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ATP ctp Questions and Answers (100% Correct
Answers) Already Graded A+
Which of the following statements regarding energy is true? Ans: 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:
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Ans: All of the above (objective in maneuvering the airplane)
What is the effect on total drag if airspeed slows below L/Dmax? Ans:
Drag increases because of increased induced drag
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A jet pilot flying at L/Dmax will obtain best: Ans: Endurance
When a jet aircraft is flown at the appropriate airspeed for maximum
range, which type of drag predominates? Ans: Parasite
When already at high speed, what happens if Mach is allowed to
increase? Ans: All of the above (what happens if Mach is allowed to
increase)
What is the result of a shock-induced separation if airflow occurring
symmetrically near the wing root of a swept wing aircraft? Ans: A severe
moment or "Mach tuck"
The speed of sound generally decreases with increasing altitude. This
occurs because: Ans: The air temperature decreases
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Critical Mach number can be defined as: Ans: 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
The most dynamic stability about the vertical axis on modern jet
transports is from: Ans: An active stability augmentation system/yaw
damper
Swept wings causes a significant Ans: Reduction in effectiveness of flaps
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Why is convergence of stall AOA and Mmo hazardous? Ans: All of the
above (convergence of stall AOA hazardous)
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To maintain altitude in a banked turn, the lift produced by the airplane
must be: Ans: Greater than the airplane weight, and the amount is a
function of bank angle
Excessive bank angles at high altitudes can be hazardous because Ans:
All of the above
High altitude recovery from slow flight turning is best accomplished by:
Ans: 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 for an airplane is: Ans: The lowest of the above listed
altitudes
1
ATP ctp Questions and Answers (100% Correct
Answers) Already Graded A+
Which of the following statements regarding energy is true? Ans: 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:
© 2026 Assignment Expert
Ans: All of the above (objective in maneuvering the airplane)
What is the effect on total drag if airspeed slows below L/Dmax? Ans:
Drag increases because of increased induced drag
Guru01 - Stuvia
A jet pilot flying at L/Dmax will obtain best: Ans: Endurance
When a jet aircraft is flown at the appropriate airspeed for maximum
range, which type of drag predominates? Ans: Parasite
When already at high speed, what happens if Mach is allowed to
increase? Ans: All of the above (what happens if Mach is allowed to
increase)
What is the result of a shock-induced separation if airflow occurring
symmetrically near the wing root of a swept wing aircraft? Ans: A severe
moment or "Mach tuck"
The speed of sound generally decreases with increasing altitude. This
occurs because: Ans: The air temperature decreases
, For Expert help and assignment handling,
2
Critical Mach number can be defined as: Ans: 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
The most dynamic stability about the vertical axis on modern jet
transports is from: Ans: An active stability augmentation system/yaw
damper
Swept wings causes a significant Ans: Reduction in effectiveness of flaps
© 2026 Assignment Expert
Why is convergence of stall AOA and Mmo hazardous? Ans: All of the
above (convergence of stall AOA hazardous)
Guru01 - Stuvia
To maintain altitude in a banked turn, the lift produced by the airplane
must be: Ans: Greater than the airplane weight, and the amount is a
function of bank angle
Excessive bank angles at high altitudes can be hazardous because Ans:
All of the above
High altitude recovery from slow flight turning is best accomplished by:
Ans: 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 for an airplane is: Ans: The lowest of the above listed
altitudes
