ATP CTP Course - Final Test
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1. d. Kinetic energy can be traded for potential energy, and potential
energy can be traded for kinetic energy: Which of the following
statements regarding energy is true?
2. d. All of the above: The objective in maneuvering the airplane is to
manage energy so that:
3. c. Drag increases because of increased induced drag.: What is the effect
on total drag if airspeed slows below L/D Max?
4. b. Endurance: A jet pilot flying at L/D Max will obtain best:
5. a. Parasite: When a jet aircraft is flown at the appropriate airspeed for
maximum range, which type of drag predominates?
6. d. All of the above: While already at high speed, what happens if Mach
is allowed to increase?
7. c. A severe moment of "Mach tuck": What is the result of a shock-
induced separation of airflow occurring symmetrically near the wing
root of a swept wing aircraft?
8. a. The air temperature decreases.: The speed of sound generally
decreases with increasing altitude. This occurs because:
9. 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.: Critical Mach number
can be defined as:
10.c. An active stability augmentation system / yaw damper.: 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:
11.b. Reduction in effectiveness of flaps.: Swept wings cause a significant:
12.d. All of the above: Why is convergence of Stall AOA and Mmo
hazardous?
13.a. Greater than the airplane weight, and the amount is a function of bank
angle.: To maintain altitude in a banked turn, the lift produced by the
airplane must be:
14.d. All of the above: Excessive bank angles at high altitudes can be
hazardous because:
15.c. Increasing thrust to maximum available thrust and reducing bank
angle while accelerating to airspeed above L/D Max speed. In a thrust
limited situa- tion, exiting slow flight will require an immediate descend as
an aerodynamic stall is imminent.: 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
1/
, ATP CTP Course - Final Test
Study online at
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:
2/
Study online at
1. d. Kinetic energy can be traded for potential energy, and potential
energy can be traded for kinetic energy: Which of the following
statements regarding energy is true?
2. d. All of the above: The objective in maneuvering the airplane is to
manage energy so that:
3. c. Drag increases because of increased induced drag.: What is the effect
on total drag if airspeed slows below L/D Max?
4. b. Endurance: A jet pilot flying at L/D Max will obtain best:
5. a. Parasite: When a jet aircraft is flown at the appropriate airspeed for
maximum range, which type of drag predominates?
6. d. All of the above: While already at high speed, what happens if Mach
is allowed to increase?
7. c. A severe moment of "Mach tuck": What is the result of a shock-
induced separation of airflow occurring symmetrically near the wing
root of a swept wing aircraft?
8. a. The air temperature decreases.: The speed of sound generally
decreases with increasing altitude. This occurs because:
9. 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.: Critical Mach number
can be defined as:
10.c. An active stability augmentation system / yaw damper.: 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:
11.b. Reduction in effectiveness of flaps.: Swept wings cause a significant:
12.d. All of the above: Why is convergence of Stall AOA and Mmo
hazardous?
13.a. Greater than the airplane weight, and the amount is a function of bank
angle.: To maintain altitude in a banked turn, the lift produced by the
airplane must be:
14.d. All of the above: Excessive bank angles at high altitudes can be
hazardous because:
15.c. Increasing thrust to maximum available thrust and reducing bank
angle while accelerating to airspeed above L/D Max speed. In a thrust
limited situa- tion, exiting slow flight will require an immediate descend as
an aerodynamic stall is imminent.: 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
1/
, ATP CTP Course - Final Test
Study online at
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:
2/
