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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D6-37537 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. ////////////////////////A / / 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CBEJ Page 1 Jul 12/01 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
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
ú ú CBEJ.101 Page 3 ú Jul 12/02 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
