23. MODULE 17A (B1) — PROPELLER

32 multi-choice. Time allowed 40 minutes.

1 / 32

How is the oil pressure delivery on a hydromatic propeller normally stopped after the

2 / 32

A compound twin spool engine is

3 / 32

If force is applied to the speeder spring, what will happen?

4 / 32

A windmilling propeller has

5 / 32

Forces acting on a propeller are.

6 / 32

If The Tas Of An Aircraft Increases, The Csu(constant Speed Unit) Will

7 / 32

Electrical power supplies on large aircraft, for electrical deicing are

8 / 32

From reverse pitch, returning to normal pitch, the blade:

9 / 32

A conventional turboprop torque meter uses.

10 / 32

Temporary storage is generally defined as non use of aircraft for

11 / 32

To achieve reverse pitch the blade angle must be.

12 / 32

The Function Of Counterweights On A Propeller Is

13 / 32

If A 2 Blade Prop Is Placed On A Knife Edge And It Ends Up Horizontal (blades At 3 And 9 O’clock Positions), It Is Said To Be In Balance

14 / 32

How is oil pressure delivery to a hydromatic propeller normally stopped after feathering?

15 / 32

The purpose of blade twist is to.

16 / 32

Counterweights are fitted to blade root to.

17 / 32

The limits for a tracking check are.

18 / 32

What Is The Angle Of Advance?

19 / 32

Ground running an aircraft with a fixed pitch prop with its tail into wind causes the

20 / 32

When on the ground with the engine idling the prop control should be.

21 / 32

Ground Running An Aircraft With A fixed Pitch Prop With Its Tail Into Wind Causes The Engine Rpm T

22 / 32

When in reverse pitch, CTM will tend to move propeller blades towards:

23 / 32

If governor flywheel overcomes the speeder spring, it indicates.

24 / 32

On an electrical de-icing system, when is the ‘fast cycle’ typically used?

25 / 32

The output of an anti-icing pump is controlled by.

26 / 32

At constant rpm, advance per revolution depends on

27 / 32

Which of the following generally renders an aluminium alloy propeller

28 / 32

After a lightning strike.

29 / 32

Multi engine aircraft synchronising works by

30 / 32

Propellers exposed to salt spray should be flushed with.

31 / 32

The limits for blade angle are controlled by pitch stops on the

32 / 32

A line of indentations across more than 25% of the chord at one blade section can be

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