• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-08 11:56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

MIDFLANGE 
BORESCOPE BOSSES CASING BODY 
(NOT SHOWN IN 
TRUE POSITION)  AIR DEFLECTOR 
HPT NOZZLE 
INNER SUPPORT 
ASEE 
HONEYCOMB SEAL 
DIFFUSER 
SUPPORT BODY 
OUTLET GUIDE VANES 
BOLT 
BOLT SHIELD  INDUCER 
VANES 
NUT SHIELD 

CDP SEAL 
FUEL NOZZLE PAD 
(20 PLACES) 
BORESCOPE 
BOSS 
PS3 PAD 

LPT 1ST-STAGEIGNITERCDP BLEED PORT COOLING AIRBOSS(4 PLACES) G-M56-SM-1026(1)-00-B
Combustion Case Location Figure 1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 72-41-00
 ALL  ú ú C01 Page 2 ú Oct 25/84
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
COMBUSTION CASE - INSPECTION/CHECK
__________________________________
 1.  General
_______
 A.  This procedure contains two tasks for the combustion case. The two tasks are as follows:
 -Combustion Case Casing Inspection
 -General Combustion Case Inspection
 B.  You must open the fan cowl panel and thrust reverser to get access to the combustion case.
 TASK 72-41-00-216-001-C00
 2.  Combustion Case Casing Inspection
_________________________________
 A.  General
 (1)  You must open the fan cowl panel and thrust reverser to get access to the combustion case.
 B.  References
 (1)  
71-11-02/201, Fan Cowl Panels

 (2)  
72-00-00/601, Engine

 (3)  
78-31-00/201, Thrust Reverser


 C.  Access
 (1)  
Location Zones
 502/602 Left Fan Cowl Panels
 503/603 Right Fan Cowl Panels
 504/604 Left Thrust Reversers
 505/605 Right Thrust Reversers
 506 Engine No. 1 - Turbine Frame
 606 Engine No. 2 - Turbine Frame


 (2)  
Access Panels
 5737L Engine No. 1 - Right Fan Cowl Panel
 5738L Engine No. 1 - Left Thrust Reverser
 5739L Engine No. 1 - Right Thrust Reverser
 5746L Engine No. 1 - Left Fan Cowl Panel
 5837R Engine No. 2 - Right Fan Cowl Panel
 5838R Engine No. 2 - Left Thrust Reverser
 5839R Engine No. 2 - Right Thrust Reverser
 5846R Engine No. 2 - Left Fan Cowl Panel

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 72-41-00
 ALL  ú ú C01 Page 601 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
COOLING AIR TO THE HPT SHROUD
SEE A  AFT FLANGE
BORESCOPE BOSSES TO
THE COMBUSTION CHAMBER
(NOT SHOWN IN
TRUE POSITION) CASE BODY
(4 LOCATIONS)

SEE B
FORWARD FLANGE
FUEL NOZZLE PAD (20 LOCATIONS) HPT BORESCOPE BOSSES (2 LOCATIONS)
PS3 PAD
CDP BLEED PAD COOLING AIR TO
(4 LOCATIONS) IGNITER BOSS THE LPT 1ST-STAGE
(2 LOCATIONS)
A G-M56-SM-1026(1)-00-B
Combustion Case Inspection
Figure 601 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 72-41-00
 ALL  ú ú C01 Page 602 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
INSULATION BLANKET
BOLT TAB AREA
INSULATION  FWD 
BLANKET FOR THE 
AIR DEFLECTOR  RETAINING BOLT 
(EXAMPLE)

Combustion Case Inspection
Figure 601 (Sheet 2)

 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 ENGINE 发动机 2(72)