R = REVISED, A = ADDED OR D = DELETED CHAPTER 76 F = FOLDOUT PAGE EFFECTIVE PAGES 17 C PAGE 2 JUL 12/02 LAST PAGE
D6-37537
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
CHAPTER 76 - ENGINE CONTROLS
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
ENGINE CONTROLS 76-00-00
_______________ Trouble Shooting 101 ALL
POWER CONTROL 76-10-00
_____________ ENGINE CONTROL SYSTEM 76-11-00
Description and Operation 1
General 1
Cables - Engine Control 6
Cables - Push-Pull 8
Drum - Engine Control 8
Drum - Start Control 8
Lever - Engine Start 6
Lever Assembly - Thrust 3
Servomechanism - Integrated 8
Autothrottle
Operation 9
Maintenance Practices 201 ALL General 201 System - Engine Control 201
Adjustment/Test 501 ALL Engine Control Cables Tension 511 Adjustment Engine Control System Rigging 501 (Travel Adjustment)
System Test 522 Inspection/Check 601 ALL BOX - CONTROL, MAIN ENGINE 76-11-08
CONTROL FUEL Removal/Installation 401 ALL BOX - CONTROL, STRUT DRUM 76-11-05 Removal/Installation 401 ALL CABLE - PUSH-PULL, START CONTROL 76-11-09 Removal/Installation 401 ALL CABLE - PUSH-PULL, THRUST 76-11-07 CONTROL Removal/Installation 401 ALL CABLES - ENGINE CONTROL 76-11-04 Maintenance Practices 201 ALL
76-CONTENTS
CBEJ Page 1 Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
CHAPTER 76 - ENGINE CONTROLS
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
CONTROL STAND COVERS, SEALS AND 76-11-11
LIGHTPLATES
Removal/Installation 401 CONFIG 1 [*]
[*] AIRPLANES WITH NON-REINFORCED CONTROL STANDS WITH A TIE ROD-AND-NUT
THROUGH THE STABILIZER TRIM SHAFT
Removal/Installation 401 CONFIG 3 [*]
[*] AIRPLANES WITH EFIS-REINFORCED CONTROL STANDS WITH A STABLIZER TRIM
SHAFT WITH A SELF-LOCKING INSERT-AND-BOLT
Removal/Installation 401 CONFIG 2 [*]
[*] AIRPLANES WITH EFIS REINFORCED CONTROL STANDS WITH A TIE ROD THROUGH
THE SPLINE SHAFT
LEVERS - START 76-11-02
Removal/Installation 401 CONFIG 1 [*]
[*] AIRPLANES WITH NON-REINFORCED CONTROL STANDS
Removal/Installation 401 CONFIG 3 [*]
[*] AIRPLANES WITH EFIS REINFORCED CONTROL STANDS WITHOUT A TIE ROD
THROUGH THE SPLINE SHAFT
Removal/Installation 401 CONFIG 2 [*]
[*] AIRPLANES WITH EFIS REINFORCED CONTROL STANDS WITH A TIE ROD THROUGH
THE SPLINE SHAFT
LEVERS - THRUST 76-11-01
Removal/Installation 401 CONFIG 1 [*]
[*] AIRPLANES WITH NON-REINFORCED CONTROL STANDS WITH A TIE ROD-AND-NUT
THROUGH THE STABILIZER TRIM SHAFT
Removal/Installation 401 CONFIG 3 [*]
[*] AIRPLANES WITH EFIS-REINFORCED CONTROL STANDS WITH A STABLIZER TRIM
SHAFT WITH A SELF-LOCKING INSERT-AND-BOLT
MECHANISM - AUTOTHROTTLE TORQUE 76-11-03
SWITCH
Removal/Installation 401 ALL
SHUTOFF ASSEMBLY - FUEL 76-11-06
Removal/Installation 401 ALL
SWITCHES - ENGINE START LEVER 76-11-10
Removal/Installation 401 ALL
Adjustment/Test 501 ALL
76-CONTENTS
ú
ú CBEJ.101 Page 2
ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
CHAPTER 76 - ENGINE CONTROLS TABLE OF CONTENTS
_________________ Chapter
Subject_______ SectionSubject_______ Page____ Effecti_______ vity____
THRUST LEVERS (DO NOT USE THIS CONFIGURATION) Removal/Installation 76-11-01 401 CONFIG 2 [*]
[*] AIRPLANES WITH EFIS REINFORCED CONTROL STANDS WITH A TIE ROD THROUGH THE SPLINE SHAFT
EMERGENCY SHUTDOWN 76-20-00
__________________ ENGINE FIRE EMERGENCY SHUTDOWN 76-21-00 Description and Operation 1 ALL General 1
76-CONTENTS
ú ú CBEJ.101 Page 3 ú Jul 12/02 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 发动机控制 ENGINE CONTROLS
