Propellers Flashcards

1
Q

What is the construction material of the mt-Propeller?

A

Wood-composite construction with a fiber-reinforced plastic coating

The mt-Propeller features a combination of wood and advanced plastic materials for enhanced durability and performance.

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2
Q

What protects the inner edge of the mt-Propeller blades?

A

A rubber strip

This rubber strip is designed to provide additional protection against wear and damage.

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3
Q

What protects the outer edges of the mt-Propeller blades?

A

A stainless steel clad edge

The stainless steel edge adds strength and resistance to environmental factors.

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4
Q

What type of regulation does the mt-Propeller use?

A

Hydraulically regulated, constant speed, full-feathering

This mechanism allows for efficient and responsive control of the propeller’s pitch.

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5
Q

How are the blades moved to a coarse pitch?

A

By counterweights and spring tension

This system utilizes mechanical forces to adjust the blade pitch for optimal performance.

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6
Q

How are the blades moved to a fine pitch?

A

By gearbox oil pressure controlled by the CSU

The Constant Speed Unit (CSU) plays a critical role in adjusting the blade pitch based on engine performance.

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7
Q

What should be checked during a preflight propeller inspection?

A

Each blade, front and back, leading and trailing edges

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8
Q

What type of surface damage is common on propeller blades?

A

Surface nicks, especially on the rear face

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9
Q

What is the acceptable condition for minor surface nicks on propeller blades?

A

Minor surface nicks are acceptable

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10
Q

What maintenance is required if nicks or de-lamination exposes underlying wood fibers?

A

Maintenance is required

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11
Q

What condition indicates that maintenance is required in relation to the propeller hub?

A

If grease or oil appears to be leaking from the propeller hub

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12
Q

What does the ECU command the CSU to do?

A

Set optimum propeller RPM for percentage power commanded by pilot

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13
Q

How does the CSU control the propeller’s blade pitch?

A

By controlling the amount of gearbox oil in the propeller hub

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14
Q

What effect does increased oil volume in the hub have on the propeller?

A

Results in a finer blade pitch (higher RPM)

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15
Q

What is the oil pressure boosted by the Combi Pump?

A

Approximately 290 PSI

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16
Q

What is the maximum continuous power RPM?

A

2300 RPM

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17
Q

What is the overspeed limit and duration?

A

2500 RPM for up to 20 seconds

18
Q

What type of governor does the DA42NG use?

A

mt P-877-16 electric governor

19
Q

What is the maximum takeoff power RPM for the DA42NG?

A

2300 RPM (5 minutes total per flight)

20
Q

What is the maximum continuous power RPM for the DA42NG?

21
Q

What should be done before turning off the Engine Master?

A

Power lever should be at idle

22
Q

What happens to the propeller when the engine stops with RPM above 1300 RPM?

A

The propeller will feather

23
Q

What prevents the propeller from feathering below 1300 RPM?

A

Coarse stop pins

24
Q

What do the ECUs do as power is reduced while airborne?

A

Reduce propeller RPM until reaching 25%

25
Q

What action do the ECUs take below 25% power?

A

Increase propeller RPM to ensure feathering if the engine is shutdown

26
Q

True or False: Increased propeller RPM is associated with power settings below 25%.

27
Q

What may cause propeller blades to move to the highest RPM setting?

A

A malfunction

This can lead to a condition known as propeller over-speed.

28
Q

What should be done if over-speed occurs in a propeller?

A

Reduce power on the affected engine and terminate the flight as soon as practicable

This helps control the RPM.

29
Q

What action should be considered if unable to maintain 2300 RPM or less?

A

Consider shutting down the affected engine

This is crucial for safety if power reduction fails.

30
Q

What power setting should be used after takeoff in a DA42NG?

A

Reduce power levers to 92%

This should be done after reaching a safe altitude.

31
Q

What is the recommended engine power setting during climbs above 14,000 feet MSL?

A

Reduce power settings below 92%

This prevents RPM from entering the yellow range.

32
Q

What is the purpose of unfeathering accumulators?

A

Enable restarting an engine while airborne

They store pressurized gearbox oil to assist in propeller movement.

33
Q

What do unfeathering accumulators store?

A

Pressurized gearbox oil in a nitrogen-charged metal cylinder

This allows for the movement of the propeller out of the feathered position.

34
Q

What happens when the Engine Master switch is turned ON?

A

Accumulator releases gearbox oil to move the propeller out of the feathered position

This is essential for engine restart procedures.

35
Q

At what speeds is the starter used to start the engine?

A

Below 90 KIAS

This is important for safe engine start procedures.

36
Q

True or False: Engaging the starter while the propeller is wind-milling is safe.

A

False

It may result in an L/R ECU A/B FAILURE CAS message.

37
Q

What may happen if the starter is disengaged below 500 RPM?

A

It may cause damage to the gearbox

This highlights the importance of proper RPM management during engine operations.

38
Q

What is the maximum time allowed to restart an engine after shutting down for training purposes while airborne?

A

Within two minutes

Restart may not succeed if the engine is not restarted within this timeframe.

39
Q

What are the two types of air start procedures defined for the DA42NG?

A
  • Windmilling propeller at 120 to 140 KIAS
  • Engine starter at 85 to 100 KIAS
40
Q

What does FAA Airworthiness Directive 2018-18-02 limit regarding windmilling restart?

A

Use for emergencies only

This is to prevent failure of engine timing chain, loss of engine thrust control, and reduced control of the airplane.

41
Q

What may happen if the starter is engaged while the propeller is wind-milling?

A

An L/R ECU A/B FAILURE CAS message may occur

This is a warning to avoid engaging the starter under such conditions.