ATP-CTP QUESTIONS AND ANSWERS | LATEST
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Terms in this set (85)
Which of the following statements (D) Kinetic energy can be traded for potential
regarding energy is true? energy, and potential energy can be traded for
kinetic energy
(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
The objective in maneuvering the (D) All of the above
airplane is to manage energy so that:
(A) Kinetic energy stays between
limits (stall and placard)
(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
,What is the effect on total drag is (C) Drag increses because of increased induced
airspeed slows below L/D Max? drag
(A) Drag increases because of
increased parasite drag
(B) Drag decreases because of lower
induced drag
(C) Drag increases because of
increased induced drag
A jet pilot flying at L/D Max is obtain (B) Endurance
best:
(A) Range
(B) Endurance
(C) Ride Quality
When a jet aircraft is flown at the (A) Parasite
appropriate airspeed for maximum
range, which type of drag
predominates?
(A) Parasite
(B) Induced
(C) Each type of drag contributes
equally
,While already at high speed, what (D) All of the above
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
What is the result of a shock-induced (C) A severe moment or "Mach Tuck
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
The speed of sound generally (A) The air temperature decreases.
decreases with increasing altitude.
This occurs because:
(A) The air temperature decreases.
(B) The air pressure decreases.
(C) The composition of the air
changes.
, Critical Mach number can be defined (C) The speed of an aicraft in which airflow over
as: any part of the aircraft or structure first reaches, but
doesn't exceed, Mach 1.0.
(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.
Stability in the vertical axis tends to (C) An active stability augmentation system/yaw
drive the sideslip angle toward zero. damper
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
Swept wings cause a significant: (B) Reduction in effectiveness of flaps
(A) increase in effectiveness of flaps.
(B) Reduction in effectiveness of
flaps
(C) flap actuation reliability issue
UPDATE | INSTANT DOWNLOAD !
Save
Terms in this set (85)
Which of the following statements (D) Kinetic energy can be traded for potential
regarding energy is true? energy, and potential energy can be traded for
kinetic energy
(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
The objective in maneuvering the (D) All of the above
airplane is to manage energy so that:
(A) Kinetic energy stays between
limits (stall and placard)
(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
,What is the effect on total drag is (C) Drag increses because of increased induced
airspeed slows below L/D Max? drag
(A) Drag increases because of
increased parasite drag
(B) Drag decreases because of lower
induced drag
(C) Drag increases because of
increased induced drag
A jet pilot flying at L/D Max is obtain (B) Endurance
best:
(A) Range
(B) Endurance
(C) Ride Quality
When a jet aircraft is flown at the (A) Parasite
appropriate airspeed for maximum
range, which type of drag
predominates?
(A) Parasite
(B) Induced
(C) Each type of drag contributes
equally
,While already at high speed, what (D) All of the above
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
What is the result of a shock-induced (C) A severe moment or "Mach Tuck
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
The speed of sound generally (A) The air temperature decreases.
decreases with increasing altitude.
This occurs because:
(A) The air temperature decreases.
(B) The air pressure decreases.
(C) The composition of the air
changes.
, Critical Mach number can be defined (C) The speed of an aicraft in which airflow over
as: any part of the aircraft or structure first reaches, but
doesn't exceed, Mach 1.0.
(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.
Stability in the vertical axis tends to (C) An active stability augmentation system/yaw
drive the sideslip angle toward zero. damper
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
Swept wings cause a significant: (B) Reduction in effectiveness of flaps
(A) increase in effectiveness of flaps.
(B) Reduction in effectiveness of
flaps
(C) flap actuation reliability issue
