ATP CTP FINAL EXAM NEWEST 2024 ACTUAL EXAM COMPLETE 250 QUESTIONS AND CORRECT DETAILED ANSWERS (VERIFIED ANSWERS) ALREADY GRADED A+
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Course
ATP CTP
Institution
ATP CTP
ATP CTP FINAL EXAM NEWEST 2024 ACTUAL EXAM COMPLETE 250
QUESTIONS AND CORRECT DETAILED ANSWERS (VERIFIED ANSWERS)
ALREADY GRADED A+
ATP CTP FINAL EXAM NEWEST 2024 ACTUAL EXAM COMPLETE 250
QUESTIONS AND CORRECT DETAILED ANSWERS (VERIFIED ANSWERS)
ALREADY GRADED A+ ATP CTP FINAL EXAM NEWEST...
ATP CTP FINAL EXAM NEWEST 2024 ACTUAL EXAM COMPLETE 250
QUESTIONS AND CORRECT DETAILED ANSWERS (VERIFIED ANSWERS)
ALREADY GRADED A+
Which of the following statements regarding energy is true?
(A) Kinetic energy decreases with increasing airspeed.
(B) Potential energy is approximately proportional to
airspeed.
(C) Chemical energy remains constant throughout a flight
(D) Kinetic energy can be traded for potential energy, and
potential energy can be traded for kinetic energy - 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:
(A) Kinetic energy stays between limits (stall and placard)
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(B) Potential energy sstays between limits (terrain and
buffet altitude)
(C) Chemical energy stays above certain thresholds (not
running out of fuel)
(D) All of the above - CORRECT ANSWER >>>>(D) All of the
above
What is the effect on total drag is airspeed slows below L/D
Max?
(A) Drag increases because of increased parasite drag
(B) Drag decreases because of lower induced drag
(C) Drag increases because of increased induced drag -
CORRECT ANSWER >>>>(C) Drag increses because of
increased induced drag
When a jet aircraft is flown at the appropriate airspeed for
maximum range, which type of drag predominates?
(A) Parasite
(B) Induced
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(C) Each type of drag contributes equally - CORRECT
ANSWER >>>>(A) Parasite
While already at high speed, what happens if Mach is
allowed to increase?
(A) Airflow over parts of the airplane begin to exceed the
speed of sound
(B) Shock waves can cause local airflow separation
(C) Characteristics such as pitch-up, pitch-down, or buffeting
may occur.
(D) All of the above - 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?
(A) A high-speed stall and sudden pitch-up
(B) Severe porpoising.
(C) A severe moment or "Mach Tuck - CORRECT ANSWER
>>>>(C) A severe moment or "Mach Tuck
The speed of sound generally decreases with increasing
altitude. This occurs because:
(A) The air temperature decreases.
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(B) The air pressure decreases.
(C) The composition of the air changes. - CORRECT ANSWER
>>>>(A) The air temperature decreases.
Critical Mach number can be defined as:
(A) The speed at which the aircraft is traveling faster than
sound.
(B) The maximum Mach number at which an aircraft may be
safely operated.
(C) The speed of an aicraft in which airflow over any part of
the aircraft or structure first reaches, but doesn't exceed,
Mach 1.0. - CORRECT ANSWER >>>>(C) The speed of an
aicraft 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:
(A) The vertical fin
(B) The rudder
(C) An active stability augmentation system/yaw damper
(D) Pilot roll input - CORRECT ANSWER >>>>(C) An active
stability augmentation system/yaw damper
Swept wings cause a significant:
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