ATP CTP Course Exam Final Latest Updated 2024
The airplane angle of attack is the angle between the wing chord and the oncoming
air or relative wind. - True
Airplane stall speeds are published in the Approved Flight Manual for each airplane
model. These speeds are presented as a function of aircraft weight. Therefor if
the pilot maintains airspeed above the appropriate speed listed for the aircraft
weight, the aircraft will not stall. - False
The stall speed of an airplane: - b. Is affected by weight and bank angle.
Large downward aileron deflections: - a. Cloud induce air separation over that
portion of the wing at very high angles of attack.
Place the following steps from the stall recovery template in the correct order: -
d. Disconnect autopilot and autothrottle / autothurst.
b. Apply nose down pitch control until impeding stall indications are eliminated.
c. Adjust bank angle to wings level.
f. Apply thrust as needed.
a. Retract speed brakes and spoilers.
,e. Return to the desire flight path.
The predominant number of airplane upsets are caused by: - a. Environmental
factors.
Which of the following statements regarding energy is true? - 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: - d. All of
the above
What is the effect on total drag if airspeed slows below L/D Max? - c. Drag
increases because of increased induced drag.
A jet pilot flying at L/D Max will obtain best: - b. Endurance
When a jet aircraft is flown at the appropriate airspeed for maximum range, which
type of drag predominates? - a. Parasite
, While already at high speed, what happens if Mach is allowed to increase? - 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? - c. A severe moment
of "Mach tuck"
The speed of sound generally decreases with increasing altitude. This occurs
because: - a. The air temperature decreases.
Critical Mach number can be defined as: - 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.
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: -
c. An active stability augmentation system / yaw damper.
Swept wings cause a significant: - b. Reduction in effectiveness of flaps.
Why is convergence of Stall AOA and Mmo hazardous? - d. All of the above
The airplane angle of attack is the angle between the wing chord and the oncoming
air or relative wind. - True
Airplane stall speeds are published in the Approved Flight Manual for each airplane
model. These speeds are presented as a function of aircraft weight. Therefor if
the pilot maintains airspeed above the appropriate speed listed for the aircraft
weight, the aircraft will not stall. - False
The stall speed of an airplane: - b. Is affected by weight and bank angle.
Large downward aileron deflections: - a. Cloud induce air separation over that
portion of the wing at very high angles of attack.
Place the following steps from the stall recovery template in the correct order: -
d. Disconnect autopilot and autothrottle / autothurst.
b. Apply nose down pitch control until impeding stall indications are eliminated.
c. Adjust bank angle to wings level.
f. Apply thrust as needed.
a. Retract speed brakes and spoilers.
,e. Return to the desire flight path.
The predominant number of airplane upsets are caused by: - a. Environmental
factors.
Which of the following statements regarding energy is true? - 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: - d. All of
the above
What is the effect on total drag if airspeed slows below L/D Max? - c. Drag
increases because of increased induced drag.
A jet pilot flying at L/D Max will obtain best: - b. Endurance
When a jet aircraft is flown at the appropriate airspeed for maximum range, which
type of drag predominates? - a. Parasite
, While already at high speed, what happens if Mach is allowed to increase? - 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? - c. A severe moment
of "Mach tuck"
The speed of sound generally decreases with increasing altitude. This occurs
because: - a. The air temperature decreases.
Critical Mach number can be defined as: - 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.
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: -
c. An active stability augmentation system / yaw damper.
Swept wings cause a significant: - b. Reduction in effectiveness of flaps.
Why is convergence of Stall AOA and Mmo hazardous? - d. All of the above
