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ATP CTP FINAL EXAM NEWEST 2024 LATEST UPDATED COMPLETE 250 QUESTIONS WITH VERIFIED CORRECT DETAILED AND CORRECT ANSWERS ACTUAL BRAND-NEW EXAM GRADED A+$14.49
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ATP CTP FINAL EXAM NEWEST 2024 LATEST UPDATED COMPLETE 250 QUESTIONS WITH VERIFIED CORRECT DETAILED AND CORRECT ANSWERS ACTUAL BRAND-NEW EXAM GRADED A+
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Course
ATP CTP
Institution
ATP CTP
ATP CTP FINAL EXAM NEWEST 2024
LATEST UPDATED COMPLETE 250
QUESTIONS WITH VERIFIED
CORRECT DETAILED AND
CORRECT ANSWERS ACTUAL
BRAND-NEW EXAM GRADED A+
ATP CTP FINAL EXAM NEWEST 2024
LATEST UPDATED COMPLETE 250
QUESTIONS WITH VERIFIED
CORRECT DETAILED AND
CORRECT ANSWERS ACTUAL
BRAND-NEW EXAM GRADED A+
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 -
....ANSWER...(C) Drag increses because of increased
induced drag
A jet pilot flying at L/D Max is obtain best:
(A) Range
(B) Endurance
(C) Ride Quality - ....ANSWER...(B) Endurance
1
,When a jet aircraft is flown at the appropriate airspeed for
maximum range, which type of drag predominates?
(A) Parasite
(B) Induced
(C) Each type of drag contributes equally -
....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 - ....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 - ....ANSWER...(C)
A severe moment or "Mach Tuck
2
,The speed of sound generally decreases with increasing
altitude. This occurs because:
(A) The air temperature decreases.
(B) The air pressure decreases.
(C) The composition of the air changes. -
....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. - ....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:
3
, 4|Page
(A) The vertical fin
(B) The rudder
(C) An active stability augmentation system/yaw damper
(D) Pilot roll input - ....ANSWER...(C) An active stability
augmentation system/yaw damper
Swept wings cause a significant:
(A) increase in effectiveness of flaps.
(B) Reduction in effectiveness of flaps
(C) flap actuation reliability issue - ....ANSWER...(B)
Reduction in effectiveness of flaps
Why is convergence of Stall AOA and MMO hazardous?
(A) Any decrease in airspeed will cause the aircraft to
buffet and potentially stall
(B) Any increase in airspeed will cause the aircraft to
buffet and potentially cause Mach Tuck
(C) Airspeed changes may occur due to environmental
factors, without pilot input.
(D) All of the above - ....ANSWER...(D) All of the above
4
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