Aerodynamics, FAA Private Pilot certification 2026

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Progress: 24% (23/94)

Learning progress ?

1. What does the red line on an airspeed indicator represent?Not learned 2. When landing behind a large aircraft, the pilot should avoid wake turbulence by stayingNot learned 3. When does P-factor cause the airplane to yaw to the left?Not learned 4. Upon encountering severe turbulence, which flight condition should the pilot attempt to maintain?Not learned 5. What determines the longitudinal stability of an airplane?Not learned 6. What force makes an airplane turn?Not learned 7. (Refer to Figure 4.) What is the caution range of the airplane?Not learned 8. VNO is defined as theNot learned 9. The term "angle of attack" is defined as the angle between theNot learned 10. In what flight condition must an aircraft be placed in order to spin?Not learned 11. VSO is defined as theNot learned 12. Which basic flight maneuver increases the load factor on an airplane as compared to straight-and-level flight?Not learned 13. The angle between the chord line of an airfoil and the relative wind is known as the angle ofNot learned 14. When departing behind a heavy aircraft, the pilot should avoid wake turbulence by maneuvering the aircraftNot learned 15. What is ground effect?Not learned 16. What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level flight?Not learned 17. What must a pilot be aware of as a result of ground effect?Not learned 18. Loading an airplane to the most aft CG will cause the airplane to beNot learned 19. (Refer to Figure 4.) Which color identifies the normal flap operating range?Not learned 20. During a spin to the left, which wing(s) is/are stalled?Not learned 21. Which statement relates to Bernoulli's principle?Not learned 22. How does frost affect the lifting surfaces of an airplane on takeoff?Not learned 23. What is one purpose of wing flaps?Not learned 24. The speed at which a single flight control can be moved, one time, to its full defection without risk of damage to the aircraft isNot learned 25. As altitude increases, the indicated airspeed at which a given airplane stalls in a particular configuration willNot learned 26. The left turning tendency of an airplane caused by P-factor is the result of theNot learned 27. Ground effect is most likely to result in which problem?Not learned 28. (Refer to Figure 2.) If an airplane weighs 2,300 pounds, what approximate weight would the airplane structure be required to support during a 60° banked turn while maintaining altitude?Not learned 29. (Refer to Figure 4.) Which marking identifies the never-exceed speed?Not learned 30. Which V-speed represents best-angle-of-climb speed?Not learned 31. (Refer to Figure 4.) What is the maximum flaps-extended speed?Not learned 32. When are the four forces that act on an airplane in equilibrium?Not learned 33. (Refer to Figure 1.) The acute angle A is the angle ofNot learned 34. What is an important airspeed limitation that is not color coded on airspeed indicators?Not learned 35. The greatest vortex strength occurs when the generating aircraft isNot learned 36. After takeoff, which airspeed would the pilot use to gain the most altitude in a given period of time?Not learned 37. (Refer to Figure 4.) What is the maximum structural cruising speed?Not learned 38. Which V-speed represents maximum landing gear extended speed?Not learned 39. Which V-speed represents maximum flap extended speed?Not learned 40. The condition that requires maximum caution when avoiding wake turbulence on landing is aNot learned 41. Which would provide the greatest gain in altitude in the shortest distance during climb after takeoff?Not learned 42. (Refer to Figure 2.) If an airplane weighs 4,500 pounds, what approximate weight would the airplane structure be required to support during a 45° banked turn while maintaining altitude?Not learned 43. (Refer to Figure 4.) Which color identifies the power-off stalling speed in a specified configuration?Not learned 44. (Refer to Figure 4.) The maximum speed at which the airplane can be operated in smooth air isNot learned 45. When landing behind a large aircraft, which procedure should be followed for vortex avoidance?Not learned 46. The amount of excess load that can be imposed on the wing of an airplane depends upon theNot learned 47. An airplane said to be inherently stable willNot learned 48. When taking off or landing at an airport where heavy aircraft are operating, one should be particularly alert to the hazards of wingtip vortices because this turbulence tends toNot learned 49. What is the purpose of the rudder on an airplane?Not learned 50. An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would beNot learned 51. Why is frost considered hazardous to flight?Not learned 52. What causes an airplane (except a T-tail) to pitch nosedown when power is reduced and controls are not adjusted?Not learned 53. (Refer to Figure 4.) What is the full flap operating range for the airplane?Not learned 54. (Refer to Figure 2.) If an airplane weighs 3,300 pounds, what approximate weight would the airplane structure be required to support during a 30° banked turn while maintaining altitude?Not learned 55. Floating caused by the phenomenon of ground effect will be most realized during an approach to land when atNot learned 56. How will frost on the wings of an airplane affect takeoff performance?Not learned 57. Which V-speed represents maneuvering speed?Not learned 58. Wingtip vortices are created only when an aircraft isNot learned 59. What is the definition of load factor?Not learned 60. Changes in the center of pressure of a wing affect the aircraft'sNot learned 61. How does the wake turbulence vortex circulate around each wingtip?Not learned 62. In what flight condition is torque effect the greatest in a single-engine airplane?Not learned 63. The angle of attack at which an airplane wing stalls willNot learned 64. The angle of attack for a propeller is defined asNot learned 65. One of the main functions of flaps during approach and landing is toNot learned 66. (Refer to Figure 4.) Which color identifies the power-off stalling speed with wing flaps and landing gear in the landing configuration?Not learned 67. Wingtip vortices created by large aircraft tend toNot learned 68. During an approach to a stall, an increased load factor will cause the airplane toNot learned 69. The four forces acting on an airplane in flight areNot learned