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时间:2011-04-08 12:04来源:蓝天飞行翻译 作者:航空
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
ENGINE CONTROLS - TROUBLE SHOOTING
__________________________________
 1. Trouble Shoot the Engine Controls System
________________________________________
 A. Procedure
 (1)  To trouble-shoot the Engine Control system, refer to the trouble-shooting diagrams in Chapter 71 (AMM 71-00-40/101).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
ENGINE CONTROL SYSTEM - DESCRIPTION AND OPERATION
_________________________________________________
 1.  General________
 A.  The engine control system for each engine is divided into three
 subsystems: the forward thrust control system, the reverse thrust
 control system, and the start control system.

 B.  The forward thrust control system consists of a thrust lever assembly for each engine, connected to each main engine control by control cables, an engine control drum and a push-pull cable (Fig. 1). The forward thrust control system regulates the engine fuel flow and hence forward thrust.
 C.  The reverse thrust control system consists of a reverse thrust lever for
 each engine connected to each main engine control by the same control
 cables, engine control drum and push-pull cable used to control forward
 thrust. However, the reverse thrust control system causes cable travel
 in the opposite direction and actuates the thrust reverser. The system
 regulates fuel flow to the engine and hence reverse thrust. A lockout
 mechanism prevents simultaneous motion of the forward and reverse thrust
 levers.


Engine Control System Component Location
Figure 1 (Sheet 1)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
THRUST CABLES
ENGINE CONTROL DRUM START CABLES START CONTROL DRUM
INBD
FWD
THRUST 
CABLE PUSH-PULL  START PUSH-PULL CABLE 
THRUST REVERSER 
____NOTE:  NO. 1 ENGINE INSTALLATION  FEEDBACK PUSH-PULL 
SHOWN.  NO. 2 ENGINE  CABLES 
INSTALLATION SIMILAR 

THRUST THRUSTPUSH-PULL PUSH-PULLCABLE CABLE
START START
PUSH-PULL PUSH-PULL
CABLE CABLE
MEC FUEL MEC FUEL
CONTROL CONTROL
BOX BOX
START CONTROL CABLES WITH  START CONTROL CABLES WITH
B
FIXED LOWER END FITTING  ADJUSTABLE LOWER END FITTING
Engine Control System Component Location
Figure 1 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
D.  An engine control drum for each engine is mounted on the forward face of the front wing spar (Fig. 1). The drum transmits engine control cable travel to the push-pull cable by means of a rack and pinion system.
 E.  The start control system consists of a start lever assembly for each engine, connected to each main engine control by control cables, a start control drum and a push-pull cable. The start control system energizes the ignition system and initiates fuel flow to the engine.
 F.  Integrated autothrottle servomechanisms are installed in the throttle control cable runs. The servomechanisms are located between floor beams at the aft end of the electronic equipment compartment. In the autothrottle mode, the system is controlled by the autothrottle computer and the throttle levers are driven through the servomechanisms (Ref Chapter 22, Auto Flight).
 
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本文链接地址:737-300 400 500 AMM 飞机维护手册 发动机控制 ENGINE CONTROLS(2)