CPL PoF propeller revision

CPL PoF propeller revision

Professional Development

20 Qs

quiz-placeholder

Similar activities

Grooming Final Exam

Grooming Final Exam

Professional Development

20 Qs

Handling Objections - Multiple Projects

Handling Objections - Multiple Projects

Professional Development

20 Qs

Cinefilos

Cinefilos

KG - Professional Development

20 Qs

name that mk character

name that mk character

KG - Professional Development

15 Qs

Wild Rift Quiz

Wild Rift Quiz

Professional Development

20 Qs

Miss Operation_RAL

Miss Operation_RAL

Professional Development

15 Qs

Captain Airway to the Rescue!!

Captain Airway to the Rescue!!

University - Professional Development

15 Qs

SUNDOWNER1

SUNDOWNER1

Professional Development

15 Qs

CPL PoF propeller revision

CPL PoF propeller revision

Assessment

Quiz

Specialty, Other

Professional Development

Medium

Created by

Needs Remedial

Used 150+ times

FREE Resource

20 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The propeller is a rotating aerofoil:

True

False

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Blade angle is:

Angle between the chord line and the plane of rotation

Angle between the blade back and the plane of rotation

Angle between the chord line and RAF

Angle between the RAF and the blade back

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The blade face is:

The side of the propeller blade facing away from the pilot

The side of the propeller blade facing toward the pilot

The leading edge of the propeller

Where the blade and the spinner meet

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The angle between the RAF and the plane of rotation is known as:

AoA

Blade angle

Helix Angle

Angle of incidence

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the purpose of helical twist?

A reduction in blade angle towards the propeller tip to maintain best thrust/torque ratio

An increase in blade angle towards the propeller tip to maintain best thrust/torque ratio

A reduction in blade angle towards the propeller tip to maintain 16° AoA for the entire blade length

An increase in blade angle towards the propeller tip to 16° AoA for the entire blade length

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The most useful thrust is produced at approximately:

50% to blade radius

25% blade radius

75% blade radius

The entire blade radius assuming the propeller is twisted to maintain best AoA

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

An aircraft with a fixed pitch propeller is cruising at 120 knots and best cruise rpm. If the speed is increase without changing RPM what will happen to the AoA and efficiency of the propeller?

AoA will decrease and efficiency will increase

AoA will increase and efficiency will increase

AoA will decrease and efficiency will decrease

AoA will increase and efficiency will increase

Create a free account and access millions of resources

Create resources
Host any resource
Get auto-graded reports
or continue with
Microsoft
Apple
Others
By signing up, you agree to our Terms of Service & Privacy Policy
Already have an account?