-036
(4)
Close the card file door.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
20-10-01
ALL ú ú 01 Page 407 ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
BEARINGS AND BUSHINGS - REMOVAL/INSTALLATION
____________________________________________
TASK 20-10-02-904-003
1. Bearings and Bushings - Removal/Installation____________________________________________
A. Procedure
S 904-004
(1) For the removal and installation of bearings and bushings (SOPM 20-50-03).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
20-10-02
ALL ú ú 01 Page 401 ú Jan 20/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
CONTROL CABLES - REMOVAL/INSTALLATION
_____________________________________
1. General_______
A. This procedure contains two tasks. The first task is the removal of control cables. The second task is the installation of control cables.
B. This procedure includes instructions for prefabricated and not prefabricated cables to make installation easier when portable swaging machines are available.
C. If this procedure does not agree with specified maintenance procedures, use the specified maintenance procedure.
D. The maintenance manual location for control cable fabrication data is found in Table I
~.......................................................... | TABLE I | ............................................................ | CABLE | MM LOCATION | ............................................................ |*[1] ENGINE THRUST CONTROL | 76-11-03-2 | | | | | FLIGHT CONTROLS | | | - AILERON | 27-00-01-2 | | - ELEVATOR | 27-00-01-2 | | - FLAP/SLAT | 27-00-01-2 | | - RUDDER | 27-00-01-2 | | - STABILIZER TRIM | 27-00-01-2 | | | | | LANDING GEAR | | | - ALTERNATE EXTENSION | 32-00-05-2 | | - BRAKES | 32-00-05-2 | | - DOOR GROUND RELEASE | 32-00-05-2 | | - EXTENSION/RETRACTION | 32-00-05-2 | | - NOSE WHEEL STEERING | 32-00-05-2 | | | | 2........................................….................1
*[1] For engines that are not FADEC.
TASK 20-10-03-004-001
2. Remove Control Cables (Fig. 401)_____________________
A. Equipment
(1) Cable Clamps - A20005-9
B. Consumable Materials
(1) G00270 Tape - Masking
C. References
(1)
AMM 20-10-04/401, Control Cable Air Seal
(2)
AMM 20-10-05/401, Clips - Turnbuckle Locking
(3)
AMM 20-10-07/401, Control Cable Pulleys
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：757 AMM 飞机维护手册 STANDARD PRACTICES - AIRFRAME(5)
