23. MODULE 17A (B1) — PROPELLER

32 multi-choice. Time allowed 40 minutes.

1 / 32

The Limits For Blade Angle Are Controlled By Pitch Stops On The

2 / 32

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

3 / 32

Manually Feathering A Hydromechanical Propeller Means To

4 / 32

A Line Of Indentations Across More Than 25% Of The Chord At One Blade Section Can Be

5 / 32

In The Beta Range, If The Power Lever Is Advanced To Increase The Fuel, The Blade Angle

6 / 32

In A Hydromatic (hamilton-standard) Propeller With Counterweights, What Is Used To Make The Propeller Move To Fine Pitch?

7 / 32

On An Underspeed Condition The Blades Are Turned To

8 / 32

Propeller Blade Sections Are Normally Measured In Intervals Of

9 / 32

If An Aircraft Is Placed In A Dive From Cruise, The Propeller Condition Will Be

10 / 32

Electrical Power Supplies On Large Aircraft, For Electrical Deicing Are

11 / 32

What Is The Angle Of Advance?

12 / 32

What Are Acceptable Methods For Marking Blade Stations On A Propeller Blade?

13 / 32

On A Free Turbine Engine It Is Possible To Vary The Propeller Rpm Whilst The Engine Rpm Remains Constant

14 / 32

How Is The Oil Pressure Delivery On A Hydromatic Propeller Normally Stopped
after The Blades Have Reached Their Full-feathered Position?

15 / 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

16 / 32

A Wooden Propeller In Storage

17 / 32

Pitch Control Using Torque Measuring Is For

18 / 32

A Propeller Blade Absorbs More Power At

19 / 32

If The Tip Of An Electrical Overshoe Is Torn

20 / 32

Low Torque Sensing Is Used To Initiate

21 / 32

A Compound Twin Spool Engine Is

22 / 32

The Function Of Counterweights On A Propeller Is

23 / 32

Aerodynamic Twisting Moment Tends To

24 / 32

A Windmilling Propeller Has

25 / 32

Blade Tracking Check Compares

26 / 32

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

27 / 32

The Function Of A Propeller Pitch Lock Is To Prevent The Propeller From

28 / 32

An Offset Fin Is Used To Counteract Propeller Slipstream Effect

29 / 32

A Propeller Blade Absorbs More Torque At

30 / 32

A Ducted Propeller Is Used Because

31 / 32

Indentations To The Blade Face Are Measured

32 / 32

A Propeller Has The Requirement Of A

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