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ATP CTP Course - Final Test Questions and answers 2024/25
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ATP CTP Course - Final Test Questions and answers 2024/25
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ATP CTP Course - Final Test Questionsand answers 2024/25
Which of the following statements regarding energy is true? - d. Kinetic energy can be
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traded for potential energy, and potential energy can be traded for kinetic energy
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The objective in maneuvering the airplane is to manage energy so that: - d. All of the
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above
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What is the effect on total drag if airspeed slows below L/D Max? - c. Drag increases
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because of increased induced drag.
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II A jet pilot flying at L/D Max will obtain best: - b. Endurance
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When a jet aircraft is flown at the appropriate airspeed for maximum range, which type of
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drag predominates? - a. Parasite
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While already at high speed, what happens if Mach is allowed to increase? - d. All of the
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above
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What is the result of a shock-induced separation of airflow occurring symmetrically near
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the wing root of a swept wing aircraft? - c. A severe moment of "Mach tuck"
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The speed of sound generally decreases with increasing altitude. This occurs because: -
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a. The air temperature decreases.
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Critical Mach number can be defined as: - c. The speed of an aircraft in which airflow over
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any part of the aircraft or structure first reaches, but doesn't exceed Mach 1.0.
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Stability in the vertical axis tends to drive the sideslip angle toward zero. The most
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dynamic stability about the vertical axis on modern jet transports is from: - c. An active
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stability augmentation system / yaw damper.
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II Swept wings cause a significant: - b. Reduction in effectiveness of flaps.
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II Why is convergence of Stall AOA and Mmo hazardous? - d. All of the above
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To maintain altitude in a banked turn, the lift produced by the airplane must be: - a.
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Greater than the airplane weight, and the amount is a function of bank angle.
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II Excessive bank angles at high altitudes can be hazardous because: - d. All of the above
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When operating at constant speed with constant thrust setting at high altitude (typically
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above FL250) in slow flight below L/D Max airspeed, any disturbance causing a decrease
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, in airspeed will result in a further decrease in airspeed unless thrust in increased. High
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altitude recovery from slow flight while turning is best accomplished by: - c. Increasing
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thrust to maximum available thrust and reducing bank angle while accelerating to
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airspeed above L/D Max speed. In a thrust limited situation, exiting slow flight will require
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an immediate descend as an aerodynamic stall is imminent.
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Maximum Altitude is the highest altitude at which an airplane can be operated. Maximum
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Altitude for an airplane is: - e. The lowest of the above listed altitudes.
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Exceed the critical angle of attack and the surface will stall, and lift will decrease instead
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of increasing. This is true: - d. Regardless of airplane speed or attitude.
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Which of the following statements is true? - d. Recovery from approach to stall warning is
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the same as recovery from a stall.
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The airplane angle of attack is the angle between the wing chord and the oncoming air or
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relative wind. - True
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Airplane stall speeds are published in the Approved Flight Manual for each airplane
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model. These speeds are presented as a function of aircraft weight. Therefor if the pilot
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maintains airspeed above the appropriate speed listed for the aircraft weight, the aircraft
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will not stall. - False
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II The stall speed of an airplane: - b. Is affected by weight and bank angle.
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Large downward aileron deflections: - a. Cloud induce air separation over that portion of
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the wing at very high angles of attack.
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Place the following steps from the stall recovery template in the correct order: - d.
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Disconnect autopilot and autothrottle / autothurst.
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b. Apply nose down pitch control until impeding stall indications are eliminated.
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c. Adjust bank angle to wings level.
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f. Apply thrust as needed.
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a. Retract speed brakes and spoilers.
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e. Return to the desire flight path.
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II The predominant number of airplane upsets are caused by: - a. Environmental factors.
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Most of the multi-engine turbojet loss-of-control incidents that are caused by
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environmental factors because of: - d. Wake turbulence
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When initiating recommended airplane upset recovery techniques, the first two
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techniques are: - c. Recognize and confirm the situation and disengage the autopilot and
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auto-throtles.
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