737-300/400/500
MAINTENANCE MANUAL
FLIGHT CONTROLS SWITCHES (SEE FIGURE 5)
STABILIZER TRIM CONTROL SWITCH
SPEED BRAKE CONTROL LEVER
RUDDER PEDALS FORWARD OVERHEAD PANEL
AILERON CONTROL WHEELS
STABILIZER TRIM CONTROL SWITCH
FLAP CONTROL LEVER
STABILIZER TRIM CONTROL WHEELS
Pilot's Controls
Figure 2
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-00-00
ALL ú ú 01 Page 3 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SPEED BRAKE HANDLE
ACBA
AILERON
CONTROL
WHEEL DRUM ACBB
AA
AILERON TRIM ACTUATOR
FLIGHT SPOILER ABSA
CABLE SLACK TAKEUP
AILERON
WING
QUADRANT
TRANSFER MECHANISM
AB SPOILER CONTROL DRUM AILERON CONTROL QUADRANT FLIGHT SPOILER AILERON BUS SYSTEM CABLES
AB AA
ABSB ABSA
ABSB MECHANISM SPOILER MIXER AILERON AILERON POWER CONTROL UNITS AILERON SPRING CARTRIDGE ARTIFICIAL FEEL CENTERING AND TRIM AILERON BALANCE TAB
AILERON BALANCE TAB
AILERON
Roll Control System Schematic
Figure 3
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-00-00
ALL ú ú 02 Page 4 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE A
LOW PRESSURE
WARNING
HOUSING SWITCH
SPOILER
SHUTOFF FLIGHT CONTROLS
VALVE SHUTOFF VALVE
COMPENSATOR CARTRIDGE
A
Flight Controls Hydraulic Modular Package Figure 4
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-00-00
ALL ú ú 01 Page 5 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
FLIGHT SPOILER ACTUATOR GROUND SPOILERTYPICAL (4 LOCATIONS) ACTUATOR INBOARD
SEE DETAILS A AND C
(FIG. 5 SHT 4)
SEE DETAIL B
3 45 6
LOW PRESSURE
SWITCH
2
7
5
7 9 4
8 1
13
2
0
FLIGHT CONTROLS
54 6
SHUTOFF VALVE
12
HYDRAULIC
HYDRAULIC SYSTEM "B"
SPOILER SHUTOFF RET SYSTEM "A" RET
PRESS PRESS
2
VALVE
AILERON POWER AILERON POWER
1
CONTROL UNIT CONTROL UNIT
MANUAL HYDRAULIC
ISOLATION VALVES
5 5
6 6
FLIGHT CONTROLSHYDRAULIC MODULARFLIGHT CONTROLS
3 3
HYDRAULIC MODULARPACKAGE SYSTEM A
7 7
PACKAGE SYSTEM B
2
2 4 4
CHECK VALVE STANDBYHYDRAULIC SYSTEM
COMPENSATOR
RUDDER
CARTRIDGE PRESSURE
REDUCER
RUDDER POWER RET PRESSCONTROL UNIT
1
ELEVATOR POWERCONTROL UNIT
(TYPICAL)
LEGEND
PRESSURE
67
RETURN
SPOILER RETRACT
SPOILER EXTEND RUDDER STANDBYPOWER UNIT
1
NOT INSTALLED ON ALL ELEVATOR FEEL COMPUTERELEVATOR HYDRAULIC
AIRPLANES (SB 27A1206) 1
FEEL DIFFERENTIAL PRESS SW FEEL ACTUATOR
Flight Controls System Hydraulic Schematic
Figure 5 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-00-00
ALL ú ú 01 Page 6 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
T82002
A
737-300/400/500MAINTENANCE MANUAL
NORMAL
BYPASS
FLAP
ASYMMETRY
SHUTOFF
RELAY
28V DC OFF
DC BUS NO. 1
FLAP VALVES
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(11)
