757 AMM 飞机维护手册 防火 FIRE PROTECTION 1(105)

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

M10259
LIGHT - R WING BODY OVHT, YNNL002  2  1  FLT COMPT, P5, BLEED AIR CONT,  *
 M10259
PANEL - (FIM 30-32-00/101) 
MISC TEST, M10398 
PANEL - (FIM 36-10-00/101)
 BLEED AIR CONT, M10259 
SWITCH - DUCT LEAK/FUEL QTY, YPHS006  2  1  FLT COMPT, P61, MISC TEST PNL,  *
 M10398 

* SEE THE WDM EQUIPMENT LIST
Duct Leak Detection - Component Index
Figure 101

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 26-18-00
 ALL  ú ú 01 Page 101 ú Sep 20/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E30099
A

757
FAULT ISOLATION/MAINT MANUAL

FLIGHT COMPARTMENT

Duct Leak Detection - Component Location
Figure 102 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 26-18-00
 ALL  ú ú 01 Page 102 ú Jun 20/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 FAULT ISOLATION/MAINT MANUAL

DUCT LEAK LIGHTS, YNNL001, YNNL002

TEST SWITCH, YPHS006
MISCELLANEOUS TEST PANEL, M10398 (REF)

Duct Leak Detection - Component Location
Figure 102 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 26-18-00
 ALL  ú ú 01 Page 103 ú Jun 20/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 FAULT ISOLATION/MAINT MANUAL
ELECTRICAL SYSTEM

Duct Leak Detection - Component Location
Figure 102 (Sheet 3)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 26-18-00
 ALL  ú ú 02 Page 104 ú Jun 20/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 WING AND BODY DUCT LEAK DETECTION - ADJUSTMENT/TEST
___________________________________________________
 1.  General_______
 A.  This section contains procedures for the operational test and the system test of the wing and body duct leak detection system.
 (1)  
The operational test makes sure the system operates properly. Only equipment installed in the plane is used for the test.

 (2)  
The system test makes sure the performance requirements of the system are met.

 TASK 26-18-00-715-001
 2.  Operational Test - Wing and Body Duct Leak Detection____________________________________________________
 A.  References
 (1)  
AMM 24-22-00/201, Electrical Power - Control

 (2)  
AMM 31-41-00/501, EICAS

 B.  Access
 (1)  
Location Zones
 100 Lower Half of Fuselage
 120 Main Equipment Center (Right)
 212 Control Cabin (Right)
 530/630 Wing Area (Right & Left )

 (2)  
Access Panel
 119BL Main Equipment Center

 

 C.  Test Wing and Body Duct Leak Detection System
 S 865-002
 (1)  
Supply electrical power to BUS R and BUS L AC bus and BUS R 28V DC (AMM 24-22-00/201).

 S 285-003

 (2)  
Make sure these circuit breakers on the overhead circuit breaker panel, P11, are closed.

 (a)  
11Q26, DUCT LEAK CONT

 (b)  
11Q17, DUCT LEAK LEFT

 (c)  
11Q25, DUCT LEAK RIGHT

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 26-18-00
 ALL  ú ú 01 Page 501 ú May 28/99
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：757 AMM 飞机维护手册 防火 FIRE PROTECTION 1(105)