• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-16 10:10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

 1) P6 Main Power Distribution Panel
 a) 6F1 IGN 1 ENG 1
 b) 6F2 IGN 1 ENG 2
 c) 6F3 IGN 1 ENG 3
 d) 6F4 IGN 1 ENG 4

 (b)  For the lower cable (3),
 1) P6 Main Power Distribution Panel
 a) 6K19 IGN 2 ENG 1
 b) 6K20 IGN 2 ENG 2
 c) 6K21 IGN 2 ENG 3
 d) 6K22 IGN 2 ENG 4

 (c)  For the upper and/or lower cable (3),
 1) P6 Main Power Distribution Panel
 a) 6G19 STBY IGN ENG 1
 b) 6G20 STBY IGN ENG 2
 c) 6G21 STBY IGN ENG 3
 d) 6G22 STBY IGN ENG 4

 S 754-030-N00
 (15) Do the ignition operational (audible) test (AMM 74-00-00/501).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 74-21-01
 ALL  ú ú N01 Page 411 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
EXCITER-TO-IGNITER PLUG CABLE - INSPECTION/CHECK
________________________________________________
 1.  General
_______
 A.  This task includes the task to do a visual inspection of the
 exciter-to-igniter plug cable.

 B.  Inspection of the exciter-to-igniter plug cable is necessary after a fast engine shutdown. During a fast engine shutdown, the ignition parts cannot sufficiently cool to prevent the damage. Examine the cables and the igniter plug terminal. Make sure that the high temperatures did not cause damage to the insulation for the high tension leads or the rubber bushings.
 TASK 74-21-01-206-001-N00
 2.  Exciter-to-Igniter Plug Cable Inspection (Fig. 601)
________________________________________
 A.  References
 (1)
AMM 71-11-04/201, Fan Cowl Panels

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

 (3)
AMM 74-21-01/401, Exciter-to-Igniter Plug Cable

 (4)
AMM 74-21-01/701, Exciter-to-Igniter Plug Cable

 (5)
AMM 78-31-00/201, Thrust Reverser System

 (6)
IPC 74-21-01 Fig. 5


 B.  Access
 (1)  
Location Zone 412 Engine 1 - HPC Aft Case to Diffuser/Combustor Case 4 or 5 o'clock 422 Engine 2 - HPC Aft Case to Diffuser/Combustor Case 4 or 5 o'clock 432 Engine 3 - HPC Aft Case to Diffuser/Combustor Case 4 or 5 o'clock

 442  Engine 4 - HPC Aft Case to Diffuser/Combustor Case 4 or 5 o'clock

 (2)  
Access Panel
 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 016-007-N00
 (1) Open the right fan cowl panel (AMM 71-11-04/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 74-21-01
 ALL  ú ú N01 Page 601 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
IGNITER PLUG END

EXCITER-TO-IGNITER PLUG CABLE

L-A4190
Exciter-to-Igniter Plug Cable Inspection Figure 601 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 74-21-01
 ALL  ú ú N01 Page 602 ú Jun 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
HIGH TENSION

LATE STAGEFLASHOVER DAMAGE

Exciter-to-Igniter Plug Cable Inspection
Figure 601 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 74-21-01
 ALL  ú ú N01 Page 603 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
 
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 点火 IGNITION(20)