DA 62 AFM Airplane Description
7.9 POWER PLANT
7.9.1 ENGINES, GENERAL
There are two Austro Engine E4P-C engines installed, which have the following
specifications:
- Liquid-cooled four-cylinder four-stroke engine with wet sump lubrication
- Inline construction
- Common rail direct injection
- Propeller speed reducing gear 1:1.69
- Digital engine control with integrated propeller governor (separate oil system)
- Turbo charger with intercooler
Displacement:
Max. power: 132.0 kW (177.0 DIN-HP) at 2300 RPM at sea level and ISA
Max. continuous power:126 kW (169.0 DIN-HP) at sea level and ISA
The indications for monitoring important engine parameters during operation are integrated
within the Garmin G1000 display. Each engine can only be operated with the ENGINE
MASTER switch ON. Each engine has an own ECU (Electrical Engine Control Unit) which
receives its electrical power from the generator when at least one engine is running. When
both engines are at standstill, the ECU receives its electrical power from the battery.
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019 Page 7 - 31
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