DGCA Module 17 Quiz Questions and Answers – Mock Test 1

DGCA Module 17 Propeller Quiz (Test 1) is helps to learners for understand how propellers convert engine power into thrust for efficient a/c movement. It focuses on the principles of blade pitch, aerodynamic forces and propeller efficiency during various flight conditions. Given About fixed pitch, variable pitch and constant speed propellers to understand how design affects performance.

The test trains to learners about evaluate torque, thrust, slipstream and aerodynamic drag. It also covers the governing systems, synchronization and feathering mechanisms to maintain smooth and safe operation. By learning these concepts, students gain insight into how propeller control impacts aircraft speed, fuel efficiency and stability.

This quiz questions is builds essential technical knowledge for aviation engineers and maintenance personnel. It prepares learners to identify and solve practical propeller related issues while ensuring operational safety and reliability. Through this test, they develop strong fundamentals for DGCA Module 17 examinations and real world maintenance tasks.

DGCA Module 17 Quiz Questions - Test 1

1 / 32

The optimum angle for a fixed pitch propeller is.

2 / 32

A left handed propeller is one that.

3 / 32

Forces acting on a propeller are.

4 / 32

The blade angle at the root is.

5 / 32

What force on a propeller blade turns the blades to a fine pitch?

6 / 32

Propeller blades are de-iced by.

7 / 32

Propeller slip rings.

8 / 32

On an electrical deicing system fast cycle is used.

9 / 32

High speed propellers are designed to.

10 / 32

When in the windmill position ATM.

11 / 32

Phosphate is not used bcoz.

12 / 32

Blades coming in contact with salt water should be washed with.

13 / 32

Propeller blade are stored in condition.

14 / 32

Static balance is done by.

15 / 32

Storage of propeller should be.

16 / 32

Auto feathering acomplies.

17 / 32

When speeder spring force dec. The blade angle will be.

18 / 32

If an propeller rotate in underspeed and the blade angle will be.

19 / 32

If an propeller rotate in overspeed and the blade angle will be.

20 / 32

Gyroscopic covering on propeller while storing.

21 / 32

The farthest portion of a propeller blade from hub is called.

22 / 32

The attaching part of a propeller blade from hub is called.

23 / 32

The attaching part of a propeller blade from hub is called.

24 / 32

The primary function front and rear cones when splined propeller shaft.

25 / 32

When flyweight overcome the speeder spling pressure it means.

26 / 32

Where air strike or frwd edge (thick side) of the propeller called.

27 / 32

The centre portion of the propeller called.

28 / 32

Where not air strike or bkwrd edge (thin side) of the propeller called.

29 / 32

Curved/cambered surface of the propeller called.

30 / 32

Flat/thrust surface of the propeller called.

31 / 32

Propeller convert.

32 / 32

One arm of propeller from hub to tip called.

Your score is

The average score is 44%

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All Modules Quiz Questions (For Better Practices)


Previous Years Question Papers (2017-2025)


Preparation Question Papers (Very Important Questions)


EASA DGCA All Module Books (Including Highlighted)


 

 


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