Airplane Description DA 42 NG AFM
Page 7 - 56 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E
7.10.2 ELECTRICAL ENGINE CONTROL UNIT / ECU
Engine Control and Regulation
The electrical ECU is used to control the engine actuators (e.g. fuel injectors)
according to the engine sensor information. The ECU monitors, controls and
regulates all important parameters for engine operation.
Sensors installed are:
- Oil temperature (lubrication system engine) / OIL TEMP
- Oil pressure (lubrication system engine) / OIL PRES
- Coolant temperature / COOLANT TEMP
- Gearbox temperature / GEARBOX
- Camshaft RPM (twice)
- Crankshaft RPM (twice)
- Fuel pressure in the common rail
- Manifold pressure
- Manifold air temperature
- Ambient air pressure
- Propeller governor / oil pressure
- Power lever position (twice)
- Voltage
- Starter switch signal
- Fuel pressure
- VOTER switch signal
- ECU TEST switch signal
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