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30 Cards in this Set
- Front
- Back
The 4 forces acting on an airplane in flight are
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lift, weight, thrust, and drag
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When are the 4 forces that act on an airplane in equilibrium?
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During unaccelerated flight
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The term "angle of attack" is defined as the angle
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between the wing chord line and the relative wind
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What is the relationship of life, drag, thrust, and weight when the airplane is in straight-and-level flight?
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Lift equals weight and thrust equals drag
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One of the main functions of flaps during approach and landing is to
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increase the angle of descent without increasing airspeed
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What is one purpose of wing flaps?
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To enable the pilot to make steeper approaches to a landing without increasing the airspeed
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The angle of attack at which an airplane wing stalls will
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remain the same regardless of gross weight
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What is ground effect?
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The result of interference of the surface of the Earth with the airflow patterns about an airplane.
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Floating caused by the phenomenon of ground effect will be most realized during an approach to land when at
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less than the length of the wingspan above the surface
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What must a pilot be aware of as a result of ground effect?
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Induced drag decreases; therefore, any excess speed at the point of flare may cause considerable floating
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Ground effect is most likely to result in which problem?
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Becoming airborne before reaching recommended takeoff speed
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Which statement relates to Bernoulli's principle?
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Air traveling faster over the curved upper surface of an airfoil causes lower pressure on the top surface
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Changes in the center of pressure of a wing affect the aircraft's
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aerodynamic balance and controllability
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An airplane said to be inherently stable will
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require less effort to control
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What determines the longitudinal stability of an airplane?
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The location of the CG with respect to the center of lift
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What causes an airplane (except a T-Tail) to pitch nosedown when power is reduced and controls are not adjusted?
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The downwash on the elevators from the propeller slipstream is reduced and elevator effectiveness is reduced
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What is the purpose of the rudder on an airplane?
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To control yaw
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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 be
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difficulty in recovering from a stalled condition
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Loading an airplane to the most aft CG will cause the airplane to be
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less stable at all speeds
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In what condition must an aircraft be placed in order to spin?
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Stalled
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During a spin to the left, which wing(s) is/are stalled?
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Both wings are stalled
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In what flight condition is torque effect the greatest in a single-engine airplane?
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Low airspeed, high power, high angle of attack
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The left turning tendency of an airplane caused by P-factor is the result of the
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propeller blade descending on the the right, producing more thrust than the ascending blade on the left
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When does P-factor cause the airpland to yaw to the left?
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When at high angles of attack
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The amount of excess load that can be imposed on the wing of an airplane depends upon the
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speed of the airplane
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Which basic flight maneuver increases the load factor on an airplane as compared to straight-and-level flight?
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turns
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What force makes an airplane turn?
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The horizontal component of lift
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During an approach to a stall, an increases load factor will cause an airplane to
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stall at a higher airspeed
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The most important rule to remember in the event of a power failure after becoming airborne is to
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immediately establish the proper gliding attitude and airspeed
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What are the 4 flight fundamentals involved in maneuvering an aircraft?
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straight-and-level flight, turns, climbs, and descents
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