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INFORMATION POINT
40 GUN ALL
78-36-00 THRUST REVERSER INDICATING SYSTEM - INTRODUCTION 2 GUN ALL
78-36-00 THRUST REVERSER INDICATING SYSTEM - GENERAL DESCRIPTION 5 GUN ALL
78-36-00 THRUST REVERSER INDICATING SYSTEM - COMPONENT LOCATION
- FLIGHT COMPARTMENT
8 GUN ALL
78-36-00 THRUST REVERSER INDICATING SYSTEM - LINEAR VARIABLE
DIFFERENTIAL TRANSFORMER
10 GUN ALL
78-36-00 THRUST REVERSER INDICATING SYSTEM - REVERSER LIGHT -
FUNCTIONAL DESCRIPTION
13 GUN ALL
78-CONTENTS
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D633A101-GUN Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
CHAPTER 78
Engine Exhaust
CH-SC-SU Subject Page Effectivity
78-36-00 THRUST REVERSER INDICATING SYSTEM - REV MESSAGE -
FUNCTIONAL DESCRIPTION
16 GUN ALL
78-36-00 THRUST REVERSER INDICATING SYSTEM - TRAINING INFORMATION
POINT
18 GUN ALL
78-CONTENTS
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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BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.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 78
Engine Exhaust
THIS PAGE IS INTENTIONALLY LEFT BLANK
78-00-00
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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BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.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 exhaust system controls the direction of the engine
exhaust gases.
The engine exhaust system has these sub-systems:
* Turbine exhaust
* Thrust reverser (T/R).
Abbreviations and Acronyms
* A/T - autothrottle
* CDS - common display system
* CDU - control display unit
* DCV - directional control valve
* DEU - display electronics unit
* EAU - engine accessory unit
* EEC - electronic engine control
* ELEC - electrical
* ENG - engine
* FCC - flight control computer
* GND - ground
* HIV - hydraulic isolation valve
* INBD - inboard
* ind - indication
* ISV - isolation valve
* LVDT - linear variable differential transformer
* P - panel
* prox - proximity
* REF - reference
* RLY - relay
* RTO - rejected take off
* S - seconds
* seq - sequence
* SL - sync lock
* stby - standby
* SW - switch
* sync - synchronizing
* sys - system
* T/R - thrust reverser
ENGINE EXHAUST SYSTEM - INTRODUCTION
EFFECTIVITY
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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
78-00-00-000
ENGINE EXHAUST SYSTEM - INTRODUCTION
ENGINE EXHAUST SYSTEM - INTRODUCTION
EFFECTIVITY
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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
78-00-00-000
General
The engine exhaust system controls the direction of the turbine
exhaust gases and the fan air exhaust gases.
Turbine Exhaust System
The turbine exhaust system supplies an exit for the engine
exhaust gases. This exit increases the velocity of the exhaust
gases. This increases engine thrust.
The major components of the turbine exhaust system are the
exhaust nozzle and the exhaust plug.
Thrust Reverser System
The thrust reverser (T/R) system changes the direction of the
fan air exhaust to help create reverse thrust. The flight crew
uses reverse thrust to slow the airplane after landing or during
a rejected takeoff (RTO). The turbine exhaust airflow direction
does not change during reverse thrust. The T/R system has a
electro-hydraulic control system and an indicating system.
The T/R system has two thrust reversers. T/R 1 is the thrust
reverser for engine 1 (left). T/R 2 is the thrust reverser for
engine 2 (right).
Each T/R has a left and right half. Each half has a translating
sleeve which moves aft (deploy position) for reverse thrust. The
two sleeves work independently from each other. Fan air
exhaust goes out radially and forward when the translating
sleeves are in the deploy position.
Four hinges attach each T/R half to the strut. You must
deactivate the thrust reverser before you open a T/R half.
Latches are at the bottom of the two halves. The latches keep
the two halves together.
ENGINE EXHAUST SYSTEM - GENERAL DESCRIPTION
EFFECTIVITY
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