Engine Flashcards

1
Q

What type of engine powers the aircraft?

A

1600 SHP Pratt and Whitney PT6A-68B free turbine engine

This engine is designed for high performance and efficiency.

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2
Q

What is unique about the airflow in the engine?

A

It is a reverse flow engine

The air inlet is at the rear and the exhaust section is at the front.

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3
Q

What type of propeller does the engine drive?

A

Hartzell constant speed, variable pitch propeller with five graphite composite blades

The propeller rotates clockwise when viewed from the cockpit.

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4
Q

What system automatically manages engine power according to airspeed?

A

Electronic power management system (PMS)

This system ensures optimal performance during different flight conditions.

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5
Q

What power restriction does the PMS impose during take-off?

A

Restricts available engine power for take-off

Full power is available above 200 KIAS for sustained high cruise speeds.

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6
Q

Does the engine have a fire extinguisher?

A

No fire extinguisher

The engine has a fire warning system but lacks an extinguisher.

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7
Q

What are the main components of the gas generator section?

A

Compressor section, compressor turbine, combustion chamber

The compressor section includes 4 stages of axial compression and 1 stage of centrifugal/radial compression.

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8
Q

What drives the accessory gearbox at the rear of the engine?

A

Gas generator section

The fixed shaft connects the gas generator to the accessory gearbox.

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9
Q

List the items driven by the accessory gearbox.

A
  • Hydraulic pump
  • No. 1 generator (engine starter motor)
  • No. 2 generator
  • Low pressure fuel pump
  • High pressure fuel pump and fuel metering unit (FMU)
  • One triple element, triple inlet, main oil pressure pump
  • Two double element, gear type, oil scavenge pumps

These components are vital for engine operation and functionality.

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10
Q

How does the gas generator section contribute to the power turbine?

A

It uses generated gas flow to drive the power turbine section

This process is essential for converting gas energy into mechanical energy.

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11
Q

How many stages does the power turbine have?

A

Two-stage power turbine

This design allows for effective power conversion to drive the propeller.

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12
Q

What is the function of the reduction gearbox?

A

Mechanically drives the propeller

It connects the power turbine to the propeller for efficient operation.

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13
Q

In what directions do the compressor turbine and power turbine rotate?

A

They rotate in opposite directions

This configuration minimizes gyroscopic effects during flight.

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14
Q

How is air supplied to the engine?

A

Air is supplied to the engine through a chin intake in the front lower cowling.

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15
Q

What system is incorporated in the intake for icing conditions?

A

The intake system incorporates an inertial separation system operated by the INTAKE switch on the de-ice panel.

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16
Q

What happens to air after it enters the compressor?

A

Air leaves the compressor and is turned through 90° by diffuser tubes, converting velocity to static pressure.

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17
Q

What occurs in the combustion chamber?

A

High pressure air is turned through 180°, mixed with fuel, and ignited.

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18
Q

What directs gas to the single-stage compressor turbine?

A

Turbine inlet guide vanes direct the gas to the single-stage compressor turbine.

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19
Q

What happens after the gas drives the compressor turbine?

A

The gas continues forward to the two-stage power turbine and exhausts to atmosphere through two exhaust ports.

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20
Q

What is a design feature of the engine related to gas flow?

A

Reversing the direction of the gas flow produces a compact engine layout.

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21
Q

What controls the engine and propeller in response to pilot inputs?

A

The PMS controls the engine and propeller through the power control lever (PCL).

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22
Q

How is engine power controlled?

A

Engine power is controlled by gas generator speed (NG) set by the position of the PCL.

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23
Q

What does the propeller interface unit (PIU) do?

A

The PIU holds NP constant and torque becomes the measure of power level.

24
Q

What happens when NP increases to the governing speed?

A

The PIU holds the NP constant by varying the propeller pitch.

25
Q

What is the range of movement for the power control lever (PCL)?

A

The PCL has a range of movement of approximately 90°.

26
Q

What are the approximate PCL angles for engine operation?

A

FUEL OFF: -5°, IDLE: 30°, MAX: 80°.

27
Q

What happens in the FUEL OFF position?

