• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-03 11:28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

 S 034-004

 (3)  
Disconnect the electrical connector from the actuator.

 (4)  
Install a cap on the electrical connector.

 S 034-005

 (5)  
Remove the nuts, washers and bolts that connect the pushrod bearings to the actuator arms.


 S 434-019
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-15-31
 ALL  ú ú 01 Page 401 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES /MAINTENANCE MANUAL ////////////////////////
SEE  B 
SEE  A 
AIR 
DIFFUSER  FWD
DUCT 
AIR INLET 
A  DOOR 
PRESSURE 
BULKHEAD 
AIR INLET 
DOOR 
AIR 
DIFFUSER 
DUCT 

PUSHROD
FWD
ACTUATOR ARM OUTPUT SHAFT
ACTUATOR
SEE C
B

Inlet Door Actuator Installation Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-15-31
 ALL  ú ú 02 Page 402 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
WASHER  BOLT  MOUNTING BRACKET  MOUNTING BOLT (2 LOCATIONS) 
PUSHROD 
BOLT DOOR SWITCH INLET 
NUT 
FWD 
PUSHROD BEARING  ACTUATOR ARM SEE D ACTUATOR C  CONNECTOR ELECTRICAL  INBD 
ACTUATOR ARM (DOOR CLOSED POSITION)  SHAFT FOR THE OUTPUT PUNCH MARK 
ACTUATOR CENTERLINE
ACTUATOR ARM POSITION) (DOOR OPEN Figure 401 (Sheet 2) Inlet Door Actuator Installation FWD D  ACTUATOR 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-15-31
 ALL  ú ú 01 Page 403 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES/MAINTENANCE MANUAL ////////////////////////
S 024-006
 (6)  Remove the actuator:
 (a)  
Remove the nuts, washers and bolts that attach the actuator to the mounting bracket.

 (b)  
Remove the actuator and the shims, if used.


 S 034-007
 (7)  Remove the actuator arms from the actuator:
 (a)  
Remove the bolts and washers from the actuator arms.

 (b)  
Remove the actuator arms from the actuator output shaft.

 (c)  
Keep the actuator arms for the installation.


 TASK 49-15-31-404-008
 3. Air Inlet Door Actuator Installation (Fig. 401)
____________________________________
 A. References
 (1)  AMM 49-15-00/501, APU Air Inlet
 B. Access
 (1)  
Location Zones
 101 Control Cabin (Left)
 701 Tail Compartment


 (2)  
Access Panels
 3701 Stabilizer Trim Access Door

 

 C. Procedure
 S 434-010
 (1)  Install the actuator arms on the actuator:
 (a)  
Put the actuator arms on the actuator output shaft.

 (b)  
Align the punch mark on the actuator output shaft with the centerline of the actuator arms.

 (c)  
Install the bolts and the washers.

 (d)  
Tighten the bolts to 22-28 pound-inches (2.5-3.2 N.m).


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-15-31
 ALL  ú ú 01 Page 404 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(2)  S 424-012Install the actuator: (a) Put the actuator on the mounting bracket. (b) If there is not a tight fit between the actuator and the mounting bracket, add the shims as it is necessary.
 
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 AIRBORNE AUXILIARY POWER 1(139)