• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-08 12:01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


 NOTE: It can be necessary to loosen the bolts that attach the strap
____ across the air diffuser to make the valve removal easier.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 75-34-01
 ALL  ú ú C02 Page 401 ú Jul 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE  A 
FLANGE N 
BSEE BLEED VALVE 5TH-STAGE START 
HOLD DOWN STRAP AIR DIFFUSER 
1 BLEED VALVE FOR THE START DEFLECTOR BAFFLE BLEED VALVE FROM THE START AIR SIGNAL TUBE 
FLANGE P 
1  FWD Figure 401 (Sheet 1) 5th-Stage Start Bleed Valve Installation A ON LATER PRODUCTION ENGINES, THE BLEED VALVE DEFLECTOR WAS REMOVED

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 75-34-01
 ALL  ú ú C01 Page 402 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
JAMNUT  ELBOW 
V-BAND CLAMP METAL GASKET AIR INLET PORT BLEED AIR INLET AIR TUBE FOR 5TH-STAGE  PORT SIGNAL  B-NUT O-RING 5TH-STAGE START BLEED VALVE AIR OUTLET PORT
(2 LOCATIONS) BOLT  V-BAND CLAMP METAL GASKET 
AIR DIFFUSER HOLD DOWN STRAP  AIR DIFFUSER 

5th-Stage Start Bleed Valve Installation
Figure 401 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 75-34-01
 ALL  ú ú C02 Page 403 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TASK 75-34-01-404-008-C00
 3. Install the 5th-Stage Start Bleed Valve
_______________________________________
 A. Consumable Materials
 (1)  G02353, Lubricant, (CP2854) Petrolatum - VV-P-236
 B. References
 (1)  
AMM 70-20-02/201, V-band Clamps

 (2)  
AMM 78-31-00/201, Thrust Reversers


 C. Access
 (1)  
Location Zones
 506 Engine No. 1
 606 Engine No. 2


 (2)  
Access Panels
 5739L/5738L Engine No. 1 - Thrust Reverser Half
 5839R/5838R Engine No. 2 - Thrust Reverser Half

 

 D. Procedure (Fig. 401)
 S 434-009-C00
 (1)  
Put a new metal gasket on the air inlet port of the bleed valve.

 S 424-010-C00

 (2)  
ENGINES WITHOUT CFMI SB 72-426; Install, but do not tighten, the valve on the inlet air tube and attach it with a V-band clamp.


 NOTE: The valve is installed with the starter air signal port
____ pointed out from the engine, but turned 25-30 degrees from the valve center line in the clockwise direction.
 S 424-020-C00
 (3)  ENGINES WITH CFMI SB 72-426; Install, but do not tighten, the valve on the inlet air tube and attach it with a V-band clamp and self-locking nut.
 NOTE: The valve is installed with the starter air signal port
____ pointed out from the engine, but turned 25-30 degrees from the valve center line in the clockwise direction.
 S 434-011-C00
 (4)  
Install the new metal gasket between the bleed valve and air diffuser.

 S 434-012-C00

 (5)  
ENGINES WITHOUT CFMI SB 72-426; Attach the bleed valve to the air diffuser with a V-band clamp.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 75-34-01
 ALL  ú ú C01 Page 404 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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 空气 AIR(131)