ATP CTP Course - Final Test Verified 100% Correct!!

ATP CTP Course - Final Test Questions and Answers 2022. Which of the following statements regarding energy is true? The objective in maneuvering the airplane is to manage energy so that: What is the effect on total drag if airspeed slows below L/D Max? A jet pilot flying at L/D Max will obtain best: When a jet aircraft is flown at the appropriate airspeed for maximum range, which type of drag predominates? While already at high speed, what happens if Mach is allowed to increase? What is the result of a shock-induced separation of airflow occurring symmetrically near the wing root of a swept wing aircraft? The speed of sound generally decreases with increasing altitude. This occurs because: Critical Mach number can be defined as: 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: Swept wings cause a significant: Why is convergence of Stall AOA and Mmo hazardous? To maintain altitude in a banked turn, the lift produced by the airplane must be: Excessive bank angles at high altitudes can be hazardous because: 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 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: Maximum Altitude is the highest altitude at which an airplane can be operated. Maximum Altitude for an airplane is: Exceed the critical angle of attack and the surface will stall, and lift will decrease instead of increasing. This is true: Which of the following statements is true? The airplane angle of attack is the angle between the wing chord and the oncoming air or relative wind. 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. The stall speed of an airplane: Large downward aileron deflections: Place the following steps from the stall recovery template in the correct order: The predominant number of airplane upsets are caused by: Most of the multi-engine turbojet