Advanced Ground Instructor Exam
2025 Questions and Answers
When, considering the forces acting upon an airplane in straight and level flight at
constant airspeed, which statement is correct? - ✔✔Weight always acts vertically
towards the center of the Earth
The critical angle of attack at which a given aircraft stalls is dependent on the -
✔✔Design of the airplane
Which subsonic plane form provides the best lift coefficient? - ✔✔Elliptical wing
On which wing plane form, does the stall begin at the wing tip and progress inward
towards the wing route? - ✔✔Swept back wing
A rectangle wing, as compared to other wing plane forms, has a tendency to stall first at
the wing - ✔✔Root providing adequate stall warning
Aspect ratio of a wing is defined as the ratio of the - ✔✔Wingspan to the mean cord
A wing with a very high aspect ratio (in comparison with a low aspect ratio wing) will
have - ✔✔High lift with a low A. O. A. and less induced drag
At a constant velocity, in airflow, a high aspect ratio wing will have (in comparison
with a low aspect ratio wing) - ✔✔Decreased drag, especially at high angles of attack
COPYRIGHT © 2025 BY OLIVIA WEST, ALL RIGHTS RESERVED 1
, If an aircraft has negative dynamic and positive static stability, this will result in -
✔✔Divergent oscillations
During a steady climb, the rate of climb depends on - ✔✔Excess power
At the angle of bank is increased, the vertical component of lift - ✔✔Decreases and the
sink rate increases
The airspeed indicated by point D is - ✔✔Maximum structural cruising speed
As altitude increases, the indicated airspeed at which a given airplane stalls in a
particular configuration will - ✔✔Remain the same as at low altitude
An airplane leaving ground effect will - ✔✔Experience a pitch up tendency and require
less elevator travel
When rolling out of a Steepbank turn, what causes the Lord aileron to create more drag,
then when rolling into the turn - ✔✔The wings angle of attack is greater as the rollout is
started
Refer to figure 22. While rolling into a right turn, if the inclinometer appears as
illustrated in A, the HCL, & CF vectors would be acting on the aircraft as illustrated in -
✔✔2, and more right pedal pressure is needed to center the ball
Refer to figure 22. While rolling into a right turn, if the inclinometer appears as
illustrated in C, the HCL and CF vectors would be acting on the rotor craft as illustrated
in - ✔✔5, and less right pedal pressure is needed to center the ball
Refer to figure 22. While rolling out of a left, turn, if the inclinometer appears as
illustrated in A, the HCL and CF factors would be acting on the aircraft as illustrated in
- ✔✔4, and more right pedal pressure is needed to center the ball
COPYRIGHT © 2025 BY OLIVIA WEST, ALL RIGHTS RESERVED 2
2025 Questions and Answers
When, considering the forces acting upon an airplane in straight and level flight at
constant airspeed, which statement is correct? - ✔✔Weight always acts vertically
towards the center of the Earth
The critical angle of attack at which a given aircraft stalls is dependent on the -
✔✔Design of the airplane
Which subsonic plane form provides the best lift coefficient? - ✔✔Elliptical wing
On which wing plane form, does the stall begin at the wing tip and progress inward
towards the wing route? - ✔✔Swept back wing
A rectangle wing, as compared to other wing plane forms, has a tendency to stall first at
the wing - ✔✔Root providing adequate stall warning
Aspect ratio of a wing is defined as the ratio of the - ✔✔Wingspan to the mean cord
A wing with a very high aspect ratio (in comparison with a low aspect ratio wing) will
have - ✔✔High lift with a low A. O. A. and less induced drag
At a constant velocity, in airflow, a high aspect ratio wing will have (in comparison
with a low aspect ratio wing) - ✔✔Decreased drag, especially at high angles of attack
COPYRIGHT © 2025 BY OLIVIA WEST, ALL RIGHTS RESERVED 1
, If an aircraft has negative dynamic and positive static stability, this will result in -
✔✔Divergent oscillations
During a steady climb, the rate of climb depends on - ✔✔Excess power
At the angle of bank is increased, the vertical component of lift - ✔✔Decreases and the
sink rate increases
The airspeed indicated by point D is - ✔✔Maximum structural cruising speed
As altitude increases, the indicated airspeed at which a given airplane stalls in a
particular configuration will - ✔✔Remain the same as at low altitude
An airplane leaving ground effect will - ✔✔Experience a pitch up tendency and require
less elevator travel
When rolling out of a Steepbank turn, what causes the Lord aileron to create more drag,
then when rolling into the turn - ✔✔The wings angle of attack is greater as the rollout is
started
Refer to figure 22. While rolling into a right turn, if the inclinometer appears as
illustrated in A, the HCL, & CF vectors would be acting on the aircraft as illustrated in -
✔✔2, and more right pedal pressure is needed to center the ball
Refer to figure 22. While rolling into a right turn, if the inclinometer appears as
illustrated in C, the HCL and CF vectors would be acting on the rotor craft as illustrated
in - ✔✔5, and less right pedal pressure is needed to center the ball
Refer to figure 22. While rolling out of a left, turn, if the inclinometer appears as
illustrated in A, the HCL and CF factors would be acting on the aircraft as illustrated in
- ✔✔4, and more right pedal pressure is needed to center the ball
COPYRIGHT © 2025 BY OLIVIA WEST, ALL RIGHTS RESERVED 2
