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77-11-00 ENGINE TACHOMETER SYSTEM - N2 SPEED SENSOR 6 GUN ALL
77-11-00 ENGINE TACHOMETER SYSTEM - FUNCTIONAL DESCRIPTION 8 GUN ALL
77-21-00 EXHAUST GAS TEMPERATURE (EGT) INDICATING SYSTEM -
GENERAL DESCRIPTION
2 GUN ALL
77-21-00 EXHAUST GAS TEMPERATURE (EGT) INDICATING SYSTEM - EGT
THERMOCOUPLES AND HARNESSES
4 GUN ALL
77-21-00 EXHAUST GAS TEMPERATURE (EGT) INDICATING SYSTEM -
FUNCTIONAL DESCRIPTION
7 GUN ALL
77-31-00 AIRBORNE VIBRATION MONITORING (AVM) SYSTEM - GENERAL
DESCRIPTION
2 GUN ALL
77-31-00 AVM SYSTEM - COMPONENT LOCATION 6 GUN ALL
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER 10 GUN ALL
77-CONTENTS
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BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.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 77
Engine Indicating
CH-SC-SU Subject Page Effectivity
77-31-00 AVM SYSTEM - FUNCTIONAL DESCRIPTION 17 GUN ALL
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - MAIN MENU -
TRAINING INFORMATION POINT
23 GUN 001-099, 101-113, 115, 201-999
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - SELF TEST -
TRAINING INFORMATION POINT
28 GUN 001-099, 101-113, 115, 201-999
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - FAULT HISTORY -
TRAINING INFORMATION POINT
32 GUN 001-099, 101-113, 115, 201-999
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - FLIGHT HISTORY
PG 1 - TRAINING INFORMATION POINT
36 GUN 001-099, 101-113, 115, 201-999
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - FLIGHT HISTORY
PG 2 - TRAINING INFORMATION POINT
39 GUN 001-099, 101-113, 115, 201-999
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - BALANCE PG 1 -
TRAINING INFORMATION POINT
43 GUN 001-099, 101-113, 115, 201-999
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - BALANCE PG 2 -
TRAINING INFORMATION POINT
48 GUN 001-099, 101-113, 115, 201-999
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - BALANCE PG 3 -
TRAINING INFORMATION POINT
51 GUN 001-099, 101-113, 115, 201-999
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - BALANCE PG 4 -
TRAINING INFORMATION POINT
56 GUN 001-099, 101-113, 115, 201-999
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - BALANCE PG 5 -
TRAINING INFORMATION POINT
62 GUN 001-099, 101-113, 115, 201-999
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - MAIN MENU -
TRAINING INFORMATION POINT
67 GUN 114
77-CONTENTS
Page 2
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BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.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 77
Engine Indicating
CH-SC-SU Subject Page Effectivity
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - SELF TEST -
TRAINING INFORMATION POINT
70 GUN 114
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - SYSTEM FAULTS -
TRAINING INFORMATION POINT
72 GUN 114
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - FLIGHT HISTORY -
TRAINING INFORMATION POINT
74 GUN 114
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - ENGINE
BALANCE PG 1 - TRAINING INFORMATION POINT
76 GUN 114
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - ENGINE
BALANCE PG 2 - TRAINING INFORMATION POINT
78 GUN 114
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - ENGINE
BALANCE PG 3 - TRAINING INFORMATION POINT
80 GUN 114
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - ENGINE
BALANCE PG 4 - TRAINING INFORMATION POINT
82 GUN 114
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - ENGINE
BALANCE PG 5 - TRAINING INFORMATION POINT
85 GUN 114
77-31-00 AVM SYSTEM - AVM SIGNAL CONDITIONER BITE - ERASE STORED
DATA - TRAINING INFORMATION POINT
88 GUN 114
77-CONTENTS
Page 3
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 77
Engine Indicating
THIS PAGE IS INTENTIONALLY LEFT BLANK
77-00-00
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 indicating system continuously supplies engine
data to the common display system (CDS). The engine
indicating system has these subsystems:
* Low pressure rotor tachometer (N1)
* High pressure rotor tachometer (N2)
* Exhaust gas temperature (EGT)
* Airborne vibration monitoring (AVM).
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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ENGINE INDICATING(2)
