2 General Information
In the present Operation Manual the proper operation of the aircraft engine E4P is documented.
With the publication of the Operation Manual Austro Engine GmbH ensures the correctness of the
instructions. In case of changes Austro Engine GmbH will inform with Service Bulletins, Service Letters
or manual amendments, if it is necessary.
In case of problems with the engine operation or any further questions about the engine,
contact Austro Engine GmbH.
The following symbols and warning signs are used in the manual to point out important instructions.
They must be heeded strictly to prevent personal injury and material damage, to insure operational
safety of the aircraft and to avoid any damage to the aircraft as a result of incorrect handling.
Warning: Disregarding these safety rules can cause personal injury or even death.
Caution: Disregarding these special instructions and safety measures can damage the
engine or other components.
Note: Additional not or instruction for better understanding of an instruction.
2.1 Description and Using
The E4P is a liquid-cooled, in-line four-stroke four cylinder engine with a double overhead camshaft
(DOHC) with four valves per cylinder. The valves are actuated by the cam follower
The direct fuel injection is realized by means of a common rail technique and the engine is charged by
a turbo charger in combination with an intercooler.
The propeller is activated by a directly integrated gearbox with an integral torsional vibration damper.
All engine components are controlled by an EECU system.
● This engine is only designed for pull propeller installations.
● The engine should not be operated without propeller.
● Only useable in aircraft.
● It is not capable for aerobatics use
● It is not allowed to run the engine without the specified quality and quantity of fluids.
● Only the use of recommended equipment and fluids grants a save run of the engine.
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