737-300 400 500 AMM 飞机维护手册 发动机控制 ENGINE CONTROLS(68)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

(b)  ON ENGINE NO. 2; Do the steps that follow: 1) Put the terminals of the ESS2A and the ESS2B cables in the
 quadrant grooves.
 2)  Connect the push-pull cable to the quadrant with the retainer pin, the cable retainer, the bushing, the washer and the nut.
 S 824-017-C00
 (6)  
Adjust the start control cables (AMM 76-11-00/501).

 S 824-018-C00

 (7)  
Adjust the start control push-pull cable (AMM 76-11-00/501).

 S 414-019-C00

 (8)  
Install the access panel No. 6301 (engine No. 1) or 6401 (engine No. 2) from the upper aft surface of the nacelle strut (AMM 12-31-71/201).

 S 444-020-C00
 WARNING: REFER TO AMM 27-81-00/201 FOR THE LEADING EDGE FLAP LOCK
_______ PROCEDURE. FLAPS MOVE VERY QUICKLY AND CAN CAUSE INJURY TO PERSONS.
 (9)  
Remove the leading edge flap locks and retract the flaps (AMM 27-81-00/201).

 S 444-021-C00

 (10)
 Remove the lockpin from the control valve of the applicable thrust reverser (AMM 78-31-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-06
 ALL  ú ú C02 Page 405 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
THRUST CONTROL PUSH-PULL CABLE - REMOVAL/INSTALLATION
_____________________________________________________
 1.  General
_______
 A.  This procedure has two tasks. The first task removes the push-pull cables for the thrust control. The second task installs the push-pull cables for the thrust control.
 TASK 76-11-07-004-001-C00
 2.  Remove the Thrust Control Push-Pull Cable
_________________________________________
 A.  Equipment
 (1)  
Rig Pin - F70207-8
 Component of Rig Pin Kit F70207-93.
 Optional: MS20392-4C pin or equivalent 0.311
 (+0.000/-0.002)-inch diameter, 3-inch long rod
 or bolt

 (2)  
Rig Pin Assembly - F70207-23.
 Component of Rig Pin Kit F70207-93.
 Optional: MS20392-3C pin (or equivalent 0.248
 (+0.000/-0.002)-inch diameter, 3-inch long rod
 or bolt)

 

 B.  References
 (1)  
AMM 12-31-71/201, Wing Upper Surface Access Doors and Panels

 (2)  
AMM 12-31-91/201, Nacelle and Engine-To-Wing Access Doors and Panels

 (3)  
AMM 27-81-00/201, Leading Edge Flap and Slat Control System

 (4)  
AMM 54-32-01/401, Forward Fairing

 (5)  
AMM 71-11-02/201, Fan Cowl Panels

 (6)  
AMM 78-31-00/201, Thrust Reverser System

 C.  Access
 (1)  
Location Zones
 5700, Engine No. 1 (Left)
 5800, Engine No. 2 (Right)

 (2)  
Access Panels
 5726L, Strut Access Door, Eng. No. 1 - left
 5727L, Strut Access Door, Eng. No. 1 - top
 5728L, Strut Access Door, Eng. No. 1 - top
 5729L, Strut Access Door, Eng. No. 1 - top
 5731L, Strut Access Door, Eng. No. 1 - right
 5746L, Fan Cowl Panel, Eng. No. 1 - left
 5826R, Strut Access Door, Eng. No. 2 - left
 5827R, Strut Access Door, Eng. No. 2 - top
 5828R, Strut Access Door, Eng. No. 2 - top
 5829R, Strut Access Door, Eng. No. 2 - top
 5831R, Strut Access Door, Eng. No. 2 - right
 5846R, Fan Cowl Panel, Eng. No. 2 - right

 

 D.  Remove the thrust control push-pull cable (Fig. 401).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-07
 ALL  ú ú C01 Page 401 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
SEE C
THRUST CONTROL CABLE STRUT ACCESS PANELS
1
CLAMP
SEE C
1
CLAMP THRUST
SEE B BLOCKS
CONTROL
　
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 发动机控制 ENGINE CONTROLS(68)