Principles of Flight

Aircraft Motion

Flight Controls

Further Effects of the Flight Controls

Effects of Speed and Power

1 Quiz

Aircraft Motion Quiz

Physics of Aircraft

Units of Measurement

Pressure, Density and Airspeed

Bernoulli’s Principle and the Venturi

1 Quiz

Physics of Aircraft Quiz

Lift

Lift Terminology

Controlling Lift

The Lift Formula

1 Quiz

Drag

Lift/Drag Ratio

1 Quiz

Weight and Thrust

Aircraft Weight

Propeller Thrust

How Propellers Work

Propeller Effects

Thrust and Power

The Four Forces

1 Quiz

Weight and Thrust Quiz

Secondary Controls

1 Quiz

Secondary Controls Quiz

Stability

Aircraft Stability

Longitudinal Stability

1 Quiz

Straight and Level

Forces in Straight and Level Flight

Effect of Flap on Straight and Level Flight

1 Quiz

Straight and Level Quiz

Climbing

Forces in a Climb

Climb Angle vs Climb Rate

Factors Affecting the Climb

1 Quiz

Descending

Power Off Descent

Factors Affecting the Descent

Wind in a Descent

Power + Attitude = Performance

1 Quiz

Descending Quiz

Turning

Forces in a Turn

Load Factor in a Turn

Coordinated Turns

1 Quiz

Aircraft Design Features

Control Surface Balancing

1 Quiz

Aircraft Design Features Quiz

The Stall

What is a Stall?

CL and the Stall

Load Factor and Stalling

Flight Controls in a Stall

External Factors Affecting the Stall

1 Quiz

Practice Exam

Principles of Flight Exam

2 Quizzes

Principles of Flight Practice Questions

Principles of Flight Mock Exam

Secondary Controls Quiz

Principles of Flight The Trim Secondary Controls Quiz

Time limit: 0

Quiz Summary

0 of 12 Questions completed

Questions:

Information

You have already completed the quiz before. Hence you can not start it again.

Quiz is loading…

You must sign in or sign up to start the quiz.

You must first complete the following:

Results

Quiz complete. Results are being recorded.

Results

0 of 12 Questions answered correctly

Time has elapsed

You have reached 0 of 0 point(s), (0)

Earned Point(s): 0 of 0, (0)
0 Essay(s) Pending (Possible Point(s): 0)

Categories

Not categorized 0%

1
2
3
4
5
6
7
8
9
10
11
12

Current
Review
Answered
Correct
Incorrect

Question 1 of 12

1. Question
The maximum flap extension speed is known as:
- VFE
- VNE
- VS
- VLE
Correct

Incorrect
Question 2 of 12

2. Question
Extending flaps increases the lift created. One of the reasons this occurs is because:
- The aerofoil camber is increased
- The form drag decreases
- The angle of attack decreases
- The induced drag decreases
Correct

Incorrect
Question 3 of 12

3. Question
Which of the following statements regarding flaps is the most correct?
- Retracting flaps very close to the ground is not advisable as the loss of lift can cause a sudden increase in descent rate
- The flaps should be retracted immediately when initiating a go-around in order to reduce drag and maximise the rate of climb
- In the case of an emergency, flaps can be fully extended rapidly at any airspeed as they are designed to withstand the forces at all airspeeds below VNE
- Flaps, also known as speed brakes, are primarily used to slow the aircraft down during the approach to land
Correct

Incorrect
Question 4 of 12

4. Question
The use of a small flap setting instead of zero flap for takeoff and climb results in:
- a shorter takeoff ground run and shallower climb angle
- a shorter takeoff ground run and steeper climb angle
- a longer takeoff ground run and shallower climb angle
- a longer takeoff ground run and steeper climb angle
Correct

Incorrect
Question 5 of 12

5. Question
How do lift and drag change when setting flaps to a lower position?
- Lift increases, drag increases
- Lift increases, drag decreases
- Lift decreases, drag increases
- Lift decreases, drag decreases
Correct

Incorrect
Question 6 of 12

6. Question
When a simple trim tab is set in flight and its associated surface is moved, the tab:
- Position remains constant relative to the control surface
- Will move to a new position and will have to be reset
- Position remains constant relative to the airflow
- Will not move and will have to be reset
Correct

Incorrect
Question 7 of 12

7. Question
During cruise flight with constant power setting, an aircraft shows a permanent tendency to raise the nose. How can this tendency be eliminated?
- By deflecting the elevator trim tab upwards
- By shifting the center of gravity backwards
- By elevator deflection upwards
- By deflecting the elevator trim tab downwards
Correct

Incorrect
Question 8 of 12

8. Question
What is a bendable (ground adjustable) trim tab?
- A fixed tab attached to the rudder or the aileron
- A balance mass at a control surface
- A term for a rudder balance
- A trim device adjustable in flight
Correct

Incorrect
Question 9 of 12

9. Question
What is the task of trim tabs?
- Avoiding permanent control forces
- Reduction of adverse yaw
- Ensuring dynamic stability
- Adjusting bank angle to center of gravity position
Correct

Incorrect
Question 10 of 12

10. Question
The elevator trim tab is deflected upwards. Towards which position will the trim tab indicator have moved?
- Nose-down position
- Neutral position
- Laterally trimmed
- Nose-up position
Correct

Incorrect
Question 11 of 12

11. Question
To remain trimmed in straight and level flight, as speed increases:
- The elevator is deflected further downwards and the trim tab further upwards
- Both the elevator and the trim tab are deflected further downwards
- The elevator and trim tab do not move
- The elevator is deflected further upwards and the trim tab further downwards
Correct

Incorrect
Question 12 of 12

12. Question
Slats are:
- Lift augmentation devices that extend forwards from the leading edge to increase lift at lower airspeeds
- Lift augmentation devices that extend backwards from the trailing edge to increase lift at lower airspeeds
- Lift augmentation devices that extend backwards from the tailing edge to increase both lift and drag
- Lift augmentation devices that extend forwards from the leading edge to increase lift at higher airspeeds
Correct

Incorrect

Login

Accessing this course requires a login. Please enter your credentials below!

Username or Email Address

Password

Remember Me

Lost Your Password?