ATPL - AGK Exam Questions and Answers
with Verified Solutions | Latest Updated
2026
1. Which of the following is B. Elevator.
considered a primary flight
control? A. Slats. B. Elevator.
C. Dorsal fin.
2. Which of the following are C. Outboard ailerons.
considered primary flight
controls? A. Tabs. B. Flaps. C.
Outboard ailerons.
3. Which of the following is C. Leading-edge flaps.
considered an auxiliary flight
control? A. Ruddervator. B.
Upper rudder. C. Leading-edge
flaps.
4. When are inboard ailerons C. Low-speed and high-speed flight.
normally used? A. Low-speed
flight only. B. High-speed flight
only. C. Low-speed and
high-speed flight.
5. When are outboard ailerons A. Low-speed flight only.
normally used? A. Low-speed
flight only. B. High-speed flight
only. C. Low-speed and
high-speed flight.
,6. Why do some airplanes B. Aerodynamic loads on the
equipped with outboard ailerons tend to twist the
inboard/outboard ailerons use wingtips at high speeds.
the outboards for slow flight
only? A. Increased surface
area provides greater
controllability with flap
extension. B. Aerodynamic
loads on the outboard ailerons
tend to twist the wingtips at
high speeds. C. Locking out
the outboard ailerons in
high-speed flight provides
variable flight control feel.
7. What is the purpose of a A. Move the flight controls in the
control tab? A. Move the flight event of manual reversion.
controls in the event of
manual reversion. B. Reduce
control forces by deflecting in
the proper direction to move a
primary flight control. C.
Prevent a control surface from
moving to a full-deflection
position due to aerodynamic
forces.
8. What is the purpose of an C. Modify the downward tail load for
elevator trim tab? A. Provide various airspeeds in flight
horizontal balance as airspeed eliminating flight-control pressures.
is increased to allow hands-off
flight. B. Adjust the speed tail
load for different airspeeds in
flight allowing neutral control
, forces. C. Modify the
downward tail load for various
airspeeds in flight eliminating
flight-control pressures.
9. Which direction from the C. Remains fixed for all positions.
primary control surface does
an elevator adjustable trim tab
move when the control surface
is moved? A. Same direction.
B. Opposite direction. C.
Remains fixed for all positions.
10. What is the purpose of a B. Reduce control forces by
servo tab? A. Move the flight deflecting in the proper direction to
controls in the event of move a primary flight control.
manual reversion. B. Reduce
control forces by deflecting in
the proper direction to move a
primary flight control. C.
Prevent a control surface from
moving to a full-deflection
position due to aerodynamic
forces.
11. Which direction from the B. Opposite direction.
primary control surface does a
servo tab move? A. Same
direction. B. Opposite
direction. C. Remains fixed for
all positions.
12. What is the purpose of an C. Prevent a control surface from
anti-servo tab? A. Move the moving to a full-deflection position
with Verified Solutions | Latest Updated
2026
1. Which of the following is B. Elevator.
considered a primary flight
control? A. Slats. B. Elevator.
C. Dorsal fin.
2. Which of the following are C. Outboard ailerons.
considered primary flight
controls? A. Tabs. B. Flaps. C.
Outboard ailerons.
3. Which of the following is C. Leading-edge flaps.
considered an auxiliary flight
control? A. Ruddervator. B.
Upper rudder. C. Leading-edge
flaps.
4. When are inboard ailerons C. Low-speed and high-speed flight.
normally used? A. Low-speed
flight only. B. High-speed flight
only. C. Low-speed and
high-speed flight.
5. When are outboard ailerons A. Low-speed flight only.
normally used? A. Low-speed
flight only. B. High-speed flight
only. C. Low-speed and
high-speed flight.
,6. Why do some airplanes B. Aerodynamic loads on the
equipped with outboard ailerons tend to twist the
inboard/outboard ailerons use wingtips at high speeds.
the outboards for slow flight
only? A. Increased surface
area provides greater
controllability with flap
extension. B. Aerodynamic
loads on the outboard ailerons
tend to twist the wingtips at
high speeds. C. Locking out
the outboard ailerons in
high-speed flight provides
variable flight control feel.
7. What is the purpose of a A. Move the flight controls in the
control tab? A. Move the flight event of manual reversion.
controls in the event of
manual reversion. B. Reduce
control forces by deflecting in
the proper direction to move a
primary flight control. C.
Prevent a control surface from
moving to a full-deflection
position due to aerodynamic
forces.
8. What is the purpose of an C. Modify the downward tail load for
elevator trim tab? A. Provide various airspeeds in flight
horizontal balance as airspeed eliminating flight-control pressures.
is increased to allow hands-off
flight. B. Adjust the speed tail
load for different airspeeds in
flight allowing neutral control
, forces. C. Modify the
downward tail load for various
airspeeds in flight eliminating
flight-control pressures.
9. Which direction from the C. Remains fixed for all positions.
primary control surface does
an elevator adjustable trim tab
move when the control surface
is moved? A. Same direction.
B. Opposite direction. C.
Remains fixed for all positions.
10. What is the purpose of a B. Reduce control forces by
servo tab? A. Move the flight deflecting in the proper direction to
controls in the event of move a primary flight control.
manual reversion. B. Reduce
control forces by deflecting in
the proper direction to move a
primary flight control. C.
Prevent a control surface from
moving to a full-deflection
position due to aerodynamic
forces.
11. Which direction from the B. Opposite direction.
primary control surface does a
servo tab move? A. Same
direction. B. Opposite
direction. C. Remains fixed for
all positions.
12. What is the purpose of an C. Prevent a control surface from
anti-servo tab? A. Move the moving to a full-deflection position
