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Airplane Description

DA 42 NG AFM

 

 

7.9 POWER PLANT

7.9.1 ENGINES, GENERAL

There are two Austro Engine E4-B 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:

123.5 kW (165.6 DIN-HP) at 2300 RPM at sea level and ISA

Max. continuous power: 113.6 kW (152.3 DIN-HP) at 2100 RPM 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.

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DA 42 NG AFM

Airplane Description

 

 

7.9.2 PROPELLER

Two mt-Propeller MTV-6-R-C-F / CF 187-129 hydraulically regulated 3-bladed constant speed feathering propellers are installed. Each propeller has wood composite blades with fiber-reinforced plastic coating and stainless steel edge cladding; in the region of the propeller hub the leading edge is coated with adhesive PU foil. These blades combine the lowest weight whilst minimizing vibration.

Propeller Control

The propeller pitch control system consists of the P-877-16 mt-Propeller governor valve.

The pitch is set by the ECU via an electro-mechanical actuator on the governor. To change the blade pitch angle gearbox oil is pumped into the propeller hub. Increasing the oil pressure leads to a decrease of pitch and a higher RPM. Decreasing the pressure leads to higher pitch and a lower RPM.

Depending on the power setting the propeller pitch is adjusted such that the required RPM will be obtained as shown in the following diagram.

Doc. No. 7.01.15-E

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18-Feb-2009

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Airplane Description

DA 42 NG AFM

 

 

Pressure Accumulator:

The pressure accumulator is a nitrogen oil type. It is connected to the gearbox oil circuit via an electric valve at the accumulator, which is operated with the ENGINE MASTER switch.

When the ENGINE MASTER switch is set to ON the valve is opened. When the engine is running, the accumulator is filled with oil at a pressure of approximately 22 bar (320 psi).

During engine operation the accumulator makes sure that enough oil pressure is available even if the oil feed by the gearbox oil pump is decreasing due to negative acceleration.

The hydraulic pressure keeps the propeller pitch angle below the start lock position, or moves the propeller blades beyond the start lock position.

Feathering:

To feather the propeller the engine must be shut down with the appropriate ENGINE

MASTER switch. This will open the electric governor valve. All oil will flow back from the propeller hub, allowing the blades to move into the feathered pitch position. At the same time the electric valve at the pressure accumulator closes, and the oil pressure is restored in the accumulator.

Feathering is only possible at propeller speeds above 1300 RPM.

CAUTION

If the engine is shut down below an RPM of 1300 the propeller pitch remains below the start lock position. In this case the speed must be increased to increase the propeller RPM.

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DA 42 NG AFM

Airplane Description

 

 

Unfeathering:

To unfeather the propeller, the associated ENGINE MASTER switch must be set to ON.

This will open the electric valve at the pressure accumulator. The pressure stored in the accumulator will move the propeller blades into a low pitch position. As soon as the propeller starts turning and the gearbox oil operates, the accumulator will be refilled.

Ground Operation:

CAUTION

Operation on the ground at high RPM should be avoided as far as possible, as the blades could suffer stone damage. For this reason a suitable site for engine runs should be selected, where there are no loose stones or similar items.

WARNING

Never move the propeller by hand.

Doc. No. 7.01.15-E

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18-Feb-2009

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