747-400 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(42)

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

VALVE - AILERON & SPOILER HYDRAULIC SYSTEM 2 SHUTOFF, V141 5  1  LEFT WING GEAR WHEEL WELL  27-13-01 
VALVE - AILERON & SPOILER HYDRAULIC SYSTEM 3 SHUTOFF, V145  5  1  RIGHT WING GEAR WHEEL WELL  27-13-01 
VALVE - AILERON & SPOILER HYDRAULIC SYSTEM 4 SHUTOFF, V149 5  1  691BB, RIGHT WING  27-13-01 

* SEE WDM EQUIPMENT LIST
Ailerons - Component Index
Figure 101 (Sheet 2)

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-10-00
 ALL  ú
 ú  01  Page 102
 ú  Oct 10/89 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
FLIGHT CONTROLS HYDRAULIC POWER MODULE, M191
P7 PANEL  SEE  C 
CONTROL 
WHEELS (REF)  P6 PANEL 
AILERON/RUDDER TRIM 
CONTROL MODULE, M7312 (REF) 
SEE  A 

AILERON DRUM ASSEMBLIES
SEE D
SHT 2 ELECTRICAL SYSTEMS CARD FILE, M7603 (REF)
SEE B
AILERON/SPOILER SURFACE POSITION DIGITIZER (SPD) YMLA17
RUDDER TRIM 105 0 510
NOSE LEFT UNITS NOSE RIGHT
AILERON
L, R STABILIZER TRIM/
RUDDER RATIO MODULES, NOSE NOSE
M3136, M3137 (REF)
LEFT
RIGHT R
AILERON TRIM
U LEFT
RIGHT
D
WING
ARMING WING
D DOWN
E
SWITCH, (S1) DOWN
R
AILERON TRIM
CONTROL
SWITCH, (S2)

AILERON/RUDDER TRIM CONTROL MODULE, M7312 (REF)
A
FLT CONTROL HYD POWER
12 34
NORM
TAIL
SHUT OFF
VALVE
VALVE VALVE VALVE CLOSEDa
CLOSEDa CLOSEDa CLOSEDa
NORM
WING
SHUT OFF
VALVE VALVE VALVE VALVE CLOSEDa CLOSEDa CLOSEDa CLOSEDa
FLIGHT CONTROLS ELECTRICAL SYSTEMS CARD FILE, M7603 (REF)
HYDRAULIC POWER MODULE, M191
BC
Ailerons - Component Location
Figure 102 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-10-00
 ALL  ú ú 01 Page 103 ú Oct 10/89
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400 FAULT ISOLATION/MAINT MANUAL
ACCESS PANEL, 211
WING GEAR
WHEEL WELL

SEE E
CAPTAIN'S 
DRUM ASSEMBLY  AILERON CONTROL 
LOAD LIMITER 
FWD 
AILERON DRUM ASSEMBLIES 
FIRST OFFICER'S 
D  FROM SHT 1  DRUM ASSEMBLY 
PASS CABIN 
SPOILER  FORWARD CEILING 
DIFFERENTIAL  ACCESS 
MECHANISMS  PANEL, 212 
(REF) 
RIGHT CENTRAL LATERAL 
CONTROL PACKAGE 
(RIGHT AUTOPILOT)  1 
AILERON TRIM  SEE  H  SHT 3 
AND FEEL 
MECHANISM  SPEED BRAKE 
SEE  F  SEQUENCE 
MECHANISM 
SHT 3  (REF) 
LEFT CENTRAL LATERAL 
CONTROL PACKAGE 
SERVO, B7085 LATERAL AUTOPILOT  (LEFT AUTOPILOT)  2 
(REF)  CLC INPUT 
QUADRANT 
LEFT OR RIGHT 
AILERON PROGRAMMER  AILERON 
SEE  G  SHT 3  FORCE LIMITER 
WING GEAR WHEEL WELL  FWD 
1  INSTALLED IN THE LEFT WHEEL WELL 
E 
2  INSTALLED IN THE RIGHT WHEEL WELL 

Ailerons - Component Location
Figure 102 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-10-00
 ALL  ú ú 01 Page 104 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400 FAULT ISOLATION/MAINT MANUAL
CENTERING AND FEEL SPRINGS
ROD FROM SPOILER DIFFERENTIAL MECHANISM (REF)
OUTPUT ROD TO CENTRAL LATERAL CONTROL PACKAGE
AILERON TRIM ACTUATOR, M254
INPUT
TRIM AND FEEL ROD (REF)MECHANISM QUADRANT
AILERON TRIM AND FEEL MECHANISM
　
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 1(42)