CPL PoF straight and level revision

CPL PoF straight and level revision

Professional Development

15 Qs

quiz-placeholder

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CPL PoF straight and level revision

CPL PoF straight and level revision

Assessment

Quiz

Specialty, Other

Professional Development

Easy

Created by

Needs Remedial

Used 47+ times

FREE Resource

15 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

1 min • 1 pt

The forces acting on an aircraft in straight and level flight are:

Weight, Lift, Thrust, Drag

Weight, Lift, Drag, Torque

Weight, Lift, Thrust, Drag

Weight, Lift, Thrust, Drag, Torque

2.

MULTIPLE CHOICE QUESTION

1 min • 1 pt

The lift and weight forces form a couple:

True. A nose down couple

False

True. A nose up couple

Whats a couple

3.

MULTIPLE CHOICE QUESTION

1 min • 1 pt

What forces create a nose up pitching moment?

Thrust and weight

Lift and Drag

Lift and Thrust

Thrust and Drag

4.

MULTIPLE CHOICE QUESTION

1 min • 1 pt

What is the purpose of the tail plane

Balance the passengers incase one is much heavier

Balance residual rolling moments

Balance residual pitching moments

Hold the elevator on

5.

MULTIPLE CHOICE QUESTION

1 min • 1 pt

In a low wing aircraft lowering flap will cause:

The change in the thrust/drag and lift/weight couples both cause a nose down pitching moment

The changes in the lift/weight couple causes a nose up pitching moment

The change in the thrust/drag and lift/weight couples both cause a nose up pitching moment

The changes in the thrust/drag couple cause a nose up pitching moment

6.

MULTIPLE SELECT QUESTION

1 min • 1 pt

Select all the correct statements regarding gear:

Raising and lowering the gear will cause a nose up moment

Raising and lowering the gear will cause a nose down moment

Raising the gear will cause a nose up moment

Raising the gear will cause a nose down moment

Lowering the gear will cause a nose down moment

7.

MULTIPLE CHOICE QUESTION

1 min • 1 pt

To maintain S&L flight, if the speed increases:

The AoA must be increased

S&L cannot be maintained if speed is increased

The AoA must be decreased

Flaps must be lowered

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