• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-08 12:04来源:蓝天飞行翻译 作者:航空
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

 STANDS WITHOUT A TIE ROD THROUGH THE ú CONFIG 3 SPLINE SHAFT ú C01 Page 409 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

Control Shaft Components Installation Figure 404 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS REINFORCED CONTROL ú

 76-11-02
 STANDS WITHOUT A TIE ROD THROUGH THE ú CONFIG 3 SPLINE SHAFT ú C01 Page 410 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F14069
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
GAP LOCATION  REQUIREMENT GAP  ACTUAL MEASUREMENT  TO OBTAIN GAP REQUIREMENT ADJUSTMENT NECESSARY 
1  FLAP LEVER  0.060 MIN  LESS THAN 0.060  67RELOCATE ONE WASHER FROM TO 
2  SPEEDBRAKE LEVER  0.030-0.060  GREATER THAN 0.100  12RELOCATE THREE WASHERS FROM TO 
0.080-0.100  2 1RELOCATE TWO WASHERS FROM TO 
0.060-0.080  2 1RELOCATE ONE WASHER FROM TO 
LESS THAN 0.030  21RELOCATE ONE WASHER FROM TO 
3  THRUST LEVER ENGINE NUMBER 1  0.025-0.054  GREATER THAN 0.054  34RELOCATE ONE WASHER FROM TO 
LESS THAN 0.025  43RELOCATE ONE WASHER FROM TO 
4  ENGINE START DETENT ENGINE NUMBER 1  0.036-0.090  GREATER THAN 0.090  8ADD TWO SHIMS MAX (AS REQUIRED) AT 
LESS THAN 0.036  8REMOVE ONE SHIM AT 
5  ENGINE NUMBER 2 THRUST LEVER 0.0325-0.0540  GREATER THAN 0.0540  54RELOCATE ONE WASHER FROM TO 
LESS THAN 0.0325  45RELOCATE ONE WASHER FROM TO 
6  ENGINE NUMBER 2 ENGINE START DETENT 0.022-0.086  GREATER THAN 0.086  9ADD THREE SHIMS MAX (AS REQUIRED) AT 
LESS THAN 0.022  9REMOVE ONE SHIM AT 

CONTROL SHAFT ADJUSTMENT GAP REQUIREMENTS
TABLE A

LOCATION QUANTITY OF WASHERS/SHIMS 
MAX  MIN 
1  4  0 
2  4  0 
3  2  0 
4  4  1 
5  2  0 
6  1  0 
7  1  0 
8  3  0 
9  4  0 

CONTROL SHAFT ADJUSTMENT SHIM REQUIREMENTS
TABLE B

Control Shaft Components Installation
Figure 404 (Sheet 4)

F14071
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS REINFORCED CONTROL ú

 76-11-02
 STANDS WITHOUT A TIE ROD THROUGH THE ú CONFIG 3 SPLINE SHAFT ú C01 Page 411 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 024-017-C03
 (2)  
Support the sprocket with one hand and remove the spline shaft, the bearings, and the spacers from the left end of the two hollow control shafts.

 S 864-018-C03

 (3)  
Prevent movement of the sprocket and chain in the bottom of the control stand.

 S 034-019-C03

 (4)  
Use a screwdriver with a 90 degree No. 2 Phillips bit to remove the aft screw for the chain guard.


 (a)  You can get access to the aft screw of the chain guard through the hole for the stabilizer trim cutout switch.
 S 034-020-C03
 (5)  Remove the two screws from the chain guard.
 (a)  You can get access to the remaining two screws of the chain guard through the side of the control stand.
 S 024-021-C03
 (6)  
Cut the safety wire on the nylon flap lever cam.

 S 024-022-C03

 (7)  
Remove the nylon flap lever cam.

 S 024-023-C03

 (8)  
Remove the chain guard.


 G.  Remove the Short Control Shaft, the Flap Lever, and the Stabilizer Trim Indicator Crank.
 S 024-024-C03
 (1)  
Use the lockwasher removal tool to straighten the crimped tab on the cup washer for the short control shaft.
 
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(46)