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FAA Written Exam FAA 107 MAIN TEST SOURCE, FAA Part 107, FAA 107 2025 (ACTUAL EXAM) QUESTIONS AND VERIFIED ANSWERS NEWEST UPDATE LEARNING TEST LATEST VERSION RATED 100%

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FAA Written Exam FAA 107 MAIN TEST SOURCE, FAA Part 107, FAA 107 2025 (ACTUAL EXAM) QUESTIONS AND VERIFIED ANSWERS NEWEST UPDATE LEARNING TEST LATEST VERSION RATED 100%

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FAA Written Exam FAA 107 MAIN TEST
SOURCE, FAA Part 107, FAA 107 2025
(ACTUAL EXAM) QUESTIONS AND VERIFIED
ANSWERS NEWEST UPDATE LEARNING TEST
LATEST VERSION 2025 2026 RATED 100%




What is one purpose of wing flaps? - ANSWER-To enable the
pilot to make steeper approaches to a landing without
increasing the airspeed.


Which is not a primary flight control surface?
A. Flaps
B. Stabilator
C Ailerons - ANSWER-A. Flaps

,The elevator controls movement around which axis? - ANSWER-
Lateral.


Which statement is true concerning primary flight controls?
A. The effectiveness of each control surface increases with
speed because there is more flow over them
B. Only when all three primary flight controls move in sequence
do the airflow and pressure distribution change over and
around the airfoil.
C. Primary flight controls include ailerons, rudder, elevator, and
trim systems - ANSWER-A. The effectiveness of each control
surface increases with speed because there is more flow over
them.


Which of the following is true concerning flaps?
A. Flaps are attached to the leading edge of the wing and are
used to increase wing lift.
B. Flaps allow an increase in the angle of descent without
increasing airspeed.
C. Flaps are high drag devices deployed from the wings to
reduce lift. - ANSWER-B. Flaps allow and increase in the angle
of descent without increasing airspeed.

,Which device is a secondary flight control?
A. Spoilers
B. Ailerons
C. Stabilators - ANSWER-A. Spoilers


Trim systems are designed to do what? - ANSWER-They relieve
the pilot of the need to maintain constant back pressure on the
flight controls.


The four forces acting on an airplane in flight are: - ANSWER-
Lift, Weight, Thrust, & Drag


One of the main functions of flaps during approach and landing
is to: - ANSWER-Increase the angle of descent without
increasing the airspeed.


What is the purpose of the rudder on an airplane? - ANSWER-
To control yaw.


When are the four forces that act on an airplane in equilibrium?
- ANSWER-During unaccelerated flight.

, What is the relationship of lift, drag, thrust, and weight when
the airplane is in straight-and-level flight? - ANSWER-Lift equals
weight.
Thrust equals drag.


Which statement relates to Bernoulli's principle? - ANSWER-Air
traveling faster over the curve upper surface of an airfoil causes
lower pressure on the top surface.


The term "angle of attack" is defined as the angle... - ANSWER-
between the wing chord line and the relative wind.


Angle of attack is defined as the chord line of an airfoil and
the... - ANSWER-Direction of the relative wind.


The angle of attack at which an airplane wing stalls will... -
ANSWER-Remain the same regardless of gross weight.


As altitude increases, the indicated airspeed at which a given
airplane stalls in a particular configuration will... - ANSWER-
Remain the same regardless of altitude.

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