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THRUST REVERSER INDICATING SYSTEM - LINEAR VARIABLE DIFFERENTIAL TRANSFORMER
THRUST REVERSER INDICATING SYSTEM - LINEAR VARIABLE DIFFERENTIAL TRANSFORMER
EFFECTIVITY
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CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
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THRUST REVERSER INDICATING SYSTEM - LINEAR VARIABLE DIFFERENTIAL TRANSFORMER
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CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
General
A REVERSER light comes on when any of these conditions
happen:
* For 10.5 seconds after T/R stow command
* T/R stow control system component fault (except during a
deploy operation)
* T/R deploy control system component fault during deploy
operation.
The engine accessory unit (EAU) contains the logic necessary
to identify T/R control system component faults. The EAU
controls the REVERSER lights.
Stow Operation
The reverser lights usually comes on for 10.5 seconds after you
command a stow operation. This is because the hydraulic
isolation valves (HIV) temporarily stay in the arm position to
supply hydraulic power to the actuators for the stow operation.
This condition usually ends 10.5 seconds after the stow
command.
See the thrust reverser control system section for more
information. (SECTION 78-34)
Stow Fault Logic
The EAU identifies any of these conditions as a stow fault:
* Any sleeve stow sensor is near (10s after stow command)
* Any sleeve lock sensor is near (10s after stow command)
* Left or right sync lock voltage (26s after stow command)
* Directional control valve (DCV) sensor near (15s after stow
command)
* HIV sensor near (15s after stow command).
For any of these conditions the REVERSER light comes on. The
light goes out when the stow fault goes away. The master
caution and the ENG annunciator come on if the fault stays for
more than 13 seconds.
The REVERSER light will come on and stay on (latch) if the EAU
sees the arm switch fail to the deploy position. This is the only
stow fault that keeps the REVERSER light on. You must replace
the switch, deploy the T/R and reset the EAU to make the
REVERSER light go out.
Deploy Fault Logic
The EAU identifies any of these conditions as a deploy fault:
* Any sleeve stow sensor far (6s after deploy command)
* Any sleeve lock sensor far (6s after deploy command)
* No left or right sync lock voltage (2s after deploy command)
* Directional control valve (DCV) sensor far (6s after deploy
command)
* HIV sensor far (6s after deploy command).
THRUST REVERSER INDICATING SYSTEM - REVERSER LIGHT - FUNCTIONAL DESCRIPTION
EFFECTIVITY
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For any of these conditions the REVERSER light comes on. The
master caution and the ENG annunciator comes on if the fault
stays for more than 13 seconds.
A deploy fault keeps the reverser light on. You must fix the
problem which causes the fault, deploy the T/R, and clear
(reset) the EAU deploy fault memory before the reverser light
can go out.
Procedures in part two of the airplane maintenance manual
(AMM) show how to clear the EAU fault memory.
THRUST REVERSER INDICATING SYSTEM - REVERSER LIGHT - FUNCTIONAL DESCRIPTION
EFFECTIVITY
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THRUST REVERSER INDICATING SYSTEM - REVERSER LIGHT - FUNCTIONAL DESCRIPTION
THRUST REVERSER INDICATING SYSTEM - REVERSER LIGHT - FUNCTIONAL DESCRIPTION
EFFECTIVITY
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CFM56 ENGINES (CFM56-7) 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
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General
An amber REV message shows when one or both sleeves of a
T/R are more than 10 percent, but less than 90 percent to the
deploy position. The REV message changes to green when both
sleeves are more than 90 percent to the deploy position.
The electronic engine control (EEC) contains the logic which
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