AUTOPILOT LATERAL
1.CONTROL SERVO
OUTPUT CRANK
ROD END (REF)
RIGHT ALCS OUTPUT
CENTER ALCS M10041AUTOPILOT
(LEFT ALCS M10040 CRANK AND CONTROL
CONTROL ROD LENGTH
CRANK (REF)
FORWARD) (REF) ROD (HIDDEN) (REF)
INCHES12.50RIGHT ALCSWASHER 3.
NOMINAL LENGTH CENTER ALCS SEE B M10042 (REF)OUTPUT CRANK
SEE B
(REF)
A
NUT4.OUTPUT CRANKJAMNUT(REF) AUTOPILOTCRANK INSPECTION HOLE
(REF)
JAMNUT
14.
CONTROL ROD
5.
(REF) (EACH END)
BOLT
2.
FILTER
8.
1 LOOSEN JAMNUT AND ADJUST ROD END UNTILELECTRICAL
PACKING 9.
DIMENSION IS OBTAINED THEN ADJUSTCONNECTORCONTROL ROD
UNION (REDUCER) 10.
CONTROL ROD LENGTH(REF) TO ALCS (REF) HYDRAULICSOLENOID VALVEPRESSURE LINENO. 2 (REF)
(REF)
ELECTROHYDRAULIC HYDRAULIC
SERVO VALVE (REF)RETURN LINE
QUADRANT
PACKING11.
SOLENOID VALVE (REF)
(REF)
JAMNUT
13.
UNION
12.
NO. 1 (REF) 1.34-1.36 INCHES
AUTOPILOT LATERAL CONTROL INSTALLATION (TYPICAL)
1
B C
Autopilot Lateral Control Servo Installation (ALCS)
Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-13-03
ALL ú ú 01 Page 403 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：757 AMM 飞机维护手册 自动飞行 AUTOFLIGHT 1(187)
