• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-16 10:09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

 A. References
 (1)  
AMM 71-11-04/201, Fan Cowl Panels

 (2)  
AMM 71-11-06/201, Core Cowl Panels

 (3)  
AMM 78-31-00/201, Thrust Reverser System

 (4)  
AIPC 73-21-07 Fig. 5

 (5)  
WDM 71-51-15, WDM 71-51-16, WDM 73-12-15, WDM 73-12-25, WDM 73-12-35, WDM 73-12-45, WDM 76-11-11, WDM 76-11-21, WDM 76-11-31, WDM 76-11-41, WDM 77-12-21, WDM 77-12-22, WDM 77-12-23, WDM 77-12-24

 (6)  
SSM 73-21-01, SSM 76-11-01, SSM 76-11-02, SSM 76-11-03, SSM 76-11-04, SSM 77-12-02

 B.
Access

 (1)  
Location Zones 412 Engine 1 - LPT Case 5:30 o'clock, HPT Case and Diffuser and Combustor Case 3:30 o'clock 422 Engine 2 - LPT Case 5:30 o'clock, HPT Case and Diffuser and Combustor Case 3:30 o'clock 432 Engine 3 - LPT Case 5:30 o'clock, HPT Case and Diffuser and Combustor Case 3:30 o'clock

 442  Engine 4 - LPT Case 5:30 o'clock, HPT Case and Diffuser and Combustor Case 3:30 o'clock

 (2)  
Access Panels
 416 Right Thrust Reverser Half - Engine 1
 426 Right Thrust Reverser Half - Engine 2
 436 Right Thrust Reverser Half - Engine 3
 446 Right Thrust Reverser Half - Engine 4


 C.
Procedure


 S 864-176-N00
 (1)  
For the applicable engine, open these circuit breakers and install the DO-NOT-CLOSE tags:

 (a)  
P6 Main Power Distribution Panel
 1) 6G15 SCU ALT PWR ENG 1
 2) 6G23 ENG SCU 1
 3) 6G16 SCU ALT PWR ENG 2
 4) 6G24 ENG SCU 2

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 73-21-07
 ALL  ú ú N01A Page 465 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
SEE  A  PROBE (TT3) THERMOCOUPLE EEC 
SEE  H  SEE  J 
SEE  I  SEE  F  SEE  J  SEE  K  SUPPORT TUBE 

SEE L
SEE M
SEE F
W5J12 ELECTRICAL CONNECTOR
W6P12 ELECTRICAL CONNECTOR
SEE G
SEE F SEE B
FWD
W6 HARNESS
A
EEC Wiring Harness W6 Installation

Figure 405 (Sheet 1)
E44643
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 73-21-07
 ALL  ú ú N01A Page 466 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
SEE E
SEE D
EGT (TT4.95) THERMOCOUPLE FWD TERMINAL BOX
SEE C
W6 HARNESS  B  W6 HARNESS  BOLT  BRACKET 
TERMINAL BOX THERMOCOUPLE EGT (TT4.95)  FWD  CUSHION CLAMP 
GROUND LEAD 
(2 LOCATIONS) ALUMEL WASHER 
(2 LOCATIONS) (2 LOCATIONS) CHROMEL WASHER ALUMEL NUT  NUT 
(2 LOCATIONS) CHROMEL NUT  FWD 

(4 LOCATIONS) SCREW 
C  COVER 
Figure 405 (Sheet 2) EEC Wiring Harness W6 Installation 

E44645
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 73-21-07
 ALL  ú ú N01A Page 467 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
NUT 
FWD  BRACKET 
NUT  SUPPORT TUBE  BOLT 
W6 HARNESS  BOLT 
NUT  SUPPORT TUBE  E  BOLT  W6 HARNESS NUT  TUBE SUPPORT 
BOLT  G 
F  W6 HARNESS 
Figure 405 (Sheet 3) EEC Wiring Harness W6 Installation 

E44647
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 发动机燃油和控制 2(59)