CHAPTER 77 - ENGINE INDICATING
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
ENGINE INDICATING 77-00-00
_________________ Description and Operation 1 ALL General 1
Component Location 101 ALL
Component Index
Component Location
POWER 77-10-00
_____ ENGINE PRESSURE RATIO INDICATING 77-11-00 SYSTEM
Description and Operation 1 ALL General 1 Indication - Engine Pressure 1
Ratio
Manifold - Engine Pressure 1
Ratio (PT4.95)
Probe - Engine Pressure Ratio 1
(PT4.95)
Probe - EEC Total Inlet 1
Pressure/Temperature
(PT2/TT2)
Operation 1 Adjustment/Test 501 ALL MANIFOLD - ENGINE PRESSURE RATIO 77-11-02
(PT4.95) Removal/Installation 401 ALL PROBE - ENGINE PRESSURE RATIO 77-11-01
(PT4.95) Removal/Installation 401 ALL Adjustment/Test 501 ALL Inspection/Check 601 ALL
77-CONTENTS
NGUN Page 1 Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
CHAPTER 77 - ENGINE INDICATING
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
ENGINE TACHOMETER SYSTEM 77-12-00
Description and Operation 1 ALL General 1 Alternator - EEC (N2 1
Transducer)
Indication 1
Speed Card - Engine 1
Transducer - EEC Speed (N1) 1
Operation 1
Adjustment/Test 501 ALL CARD - ENGINE SPEED 77-12-01 Removal/Installation 401 ALL
TEMPERATURE 77-20-00
___________ EXHAUST GAS TEMPERATURE INDICATING 77-21-00 SYSTEM
Description and Operation 1 ALL General 1 Cable - Thermocouple, EGT 1
(TT4.95)
Indication - Exhaust Gas 1
Temperature
Probe - Thermocouple, EGT 1
(TT4.95)
Terminal Box - EGT (TT4.95) 1
Thermocouple Cable
Operation 5 Adjustment/Test 501 ALL BOX - TERMINAL, THERMOCOUPLE 77-21-04
CABLE, EXHAUST GAS TEMPERATURE
(TT4.95) Removal/Installation 401 ALL Inspection/Check 601 ALL Cleaning/Painting 701 ALL
CABLE - THERMOCOUPLE, EXHAUST 77-21-02
GAS TEMPERATURE (TT4.95) Removal/Installation 401 ALL Inspection/Check 601 ALL
77-CONTENTS
NGUN Page 2 Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
CHAPTER 77 - ENGINE INDICATING
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
Cleaning/Painting 701 ALL HOUSING - THERMOCOUPLE, EXHAUST 77-21-05
GAS TEMPERATURE (TT4.95) Removal/Installation 401 ALL Inspection/Check 601 ALL
PROBE - THERMOCOUPLE, EXHAUST 77-21-01
GAS TEMPERATURE (TT4.95) Removal/Installation 401 ALL Inspection/Check 601 ALL Cleaning/Painting 701 ALL
ANALYZERS 77-30-00
_________ AIRBORNE VIBRATION MONITORING 77-31-00 (AVM) SYSTEM
Description and Operation 1 ALL General 1 Accelerometer - Engine 1 Indication 3 Signal Conditioner - Airborne 3
Vibration Monitoring (AVM) Operation 3 Adjustment/Test 501 ALL
Universal Airborne Vibration 503
Monitor (AVM) Signal
Conditioner - Self Test
Inspection/Check 601 ALL ACCELEROMETER - ENGINE 77-31-01 Removal/Installation 401 ALL CONDITIONER - SIGNAL, AIRBORNE 77-31-03 VIBRATION MONITOR Removal/Installation 401 ALL
77-CONTENTS
NGUN Page 3 Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
ENGINE INDICATING - DESCRIPTION AND OPERATION
_____________________________________________
1. General (Fig. 1 and 2)
_______
A. The engine indicating system includes these systems:
(1)
Engine Pressure Ratio (EPR) Indicating System (AMM 77-11-00)
(2)
Engine Tachometer System (AMM 77-12-00)
(3)
Exhaust Gas Temperature (EGT) Indicating System (AMM 77-21-00)
(4)
Airborne Vibration Monitoring (AVM) System (AMM 77-31-00)
B.
EPR Indicating System
(1)
The engine inlet pressure (PT2) and the exhaust gas pressure (PT4.95) of the engine are sent to the electronic engine control (EEC) where actual EPR is computed and transmitted to the EFIS/EICAS interface units (EIU's) for display on the main EICAS display.
C. 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：747-400 AMM 飛機維護手冊 發動機指示 ENGINE INDICATING
