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R = REVISED, A = ADDED OR D = DELETED CHAPTER 77 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D6-37537 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 77 - ENGINE INDICATING TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject ____ Effectivity _______ Page ___________ ENGINE INDICATING SYSTEM 77-00-00 ________________________ Description and Operation 1 ALL Trouble Shooting 101 ALL POWER 77-10-00 _____ ENGINE TACHOMETER SYSTEM 77-12-00 Description and Operation 1 ALL Indicator - N1 Tachometer 1 Indicator - N2 Tachometer 6 Sensor - N1 Speed 1 Sensor - N2 Control Alternator 1 Speed Operation 6 Adjustment/Test 501 ALL Operational Test -501 N1 Tachometer System 501 Operational Test -507 N2 Tachometer System 507 Operational Test -507 N2 Tachometer System 507 System Test -501 N1 Tachometer System 501
INDICATORS - N1 AND N2 77-12-02 TACHOMETER Removal/Installation 401 [*] [*] AIRPLANES WITHOUT ENGINE INSTRUMENT SYSTEM (EIS) DISPLAY SENSOR - N1 SPEED 77-12-01 Maintenance Practices 201 ALL Cleaning 201 Installation 203 Removal 201 Visual Check 203 TEMPERATURE 77-20-00 ___________ 77-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CBEJ Page 1 Jul 12/01 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 77 - ENGINE INDICATING TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject ____ Effectivity _______ Page ___________ EXHAUST GAS TEMPERATURE (EGT) 77-21-00 INDICATION SYSTEM Description and Operation 1 ALL Assembly - Thermocouple 1 Harness
9 Probe EGT System 1 Indicator - EGT 4 Operation 4
Adjustment/Test 501 ALL Operational Test 501 System Test 502
HARNESS AND PROBES - EGT 77-21-01 THERMOCOUPLE Maintenance Practices 201 ALL Broken EGT Harness Isolation 201 (Do not use this 401 configuration.) [*] 6 PROBE EGT SYSTEM
Removal/Installation 401 CONFIG 2 [*] 9 Probe EGT System - Rigid 401 Mount [*] 9 PROBE EGT SYSTEM (RIGID MOUNT) Removal/Installation 401 CONFIG 3 [*] 9 Probe EGT System - Soft 401 Mount [*] 9 PROBE EGT SYSTEM (SOFT MOUNT) Inspection/Check 601 ALL INDICATOR - EXHAUST GAS 77-21-02 TEMPERATURE (EGT) Removal/Installation 401 [*] [*] AIRPLANES WITHOUT EIS
ANALYZERS 77-30-00 _________
CBEJ Page 2 Jul 12/01 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. ////////////////////////A / / CFM56 ENGINES 737-300/400/500/ /MAINTENANCE MANUAL //////////////////////// CHAPTER 77 - ENGINE INDICATING TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject ____ Effectivity _______ Page ___________ AIRBORNE VIBRATION MONITORING 77-31-00 (AVM) SYSTEM
Description and Operation 1 ALL Conditioner - AVM Signal 1 Indicator - AVM 8 Sensors - Engine Vibration 1 Operation 8 Maintenance Practices 201 ALL System Test (S332T304) 220 System Test (S360N021-100, 201 -102) System Test 243 (S360N021-113/-114) System Test (S360N021-201, 227 -202) System Test (S360N021-213) 235
Adjustment/Test 501 ALL Operational Test 501 Self Test 508 CONDITIONER - AIRBORNE VIBRATION 77-31-03 MONITOR (AVM) SIGNAL Removal/Installation 401 ALL INDICATOR - AIRBORNE VIBRATION 77-31-04 MONITOR (AVM) Removal/Installation 401 [*] [*] AIRPLANES WITHOUT EIS SENSOR - ALTERNATE NO. 1 BEARING 77-31-01 (NOB) VIBRATION (FFCCV) Removal/Installation 401 ALL SENSOR - TRF VIBRATION (CORE) 77-31-02 Removal/Installation 401 ALL Inspection/Check 601 ALL
CBEJ Page 3 Mar 12/02 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. ////////////////////////A / / CFM56 ENGINES 737-300/400/500/ /MAINTENANCE MANUAL //////////////////////// ENGINE INDICATING SYSTEM - DESCRIPTION AND OPERATION ____________________________________________________ 1. General (Fig. 1) 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 发动机指示 ENGINE INDICATIN
