DA-42 Engine/Fuel Flashcards

1
Q

When I flip the engine master on, what is getting power?

A

Engine, Engine Preheat System (glow plugs), Un-feathering accumulator

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2
Q

How does the fire protection work?

A

Bi-Metal switches, heat at different rates, bend and contact a switch. 250 C

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3
Q

When does the L/R Fuel Low warning come on?

A

When there is 4 +- 1 gal in the tank.

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4
Q

What does the check valve on the bottom of the fuel tank do?

A

Allows air to enter

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5
Q

What does the relief pressure valve do?

A

Allows air and fuel to exit

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6
Q

What is the horsepower at 2300 RPM’s?

A

135

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7
Q

What does the pressure relief valve protect agains?

A

Protects against a high pressure

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8
Q

What is the common rail?

A

High Pressure fuel reservoir that supplies fuel to the injectors

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9
Q

What is the fuel pressure in the rail measured by?

A

The rail pressure sensor

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10
Q

What does a higher fuel pressure do?

A

Ensures better vaporization and therefore better combustion.

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11
Q

Where is the high pressure pump getting the fuel from?

A

The low pressure fuel pump

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12
Q

What is a bar in relation to PSI?

A

14.5

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13
Q

What does the fuel metering unit do?

A

Ensures that only the required quantity of fuel is compressed.

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14
Q

What controls the rail pressure?

A

The rail pressure valve

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15
Q

How much excessive fuel is brought in?

A

4,5l/min

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16
Q

What does the extra fuel do?

A

Cool and lubricates the high pressure pump

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17
Q

What does TVD stand for?

A

Torsion Vibration Damper

18
Q

What is the maximum permitted engine speed?

19
Q

What is the maximum engine overspeed?

A

2500rpm max for 20 seconds

20
Q

Engine MCT (%)?

21
Q

Fuel temperature temp range?

22
Q

Oil pressure range?

A

1.0/6.5 bar

23
Q

Oil quantity (per engine)?

A

Quantity Min 4.5/ max 6.0 ltr consumption - 0.1 ltr/hr

24
Q

Oil temp range?

A

-30/+140*C

25
Gearbox max temp?
120\*C
26
Coolant temp range?
-30\*C/+105\*C freezing point of coolant is -36\*C
27
Voltage range? Amperage max?
24.1/32 V 60 Amps
28
Prop steps
12\* - low pitch 15\* - start lock 81\* - feathered
29
Restart envelope of TAE-02-99?
Max PA 8000' ASI 80/120 KIAS
30
What are the fuel tank capacities (useable)?
MAIN - 2\*25USG AUX - 2\*13.2USG
31
Describe the Pressure Accumulator function
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 20 bar (290 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.
32
Describe the journey of the fuel from the tanks to the engine and back
On each engine fuel is injected with high pressure directly into the cylinders. The injection nozzles (one per cylinder) are supplied with fuel by the common rail. Pressure inside the rail is generated by a high pressure pump which receives fuel from a low pressure pump. Depending on the power setting the rail pressure is controlled by the ECU through an electric valve. Both pumps are powered mechanically by the engine. Fuel that is not injected is fed back into the appropriate wing tank.
33
Describe the MAIN and AUX fuel tanks
**MAIN** * consists of three aluminum chambers which are connected by a flexible hose. * (1 US gal) of fuel in each wing are unusable, so that a total quantity of 94.6 liter (25 US gal) in each wing is usable * There are two tank vents. One includes a check valve with a capillary and one includes a relief pressure valve, which operates at 150 mbar (2 PSI) **AUX** * The vent line for the auxiliary fuel tank has a check valve with capillary. It allows air to enter the tank but prevents flow of fuel to the outside. The capillary equalizes the air pressure during climb
34
Describe the cooling system
Each engine is liquid cooled. The liquid cooling system consists of a radiator and a bypass to this radiator. The bypass is in operation when coolant temperatures are low. It therefore allows the engine to warm-up quickly. Upon reaching a certain temperature (approximately 88 °C or 190 °F) the radiator is activated by a thermostat valve. Additionally a coolant to air heat exchanger is provided for the cabin heat system. The flow through the heat exchanger is independent of the coolant temperature. An expansion tank helps to adjust the pressure in the system. The system is protected against over pressure by means of a pressure relief valve.
35
Describe the oil systems of the DA42
1. **Lubrication System (Engine and Turbo-Charger)** wet sump lubrication system; oil is cooled by a separate cooler on the underside of the engine. 2. **Gearbox and Propeller Governor System**
36
What is the waste gate based on?
The bypass is controlled by the ECU through the waste gate valve. A manifold pressure sensor behind the compressor allows the ECU to calculate the correct position of the waste gate valve
37
Why do you cool the air after you make it hot?
Cooler air makes it more dense
38
Describe the engine induction system (+ turbo)
39
Describe the DA42 FIRE DETECTION SYSTEM
consists of an overheat detector in the hot area of each engine. In case of an increase of the engine compartment temperature above 250 °C (480 °F) the overheat detector closes the electric circuit and a warning message appears in the annunciation window of the G1000 PFD. CAUTION If the aural alert or the warning does not appear, an unscheduled maintenance is necessary.
40
How many ECUs make 1 FADEC?
2 ECUs make 1 FADEC
41
Your DA42 can use diesel, and the airfield you land at offers you to put in diesel. Can you do it?
No, only JET A1 may be used (CTC SOP)
42
What is the oil guidance on the DA42? How much can you dispatch with? What is the recommended level for dispatch?
* -The absolute minimum oil level required as stated in the AFM is 4.5 Litres. * Plan to land with minimum 4.5 Litres. For land-away flights, take a spare bottle per engine. (if unused, return after flight). * -In order to ensure oil will remain sufficient throughout the flight, dispatch with a minimum of 5 Litres. * - The oil level shall be between 5 and 6 Litres, about 1/2cm above the bottom red mark