A

The PCL cuts off the engine fuel supply mechanically and activates the propeller feathering system electrically.

28
Q

What does the friction control knob do?

A

The friction control knob increases the force needed to move the PCL when rotated clockwise.

29
Q

What is the purpose of the de-icing strips on propeller blades?

A

The de-icing strips prevent the build-up of ice on the surface of the blades.

30
Q

How do the de-icing strips work?

A

An electrically operated heater element melts the ice on the surface of the blade, and centrifugal force removes the melted ice.

31
Q

What protects the leading edge surfaces of each propeller blade?

A

An erosion strip protects the leading edge surfaces from the effects of erosion.

32
Q

What does the erosion strip provide in case of a lightning strike?

A

The erosion strip gives an earth path for the lightning.

33
Q

What is the function of the engine oil system?

A

The engine oil system provides a constant supply of clean oil to the engine bearings, reduction gears, accessory drives, and the PIU.

34
Q

How is oil supplied to the engine?

A

Oil is supplied from the oil tank by a three element pressure pump and is scavenged by two double element pumps.

35
Q

What does the oil system lubricate and cool?

A

The oil lubricates and cools the bearings, lubricates the gears and drives, and provides oil for propeller speed control.

36
Q

How is the oil cooled?

A

The oil is cooled by the airframe mounted oil cooler.

37
Q

Does the oil system require input from the pilot?

A

No, the oil system operates fully automatically with no input required from the pilot.

38
Q

What should be avoided to maintain oil pressure?

A

Manoeuvres causing the oil pressure to go outside the approved limits should be avoided.

39
Q

Where is the oil tank located?

A

The oil tank is an integral part of the accessory gearbox assembly.

40
Q

How is the oil level checked?

A

Oil contents are indicated by a sight glass on the left side of the compressor inlet case.

41
Q

What do the magnetic chip detectors do?

A

They attract ferrous contamination in the oil system.

42
Q

What happens if sufficient contamination is detected?

A

An amber CHIP indication on the DWP comes on.

43
Q

How is oil cooled in the system?

A

Oil is air-cooled by passing through an oil cooler in a duct under the engine bay.

44
Q

What regulates the temperature of the oil?

A

A thermal actuator automatically regulates the temperature of the oil.

45
Q

What happens to the external flap assembly when the NLG is extended?

A

The external flap is opened to allow increased airflow through the oil cooler at low speeds and on the ground.

46
Q

What is the purpose of the ignition system?

A

The ignition system is used to ignite the fuel/air mixture in the combustion chamber during engine start or rapid engine deceleration to reduce the risk of inadvertent flameout.

47
Q

How does the igniter exciter unit function?

A

A sealed igniter exciter unit transforms the 28V DC input to a pulsed high voltage output.

48
Q

What do the ignition cable assemblies do?

A

Two individual ignition cable assemblies carry electrical energy from the ignition exciter unit to the engine-mounted spark igniters.

49
Q

What is the normal position of the ignition switch?

A

The normal switch position is AUTO.

50
Q

What happens when the ignition switch is in the IGN position?

A

In the forward (IGN) position, the igniters are manually selected to ON.

51
Q

What occurs in the OFF position of the ignition switch?

A

If either front or rear cockpit switch is held to the rear (OFF) position, the igniters are inhibited.

52
Q

What does the AUTO position of the ignition switch do?

A

In the central (AUTO) position, the igniters function automatically, controlled by the PMU.

53
Q

What indicates that the igniters are operating?

A

A green IGN caption illuminates on both the DWP and the MFD ENG page whenever the igniters are operating.

54
Q

What functions are combined in the starter motor unit?

A

The functions of the starter motor and generator No. 1 (GEN 1) are combined in one unit.

55
Q

How can the starter motor be energized manually?

A

The starter motor can be energized manually by selecting the STARTER switch to MAN.

56
Q

What happens when the STARTER switch is set to AUTO?

A

When set to AUTO, the PMU automatically controls the starter motor and the auto start sequence starts when the AUTO START push-button is pressed.

57
Q

What appears on the MFD when the starter is activated?

A

Whenever the starter is activated, the MFD ENG page appears automatically on the right MFD.