• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-03 11:32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

 (3)  Remove the lower shroud:
 (a) Hold the lower shroud and open the shroud latches.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-52-41
 ALL  ú ú 01 Page 401 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES /MAINTENANCE MANUAL ////////////////////////
SHROUD UPPER  CONNECTOR ELECTRICAL SEE  A  FWD 
VALVE SURGE BLEED SEE B 

A  1
SHROUD UPPER 
CONNECTOR ELECTRICAL 
LOCKWIRE  PLENUM TURBINE 
VALVE SURGE BLEED SEE B  VALVE BLEED SURGE 
A  2  PACKING  SCREW WASHER 
2 1  AIRPLANES WITHOUT THE ETC AIRPLANES WITH THE ETC  B 
Surge Bleed Valve Installation Figure 401 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-52-41
 ALL  ú ú 01 Page 402 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(b)  Remove the lower shroud.
 S 024-005
 (4)  Remove the surge bleed valve:
 (a)  
Disconnect the electrical connector from the surge bleed valve.

 (b)  
Remove the two screws and the washers that attach the surge bleed valve to the turbine plenum.

 (c)  
Remove the surge bleed valve and the packing. 1) Discard the packing.


 TASK 49-52-41-404-006
 3. Surge Bleed Valve Installation (Fig. 401)
______________________________
 A. References
 (1)  IPC 49-50-00 Fig. 2
 B. Access
 (1)  
Location Zones
 101 Flight Compartment, LH
 205 Electronic Compartment
 703 APU Compartment


 (2)  
Access Panels
 1201 Electronic Equipment Access Door
 3804 APU Cowl Door

 

 C. Procedure
 S 424-007
 (1)  Install the surge bleed valve:
 (a)  
Install the new packing in the groove on the surge bleed valve.

 (b)  
Attach the surge bleed valve to the turbine plenum with the two screws and the washers. 1) Tighten the screws to 20-26 pound-inches

 (2.3-3.0 newton-meters). 2) Install lockwire to the screws.

 (c)  
Connect the electrical connector to the surge bleed valve.


 S 414-008
 CAUTION: KEEP A MINIMUM CLEARANCE OF 0.18 INCHES (5 MM) BETWEEN THE
_______ ENGINE, THE FIRE DETECTOR, THE CLAMPS, AND THE LOWER SHROUD.
 BE CAREFUL WHEN YOU MOVE THE LOWER SHROUD. DAMAGE TO THE SHROUD DRAIN LINES CAN OCCUR.
 (2)  Install the lower shroud:
 (a)  
Hold the lower shroud against the upper shroud.

 (b)  
Close the shroud latches.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-52-41
 ALL  ú ú 01 Page 403 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES/MAINTENANCE MANUAL ////////////////////////
S 414-009
 (3)  Close the APU cowl door: (a) Disconnect the door support rods. (b) Put the door support rods in the clips on the APU cowl door. (c) Close the APU cowl door. (d) Close the latches for the APU cowl door.
 S 864-010
 (4)  Set the circuit breaker and the switch: (a) Remove the DO-NOT-CLOSE tag and close this circuit breaker: 1) E3-3 Electrical Shelf, APU Control Unit (b) Remove the DO-NOT-OPERATE tag from the APU master switch on the P5 forward overhead panel.
 S 714-011
 (5)  Do the operational test of the surge bleed valve (AMM 49-52-41/501).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 
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 2(92)