Engines-Propellers Flashcards

1
Q

The hydraulic over speed governor increases Propeller pitch when propeller speed exceeds approximately what?

A

1236 Np

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2
Q

The propeller synchro phase system uses which engines propeller as the master?

A

Engine #1

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3
Q

The pneumatic section of the overspeed Governor increases propeller pitch when propeller speed exceeds approximately what?

A

1309 NP

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4
Q

Auto feather is triggered when the failing engine falls below what?

A

28% torque

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5
Q

The propeller control unit is mounted on the what?

A

The reduction gearbox

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6
Q

The beta backup system provides protection against the propellers entering the beta ground range when ?

A

When the power levers are forward of the ground range

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7
Q

Propeller overspeed Governing is achieved how?

A

Hydraulically and Pneumatically

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8
Q

Should oil pressure be lost to the propeller control unit the pitch lock feature does what?

A

Prevents the blades from reducing the angle more than 1°

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9
Q

Prior to synchro phase system Activation the propellers must be manually synchronised to within what?

A

20 NP

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10
Q

The PCU controls blade angle by metering oil to one side of the pitch change mechanism, and is oppose by what?

A

Engine oil pressure

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11
Q

Aerodynamic loads on the propeller tend to drive the blades to what blade angles?

A

Low blade angles

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12
Q

The pitch lock feature stops the speed of the propeller increasing more than what?

A

More than 2% from the point of the oil pressure loss

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13
Q

How does the propeller governor set rpm using the condition leavers in the forward thrust range?

A

By adjusting spring pressure on a set of internal Governor flyweights

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14
Q

What two things feather the propeller?

A

The feather solenoid or the mechanical feather valve.

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15
Q

At what blade angle do you get the propeller ground range indication lights?

A

+16.5° which corresponds to just below flight idle

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16
Q

The beta backup protection system uses what solenoid?

A

Uses the feather solenoid causing the propeller to begin feathering until blade angle increases past the ground range point.

17
Q

When does the auto feather arm?

A

Above 38% engine Tq

18
Q

When is power up trim cancelled?

A

When auto feather is selected off

19
Q

Alternate feather is inhibited when?

A

The power levers are in the ground range

20
Q

An unfeather selection energises what?

A

Energises the related auxiliary feathering pump which runs for approximately 18 seconds to provide supplemental oil pressure to unfeathet the propeller