(a)
Hold aileron trim switches in LEFT WING DOWN or RIGHT WING DOWN position. Control wheels will move in response to switch commands.
(7)
Remove hydraulic power.
(8)
Remove electrical power.
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ALL ú ú 02 Page 15 ú Mar 15/87
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
FAULT ISOLATION/MAINT MANUAL
AILERON AND AILERON TRIM CONTROL SYSTEM
COMPONENT SHT 102 FIG. QTY ACCESS/AREA REFERENCE
ACTUATOR (PCA) - AILERON POWER CONTROL 3 4 561CB,661CB 27-11-20
ACTUATOR - LATERAL TRIM, M488 2 1 AND TRIM MECHANISMLEFT MAIN GEAR WHEEL WELL, LATERAL CONTROL FEEL, CENTERING 27-11-14
AILERON, 568,668 3 2 WING TRAILING EDGE 27-11-21
ASSEMBLY - AILERON CONTROL DRUM CABLES - CONTROL (REF MM 27-00-01/201) 1 2 113AL, FWD EQUIP COMPT 27-11-03
CIRCUIT BREAKER 1 FLT COMPT, P11
AILERON POS L, C4099 1 11J14 *
AILERON POS R, C4100 1 11J23 *
AILERON TRIM, C1035 1 11J15 *
FILTER - AILERON PCA 3 4 561CB,661CB, AILERON PCA 27-11-20
INDICATOR - AILERON TRIM 1 2 FLT COMPT, CONTROL WHEEL 27-11-00
LIMITER - BUS FORCE 1 1 113AL, FWD EQUIP COMPT 27-11-03
MECHANISM - AILERON QUADRANT AND OVERRIDE 3 2 561AB,661AB 27-11-18
MECHANISM - LATERAL CONTROL FEEL, CENTERING, AND TRIM 2 1 BULKHEAD LEFT MAIN GEAR WHEEL WELL, FWD 27-11-14
MECHANISM - LATERAL CONTROL OVERRIDE 2 1 BULKHEAD RIGHT MAIN GEAR WHEEL WELL, FWD 27-11-16
CONTROL, M10042 (REF 22-13-00, FIG. 101) SERVO (ALCS) - LEFT AUTOPILOT LATERAL CONTROL, M10040 (REF 22-13-00, FIG. 101) SERVO (ALCS) - CENTER AUTOPILOT LATERAL SERVO (ALCS) - LEFT AUTOPILOT LATERAL CONTROL, M10041 (REF 22-13-00, FIG. 101) PANEL - AILERON/RUDDER TRIM CONTROL, M74 1 1 FLT COMPT, P8 *
SWITCH - AILERON TRIM ARM 1 1 CONT PANEL, M74 FLT COMPT, P8, AIL/RUD TRIM *
TS5068 (REF 22-13-00, FIG. 101) TS16 (REF 22-13-00, FIG. 101) TRANSDUCER - LEFT AILERON CONTROL FORCE, TRANSDUCER - RIGHT AILERON CONTROL FORCE, TS5082 (REF 27-61-00, FIG. 101) UNIT - SPOILER TRANSDUCER (RVDT), TS5081, SWITCH - AILERON TRIM CONTROL1 1 1 1 CONT PANEL, M74 FLT COMPT, P8, AIL/RUD TRIM *
WHEEL - LATERAL CONTROL 1 2 FLT COMPT, CONTROL COLUMN 27-11-02
* SEE THE WDM EQUIPMENT LIST
1 GUN 001-010
Aileron and Aileron Trim Control System - Component Index
Figure 101
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ALL ú
ú 05 Page 101
ú Jun 20/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
FAULT ISOLATION/MAINT MANUAL
TRIM INDICATOR
SEE B AILERON
CAPTAIN'S TRIM ARM
CONTROL WHEEL SWITCH
FIRST
OFFICER'S
CONTROL
WHEEL
AILERON TRIM CONTROL SWITCH
AILERON/RUDDER TRIM P8 PANEL CONTROL PANEL, M74 AILERON/RUDDER
A
TRIM CONTROL PANEL, M74 CONTROL
FLIGHT COMPARTMENT
SEE A COLUMN
CSEE ASSEMBLY CONTROL DRUM AILERON INDICATOR TRIM WHEEL CONTROL
MECHANISMS LATERAL CONTROL SEE D SHT 2 TRIM INDICATOR B
FWD BUS FORCE LIMITER CONTROL DRUM HOUSING DRUM
AFT INBD PUSHROD PEDAL RUDDER
RVDT UNIT SPOILER
AILERON CONTROL DRUM ASSEMBLY (2 LOCATIONS)
C
Aileron and Aileron Trim Control - Component Location Figure 102 (Sheet 1)
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27-11-00
ALL ú ú 01 Page 102 ú Jun 20/91
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本文鏈接地址：757 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 1(62)
