What is one purpose of wing flaps?
Flight Controls Quiz

Quiz
•
Other
•
12th Grade
•
Hard
Rick Chapman
Used 5+ times
FREE Resource
9 questions
Show all answers
1.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
To enable the pilot to make steeper approaches to a landing without increasing the airspeed.
To relieve the pilot of maintaining continuous pressure on the controls.
To decrease wing area to vary the lift.
2.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
One of the main functions of flaps during approach and landing is to
decrease the angle of descent without increasing the airspeed.
permit a touchdown at a higher indicated airspeed.
increase the angle of descent without increasing the airspeed.
3.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the purpose of the rudder on an airplane?
To control yaw.
To control overbanking tendency.
To control roll.
4.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Which is not a primary flight control surface?
Flaps.
Stabilator.
Ailerons.
5.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
The elevator controls movement around which axis?
Longitudinal.
Lateral.
Vertical.
6.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Which of the following is true concerning flaps?
Flaps are attached to the leading edge of the wing and are used to increase wing lift.
Flaps allow an increase in the angle of descent without increasing airspeed.
Flaps are high drag devices deployed from the wings to reduce lift.
7.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Which device is a secondary flight control?
Spoilers.
Ailerons.
Stabilators.
8.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Trim systems are designed to do what?
They relieve the pilot of the need to maintain constant pressure on the flight controls.
They are used during approach and landing to increase wing lift.
They move in the opposite direction from one another to control roll.
9.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Which statement is true concerning primary flight controls?
The effectiveness of each control surface increases with speed because there is more airflow over them.
Only when all three primary flight controls move in sequence do the airflow and pressure distribution change over and around the airfoil.
Primary flight controls include ailerons, rudder, elevator, and trim systems.
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