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CHAPTER 76 Engine Controls Subject/Page Date COC EFFECTIVE PAGES 1 Jun 10/2006 2 BLANK 76-CONTENTS 1 Jun 10/2002 2 BLANK 76-00-00 1 Oct 10/2002 2 Oct 10/2002 3 Feb 10/2003 4 Oct 10/2002 5 Jun 10/2003 6 Jun 10/2003 7 Feb 10/2003 8 Oct 10/2002 9 Feb 10/2003 10 Oct 10/2002 11 Oct 10/2002 12 Oct 10/2002 13 Feb 10/2003 14 Oct 10/2002 15 Oct 10/2002 16 Oct 10/2002 17 Feb 10/2003 Subject/Page Date COC 76-00-00 (cont.) 18 Oct 10/2002 19 Feb 10/2003 20 Jun 10/2003 21 Feb 10/2003 22 Jun 10/2003 23 Feb 10/2003 24 BLANK A=Added, R=Revised, D=Deleted, O=Overflow, C=Customer Originated Change 76-EFFECTIVE PAGES Page 1 D633A101-GUN Jun 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL CHAPTER 76 Engine Controls CH-SC-SU Subject Page Effectivity 76-00-00 ENGINE CONTROLS - INTRODUCTION 2 GUN ALL 76-00-00 ENGINE CONTROLS - GENERAL DESCRIPTION 5 GUN ALL 76-00-00 ENGINE CONTROLS - COMPONENT LOCATION 8 GUN ALL 76-00-00 ENGINE CONTROLS - INTERFACES 11 GUN ALL 76-00-00 ENGINE CONTROLS - THRUST LEVER 15 GUN ALL 76-00-00 ENGINE CONTROLS - START LEVER 18 GUN ALL 76-00-00 ENGINE CONTROLS - START LEVER - FUNCTIONAL DESCRIPTION 20 GUN ALL 76-00-00 ENGINE CONTROLS - REVERSE THRUST INTERLOCK SOLENOIDS 22 GUN ALL 76-CONTENTS Page 1 D633A101-GUN Jun 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL CHAPTER 76 Engine Controls THIS PAGE IS INTENTIONALLY LEFT BLANK 76-00-00 Page 1 D633A101-GUN Oct 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL Purpose The engine control system supplies most of the signals to control the engine thrust. It also supplies signals to other airplane systems that use engine control status. The engine control system has these components: * Thrust lever assemblies * Thrust lever resolvers * Engine start levers and switches * Thrust lever interlock solenoids. Abbreviations and Acronyms * AGB - accessory gearbox * AMM - aircraft maintenance manual * ASM - autothrottle servomotor * CDS/DEU - common display system/display electronics unit * EEC - electronic engine control * FDAU - flight data acquisition unit * IDG - integrated drive generator * HPSOV - high pressure shutoff valve * RLA - reverse thrust lever angle * TLA - thrust lever angle * TO/GA - takeoff/go-around * TRA - thrust lever resolver angle * T/R - thrust reverser ENGINE CONTROLS - INTRODUCTION EFFECTIVITY GUN ALL 76-00-00 Page 2 D633A101-GUN Oct 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 76-00-00-000 ENGINE CONTROLS - INTRODUCTION ENGINE CONTROLS - INTRODUCTION EFFECTIVITY GUN ALL 76-00-00 Page 3 D633A101-GUN Feb 10/2003 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 76-00-00-000 THIS PAGE IS INTENTIONALLY LEFT BLANK ENGINE CONTROLS - INTRODUCTION 76-00-00 Page 4 D633A101-GUN Oct 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL General The engine control system supplies manual and automatic control inputs to operate the engine. The engine control system has these components: * Thrust levers (forward and reverse) * Thrust lever resolvers * Engine start levers and switches * Thrust lever interlock solenoids. Thrust Levers You use the thrust levers to supply the manual inputs to the engine control system. There are two thrust lever assemblies, one for each engine. For each engine, there is a forward thrust lever and a reverse thrust lever. The reverse thrust lever is on the forward thrust lever. For each engine, the thrust levers supply a thrust command signal to the electronic engine control (EEC) through the thrust lever resolver. Each thrust lever assembly connects mechanically to the resolver through an adjustable rod. An interlock latch prevents the operation of the forward thrust www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：ENGINE CONTROL
