ATP CTP Course Final Test with all Correct & 100%
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Graded A+ (Just Released)
Which of the following statements regarding energy is true? ✔Correct Answer-d. Kinetic
energy can be traded for potential energy, and potential energy can be traded for kinetic energy
The objective in maneuvering the airplane is to manage energy so that: ✔Correct Answer-d.
All of the above
What is the effect on total drag if airspeed slows below L/D Max? ✔Correct Answer-c. Drag
increases because of increased induced drag.
A jet pilot flying at L/D Max will obtain best: ✔Correct Answer-b. Endurance
When a jet aircraft is flown at the appropriate airspeed for maximum range, which type of drag
predominates? ✔Correct Answer-a. Parasite
While already at high speed, what happens if Mach is allowed to increase? ✔Correct Answer-
d. All of the above
What is the result of a shock-induced separation of airflow occurring symmetrically near the
wing root of a swept wing aircraft? ✔Correct Answer-c. A severe moment of "Mach tuck"
The speed of sound generally decreases with increasing altitude. This occurs because:
✔Correct Answer-a. The air temperature decreases.
Critical Mach number can be defined as: ✔Correct Answer-c. The speed of an aircraft in which
airflow over any part of the aircraft or structure first reaches, but doesn't exceed Mach 1.0.
Stability in the vertical axis tends to drive the sideslip angle toward zero. The most dynamic
stability about the vertical axis on modern jet transports is from: ✔Correct Answer-c. An
active stability augmentation system / yaw damper.
Swept wings cause a significant: ✔Correct Answer-b. Reduction in effectiveness of flaps.
Why is convergence of Stall AOA and Mmo hazardous? ✔Correct Answer-d. All of the above
To maintain altitude in a banked turn, the lift produced by the airplane must be: ✔Correct
Answer-a. Greater than the airplane weight, and the amount is a function of bank angle.
, Excessive bank angles at high altitudes can be hazardous because: ✔Correct Answer-d. All of
the above
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 descend 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.
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. ✔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. Therefor if the pilot maintains
airspeed above the appropriate speed listed for the aircraft weight, the aircraft will not stall.
✔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. Cloud 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 / autothurst.
b. Apply nose down pitch control until impeding stall indications are eliminated.
c. Adjust bank angle to wings level.
f. Apply thrust as needed.
a. Retract speed brakes and spoilers.
e. Return to the desire flight path.
The predominant number of airplane upsets are caused by: ✔Correct Answer-a.
Environmental factors.
Verified Answers |Actual Complete Update |Already
Graded A+ (Just Released)
Which of the following statements regarding energy is true? ✔Correct Answer-d. Kinetic
energy can be traded for potential energy, and potential energy can be traded for kinetic energy
The objective in maneuvering the airplane is to manage energy so that: ✔Correct Answer-d.
All of the above
What is the effect on total drag if airspeed slows below L/D Max? ✔Correct Answer-c. Drag
increases because of increased induced drag.
A jet pilot flying at L/D Max will obtain best: ✔Correct Answer-b. Endurance
When a jet aircraft is flown at the appropriate airspeed for maximum range, which type of drag
predominates? ✔Correct Answer-a. Parasite
While already at high speed, what happens if Mach is allowed to increase? ✔Correct Answer-
d. All of the above
What is the result of a shock-induced separation of airflow occurring symmetrically near the
wing root of a swept wing aircraft? ✔Correct Answer-c. A severe moment of "Mach tuck"
The speed of sound generally decreases with increasing altitude. This occurs because:
✔Correct Answer-a. The air temperature decreases.
Critical Mach number can be defined as: ✔Correct Answer-c. The speed of an aircraft in which
airflow over any part of the aircraft or structure first reaches, but doesn't exceed Mach 1.0.
Stability in the vertical axis tends to drive the sideslip angle toward zero. The most dynamic
stability about the vertical axis on modern jet transports is from: ✔Correct Answer-c. An
active stability augmentation system / yaw damper.
Swept wings cause a significant: ✔Correct Answer-b. Reduction in effectiveness of flaps.
Why is convergence of Stall AOA and Mmo hazardous? ✔Correct Answer-d. All of the above
To maintain altitude in a banked turn, the lift produced by the airplane must be: ✔Correct
Answer-a. Greater than the airplane weight, and the amount is a function of bank angle.
, Excessive bank angles at high altitudes can be hazardous because: ✔Correct Answer-d. All of
the above
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 descend 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.
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. ✔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. Therefor if the pilot maintains
airspeed above the appropriate speed listed for the aircraft weight, the aircraft will not stall.
✔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. Cloud 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 / autothurst.
b. Apply nose down pitch control until impeding stall indications are eliminated.
c. Adjust bank angle to wings level.
f. Apply thrust as needed.
a. Retract speed brakes and spoilers.
e. Return to the desire flight path.
The predominant number of airplane upsets are caused by: ✔Correct Answer-a.
Environmental factors.
