ATP CTP Course - Final Test
ATP CTP COURSE - FINAL TEST NEWEST 2025/2026 COMPLETE
QUESTIONS AND CORRECT DETAILED ANSWERS (VERIFIED
ANSWERS) |BRAND NEW VERSION!!
When operating at constant speed with constant thrust setting at high altitude
(typically above FL250) in slow flight below L/D Max airspeed, any disturbance
causing a decrease in airspeed will result in a further decrease in airspeed unless
thrust in increased. High altitude recovery from slow flight while turning is best
accomplished by: - Correct Answer-c. Increasing thrust to maximum available
thrust and reducing bank angle while accelerating to airspeed above L/D Max
speed. In a thrust limited situation, exiting slow flight will require an immediate
descent as an aerodynamic stall is imminent.
Maximum Altitude is the highest altitude at which an airplane can be operated.
Maximum Altitude for an airplane is: - Correct Answer-e. The lowest of the above
listed altitudes.
a) Maximum Certified Altitude - the altitude determined during certification set by
the pressurization structural load limits on the fuselage.
b) Thrust Limited Altitude - the altitude at which sufficient thrust is available to
provide a specific minimum rate of climb.
c) Buffet or Maneuver Limited Altitude - the altitude at which a specific maneuver
margin exists prior to buffet onset.
e) The lowest of the above listed altitudes.
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, ATP CTP Course - Final Test
Exceed the critical angle of attack and the surface will stall, and lift will decrease
instead of increasing. This is true: - Correct Answer-d. Regardless of airplane speed
or attitude.
Which of the following statements is true? - Correct Answer-d. Recovery from
approach to stall warning is the same as recovery from a stall.
The airplane angle of attack is the angle between the wing chord and the
oncoming air or relative wind. (True or False) - Correct Answer-True
Airplane stall speeds are published in the Approved Flight Manual for each
airplane model. These speeds are presented as a function of aircraft weight.
Therefore if the pilot maintains airspeed above the appropriate speed listed for
the aircraft weight, the aircraft will not stall. (True or False) - Correct Answer-False
The stall speed of an airplane: - Correct Answer-b. Is affected by weight and bank
angle.
Large downward aileron deflections: - Correct Answer-a. Could induce air
separation over that portion of the wing at very high angles of attack.
Place the following steps from the stall recovery template in the correct order: -
Correct Answer-d. Disconnect autopilot and autothrottle / auto thrust.
b. Apply nose down pitch control until impeding stall indications are eliminated.
c. Adjust bank angle to wings level.
f. Apply thrust as needed.
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, ATP CTP Course - Final Test
a. Retract speed brakes and spoilers.
e. Return to the desired flight path.
The predominant number of airplane upsets are caused by: - Correct Answer-a.
Environmental factors.
Most of the multi-engine turbojet loss-of-control incidents that are caused by
environmental factors because of: - Correct Answer-d. Wake turbulence
When initiating recommended airplane upset recovery techniques, the first two
techniques are: - Correct Answer-c. Recognize and confirm the situation and
disengage the autopilot and auto-throttles.
In a nose high, wings level airplane upset, after accomplishing the first two
recommended techniques: - Correct Answer-a. Apply up to full nosedown elevator
and consider trimming off some control force.
During recovery from a nose-low, high-bank-angle airplane upset: - Correct
Answer-b. It may be necessary to unload the airplane by decreasing backpressure.
When should an upset recovery be initiated? - Correct Answer-c. Whenever an
unintentional excessive divergence from the intended flight path and/or airspeed
occurs.
During recovery from an airplane upset: - Correct Answer-d. Pilots must be
prepared to use full control authority.
3|Page
ATP CTP COURSE - FINAL TEST NEWEST 2025/2026 COMPLETE
QUESTIONS AND CORRECT DETAILED ANSWERS (VERIFIED
ANSWERS) |BRAND NEW VERSION!!
When operating at constant speed with constant thrust setting at high altitude
(typically above FL250) in slow flight below L/D Max airspeed, any disturbance
causing a decrease in airspeed will result in a further decrease in airspeed unless
thrust in increased. High altitude recovery from slow flight while turning is best
accomplished by: - Correct Answer-c. Increasing thrust to maximum available
thrust and reducing bank angle while accelerating to airspeed above L/D Max
speed. In a thrust limited situation, exiting slow flight will require an immediate
descent as an aerodynamic stall is imminent.
Maximum Altitude is the highest altitude at which an airplane can be operated.
Maximum Altitude for an airplane is: - Correct Answer-e. The lowest of the above
listed altitudes.
a) Maximum Certified Altitude - the altitude determined during certification set by
the pressurization structural load limits on the fuselage.
b) Thrust Limited Altitude - the altitude at which sufficient thrust is available to
provide a specific minimum rate of climb.
c) Buffet or Maneuver Limited Altitude - the altitude at which a specific maneuver
margin exists prior to buffet onset.
e) The lowest of the above listed altitudes.
1|Page
, ATP CTP Course - Final Test
Exceed the critical angle of attack and the surface will stall, and lift will decrease
instead of increasing. This is true: - Correct Answer-d. Regardless of airplane speed
or attitude.
Which of the following statements is true? - Correct Answer-d. Recovery from
approach to stall warning is the same as recovery from a stall.
The airplane angle of attack is the angle between the wing chord and the
oncoming air or relative wind. (True or False) - Correct Answer-True
Airplane stall speeds are published in the Approved Flight Manual for each
airplane model. These speeds are presented as a function of aircraft weight.
Therefore if the pilot maintains airspeed above the appropriate speed listed for
the aircraft weight, the aircraft will not stall. (True or False) - Correct Answer-False
The stall speed of an airplane: - Correct Answer-b. Is affected by weight and bank
angle.
Large downward aileron deflections: - Correct Answer-a. Could induce air
separation over that portion of the wing at very high angles of attack.
Place the following steps from the stall recovery template in the correct order: -
Correct Answer-d. Disconnect autopilot and autothrottle / auto thrust.
b. Apply nose down pitch control until impeding stall indications are eliminated.
c. Adjust bank angle to wings level.
f. Apply thrust as needed.
2|Page
, ATP CTP Course - Final Test
a. Retract speed brakes and spoilers.
e. Return to the desired flight path.
The predominant number of airplane upsets are caused by: - Correct Answer-a.
Environmental factors.
Most of the multi-engine turbojet loss-of-control incidents that are caused by
environmental factors because of: - Correct Answer-d. Wake turbulence
When initiating recommended airplane upset recovery techniques, the first two
techniques are: - Correct Answer-c. Recognize and confirm the situation and
disengage the autopilot and auto-throttles.
In a nose high, wings level airplane upset, after accomplishing the first two
recommended techniques: - Correct Answer-a. Apply up to full nosedown elevator
and consider trimming off some control force.
During recovery from a nose-low, high-bank-angle airplane upset: - Correct
Answer-b. It may be necessary to unload the airplane by decreasing backpressure.
When should an upset recovery be initiated? - Correct Answer-c. Whenever an
unintentional excessive divergence from the intended flight path and/or airspeed
occurs.
During recovery from an airplane upset: - Correct Answer-d. Pilots must be
prepared to use full control authority.
3|Page
