27-09-00
ALL ú ú 01 Page 203 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
AILERONS
COMPONENT SHT 102 FIG. QTY ACCESS/AREA REFERENCE
ACTUATOR - AILERON TRIM, M254 3 1 LEFT WING GEAR WHEEL WELL 27-11-06
ACTUATOR - INBOARD POWER CONTROL PACKAGE 4 2 573AB,673AB,573BB,673BB 27-11-12
ACTUATOR - LEFT OUTBOARD AILERON LOCKOUT, X452 4 1 591CB, LEFT WING 27-11-14
ACTUATOR - OUTBOARD POWER CONTROL PACKAGE 4 2 591CB,691CB,591CB,691DB 27-11-13
X453 ACTUATOR - RIGHT OUTBOARD AILERON LOCKOUT, 4 1 691CB, RIGHT WING 27-11-14
AILERON - INBOARD 4 2 WING TRAILING EDGE 27-11-01
AILERON - OUTBOARD 4 2 WING TRAILING EDGE 27-11-02
ASSEMBLY - AILERON DRUM 1 2 211,212, FWD PASS CABIN CEILING 27-11-04
CARD - AILERON/SPOILER SURFACE POSITION DIGITIZER (SPD), YMLA17 1 1 ELEC SYS CARD FILE, M7603 (REF) LEFT OF NOSE GEAR WHEEL WELL, 27-18-02
CIRCUIT BREAKERS SPLR/ALRN SENSOR, C384 SPLR/ALRN IND, C10062 OUTBOARD AILERON LOCKOUT, C1186 AILERON TRIM, C75 1 16 6J20 6J21 7D18 7D17 FLT COMPT, P6,P7 * * * *
LIMITER - AILERON CONTROL LOAD 2 1 212, FWD PASS CABIN CEILING 27-11-05
LIMITER - AILERON FORCE 2 1 LEFT WING GEAR WHEEL WELL 27-11-26
MECHANISM - AILERON TRIM AND FEEL 3 1 LEFT WING GEAR WHEEL WELL 27-11-06
MECHANISM - OUTBOARD AILERON LOCKOUT 4 2 591CB,691CB, WING 27-11-14
MODULE - (REF 27-40-00, FIG. 101) R STABILIZER TRIM/RUDDER RATIO, M3137 MODULE - FLIGHT CONTROLS HYDRAULIC POWER, M191 MODULE - (REF 27-20-00, FIG. 101) AILERON/RUDDER TRIM CONTROL, M7312 L STABILIZER TRIM/RUDDER RATIO, M3136 1 1 FLT COMPT, P461 *
PACKAGE - RIGHT AUTOPILOT - CENTERAL LATERAL CONTROL 3 1 LEFT WING GEAR WHEEL WELL 27-11-08
AUTOPILOT - CENTERAL LATERAL CONTROL PACKAGE - LEFT 3 1 RIGHT WING GEAR WHEEL WELL 27-11-08
* SEE THE WDM EQUIPMENT LIST
Ailerons - Component Index
Figure 101 (Sheet 1)
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27-10-00
ALL ú
ú 01 Page 101
ú Jun 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
QUADRANT - CLC INPUT 2 1 RIGHT WING GEAR WHEEL WELL 27-11-09
QUADRANT - INBOARD AILERON 4 1 573AB,673AB,573BB,673BB, WING 27-11-11
QUADRANT - LEFT AILERON PROGRAMMER 3 1 LEFT WING GEAR WHEEL WELL 27-11-10
QUADRANT - OUTBOARD AILERON 4 1 591CB,691CB,591DB,691DB, WING 27-11-14
QUADRANT - RIGHT AILERON PROGRAMMER 3 1 RIGHT WING GEAR WHEEL WELL 27-11-10
QUADRANT - TRIM AND FEEL MECHANISM 3 1 LEFT WING GEAR WHEEL WELL 27-11-06
ROD - LEFT CLC CONTROL 3 1 LEFT WING GEAR WHEEL WELL 27-11-26
SERVO - (REF 22-10-00, FIG. 101) SWITCHES -LATERAL AUTOPILOT, B7085 ROD - RIGHT CLC CONTROL 3 1 RIGHT WING GEAR WHEEL WELL 27-11-26
AILERON TRIM ARMING SWITCH, S1 1 1 TRIM CONTROL PANEL M7312 FLT COMPT, P8, AILERON/RUDDER *
AILERON TRIM CONTROL SWITCH, S2 1 1 TRIM CONTROL PANEL M7312 FLT COMPT, P8, AILERON/RUDDER *
TRANSMITTER - LEFT INBOARD AILERON POSITION, T1670 6 1 573BB, LEFT WING 27-18-01
TRANSMITTER - LEFT OUTBOARD AILERON POSITION, T489 6 1 591BB, LEFT WING 27-18-01
TRANSMITTER - RIGHT INBOARD AILERON POSITION, T1671 6 1 673BB, RIGHT WING 27-18-01
TRANSMITTER - RIGHT OUTBOARD AILERON UNIT - (REF 31-61-00, FIG. 101) R EFIS/EICAS INTERFACE, M7351 L EFIS/EICAS INTERFACE, M7353 C EFIS/EICAS INTERFACE, M7352 POSITION, T488 6 1 691CB, RIGHT WING 27-18-01
VALVE - AILERON & SPOILER HYDRAULIC SYSTEM 1 SHUTOFF, V140 5 1 591BB, LEFT WING 27-13-01
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