* SEE THE WDM EQUIPMENT LIST
1
AMM 76-11-03/201 - ENGINE START MODULE
Horizontal Stabilizer - Component Index
Figure 101 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-40-00
ALL ú
ú 01 Page 102
ú Oct 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
COMPONENT SHT 102 FIG. QTY ACCESS/AREA REFERENCE
TRANSMITTER - C STABILIZER POSITION, M7883 3 1 315A, STABILIZER HINGE 27-48-01
TRANSMITTER - L STABILIZER POSITION, M7884 3 1 315A, STABILIZER HINGE 27-48-01
TRANSMITTER - R STABILIZER POSITION, M7882 UNIT - (REF 31-61-00, FIG. 101) L EFIS/EICAS INTERFACE, M7353 C EFIS/EICAS INTERFACE, M7352 R EFIS/EICAS INTERFACE, M7351 UNIT - (REF 27-50-00, FIG. 101) C FLAP CONTROL, M7880 L FLAP CONTROL, M7881 R FLAP CONTROL, M7879 3 1 315A, STABILIZER HINGE 27-48-01
VALVE - SHUTOFF, MOTOR OPERATED 2
- L, YM1V006 1 312A, STABILIZER JACKSCREW 27-41-04
- R, YM2V006 1 312A, STABILIZER JACKSCREW 27-41-04
VALVE - SOLENOID 2
- L NOSE DOWN ARMING, YM1V003 1 312A, STABILIZER JACKSCREW 27-41-04
- L NOSE DOWN CONTROL, YM1V004 1 312A, STABILIZER JACKSCREW 27-41-04
- L NOSE UP ARMING, YM1V001 1 312A, STABILIZER JACKSCREW 27-41-04
- L NOSE UP CONTROL, YM1V002 1 312A, STABILIZER JACKSCREW 27-41-04
- L RATE CONTROL, YM1V005 1 312A, STABILIZER JACKSCREW 27-41-04
- R NOSE DOWN ARMING, YM2V003 1 312A, STABILIZER JACKSCREW 27-41-04
- R NOSE DOWN CONTROL, YM2V004 1 312A, STABILIZER JACKSCREW 27-41-04
- R NOSE UP ARMING, YM2V001 1 312A, STABILIZER JACKSCREW 27-41-04
- R NOSE UP CONTROL, YM2V002 1 312A, STABILIZER JACKSCREW 27-41-04
- R RATE CONTROL, YM2V005 1 312A, STABILIZER JACKSCREW 27-41-04
Horizontal Stabilizer - Component Index
Figure 101 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-40-00
ALL ú ú 01 Page 103 ú Oct 10/89
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 飞行操纵 FLIGHT CONTROLS 3(116)