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ALL CFM56-5B ENGINES FOR A319-A320-A321
ENGINE SYSTEMS Jan 03
CFMI PROPRIETARY INFORMATION
CFM56-5B TRAINING MANUAL
EFG
ENGINE SENSORS
TRF vibration sensor.
The TRF vibration sensor is secured at the 12 o’clock position on the turbine rear frame.
It is a 50 pC/g piezo-electric sensor.
A semi-rigid cable is routed from the vibration sensor to an electrical connector, which is secured on a bracket on the core engine at the 10 o’clock position.
The TRF vibration sensor monitors the vertical acceleration of the rotors and sends the analogue signals to the EVMU for vibration analysis processing.
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ALL CFM56-5B ENGINES FOR A319-A320-A321
ENGINE SYSTEMS Jan 03
CFMI PROPRIETARY INFORMATION
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EFG
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ENGINE WIRING HARNESSES
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ALL CFM56-5B ENGINES FOR A319-A320-A321
ENGINE SYSTEMS Jan 03
CFMI PROPRIETARY INFORMATION
CFM56-5B TRAINING MANUAL
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ENGINE WIRING HARNESSES
Two types of harnesses are used, depending on where they are installed on the engine.
Fan section.
Harnesses that run on the fan inlet case and the fan frame, have a conventional design.
Cold section harnesses are designated :
-HJ7, HJ8, HJ9, HJ10, HJ11, HJ12, HJ13, DPM.
DPM is the harness routed from the Master Chip Detector (MCD) to the visual contamination indicator.
Core engine section.
Harnesses routed along the core engine section have a special design that can withstand high temperatures.
Hot section harnesses are designated :
-HCJ11L, HCJ11R, HCJ12L, HCJ12R, HCJ13.
EFG
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ALL CFM56-5B ENGINES FOR A319-A320-A321
ENGINE SYSTEMS Jan 03
CFMI PROPRIETARY INFORMATION
CFM56-5B TRAINING MANUAL
EFG
ENGINE WIRING HARNESSES
The electrical harnesses ensure the connections between the various electrical, electronic and electro-mechanical components, mounted on the engine.
All the harnesses converge to the 6 o’clock junction box, which provides an interface between the two types.
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