SLEEVE - TRANSLATING 78-31-02
Removal/Installation 401 ALL
TENSION LATCHES 78-31-11
Removal/Installation 401 ALL
Adjustment/Test 501 ALL
THRUST REVERSER 78-31-01 Removal/Installation 401 CONFIG 1 - [*] [*] COWL/REVERSERS USED ON STRUTS WITHOUT VIBRATION ISOLATOR SUSPENSION
Removal/Installation 401 CONFIG 2 - [*] [*] COWL/REVERSERS USED ON STRUTS WITH VIBRATION ISOLATOR SUSPENSION AND WITH HINGE CROSS RODS (AIRPLANES PRE-BOEING-SB 737-54-1036)
Removal/Installation 401 CONFIG 3 - [*] [*] COWL/REVERSERS USED ON STRUTS WITH VIBRATION ISOLATOR SUSPENSION AND WITH CROSS BEAMS (AIRPLANES POST-BOEING-SB 737-54-1036)
Cleaning/Painting 701 ALL
Approved Repairs 801 ALL
THRUST REVERSER - AUXILIARY 78-31-13
SLIDER
Inspection/Check 601 ALL
THRUST REVERSER - AUXILIARY 78-31-12
TRACK
Inspection/Check 601 ALL
78-CONTENTS
CBEJ Page 3 Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
CHAPTER 78 - EXHAUST
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
THRUST REVERSER CONTROL SYSTEM 78-34-00
Description and Operation 1 ALL
Cables - Thrust Reverser 2
Feedback Push-Pull
Hydraulic Fuse, Thrust 1
Reverser
Sensor - Not Stow and Auto 2
Restow Proximity
Valve Module - Thrust Reverser 1
Control
Valve, Thrust Reverser Shuttle 1
Operation 2
CABLES - PUSH-PULL, FEEDBACK 78-34-02
Maintenance Practices 201 ALL General 201 Adjust Feedback Push-Pull 208
Cable Install Feedback Push-Pull 206 Cable Remove Feedback Push-Pull 201 Cable FUSES - VOLUMETRIC HYDRAULIC 78-34-07 Removal/Installation 401 ALL PROXIMITY SENSORS 78-34-03
Removal/Installation 401 ALL General 401 Install the Proximity 406
Sensors Remove the Proximity Sensors 401 Adjustment/Test 501 ALL Adjust the Proximity Sensors 501 SHUTTLE VALVE 78-34-11 Removal/Installation 401 ALL SWITCH, CONTROL - THRUST 78-34-04 REVERSER
Maintenance Practices 201 ALL Switch Adjustment 205 Switch Installation 204 Switch Removal 201
78-CONTENTS
CBEJ Page 4 Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
CHAPTER 78 - EXHAUST
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
SWITCHES, ARM AND STOW - THRUST 78-34-05
REVERSER
Maintenance Practices 201 CONFIG 1 [*] Switch Adjustment 209 Switch Installation 208 Switch Removal 201
[*] AIRPLANES WITH RAKE ACTUATED ARM AND STOW SWITCHES
Maintenance Practices 201 CONFIG 2 [*] General 201 Switch 205
Installation/Adjustment
Switch Removal 201
[*] AIRPLANES WITH PADDLE ACTUATED ARM AND STOW SWITCHES
SYNC LOCK - THRUST REVERSER 78-34-10
Removal/Installation 401 ALL
THRUST REVERSER CONTROL VALVE 78-34-01
MODULE
Removal/Installation 401 ALL
UNIT - ENGINE ACCESSORY 78-34-06
Removal/Installation 401 ALL
THRUST REVERSER INDICATING SYSTEM 78-36-00
Description and Operation 1 ALL
General 1
Lights - Indicator 1
Switches - Proximity 10
Unit - Engine Accessory (EAU) 6
Operation 10
78-CONTENTS
CBEJ Page 5 Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
EXHAUST - DESCRIPTION AND OPERATION
___________________________________
1. General
_______
A. The exhaust system receives and discharges the fan and turbine air through separate propelling nozzles to the atmosphere at a velocity and direction to produce the required thrust.
2. Turbine Exhaust (Fig. 1)
_______________
A. The turbine exhaust system provides an efficient exit for the turbine exhaust. The turbine exhaust consists of hot, combusted gases exiting the low pressure turbine at high velocity. The major components of the turbine exhaust system are the turbine exhaust sleeve and turbine exhaust plug.
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