FAA Newest Exam 1 with accurate detailed answers

2



FAA Newest Exam 1 with accurate detailed answers
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[3204] The term angle of attack (AOA) is defined as the angle ______ - ✔✔between the
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wing cord line and the relative wind.
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[3204-1] The angle between the chord line of an airfoil and the relative wind is known as
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the angle of ______ - ✔✔attack
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[3317] Angle of attack is defined as the angle between between the cord line of an airfoil
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and the ________ - ✔✔direction of the relative wind
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[2225] The angle of attack at which the airfoil stalls will _______ - ✔✔remain the same
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regardless of gross weight || || ||




[2225-1] What is the effect of advancing the throttle in flight? - ✔✔airspeed will remain
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relatively constant but the aircraft will climb
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[3201-1] Which statement relates to Bernoulli's principle? - ✔✔air traveling faster over the
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curved upper surface of an airfoil causes lower pressure on the top surface.
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[3201] The four forces acting on an airplane in flight are: - ✔✔thrust, weight, drag, and lift
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[3213] What is the purpose of the rudder on an airplane? - ✔✔to control yaw
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[3205] What is the relationship of lift, drag, thrust, and weight, when an airplane is in
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straight and level flight? - ✔✔lift equals weight and thrust equals drag.
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[3202] When are the four forces that act on an airplane in equilibrium? - ✔✔during
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unaccelerated flight. ||




[2239] The best speed to use for a glide is one that will result in the greatest glide distance
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for a given amount of - ✔✔altitude
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[2229] Climb performance depends upon the ______ - ✔✔reserve power or thrust.
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[3210] An airplane said to be inherently stable will ______ - ✔✔require less effort to
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control



[3211] What determines the longitudinal stability of an airplane? - ✔✔the location of the
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CG with respect to the center of lift.
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[3212] What causes an airplane to pitch nosedown when power is reduced and controls are
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not adjusted? - ✔✔the downwash on the elevators from the propeller slipstream is reduced
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and elevator effectiveness is reduced.
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[3287] An airplane has been loaded in such a manner that the CG is located aft of the aft
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CG limit. One undesirable flight characteristic a pilot might experience with this airplane
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would be: - ✔✔difficulty in recovering from a stalled condition.
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[3288] Loading an airplane to the most aft CG will cause the airplane to be ______ -
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✔✔less stable at all speeds. || || || ||




[3211-1]Changes in the center of pressure of a wing affect the aircraft's _____ - || || || || || || || || || || || || || ||




✔✔aerodynamic balance and controllability. || || ||




[3217] The amount of excess load that can be imposed on the wing of an airplane depends
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upon the _______ - ✔✔speed of the airplane.
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[3218] Which basic flight maneuver increases the load factor on an airplane as compared to
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straight and level flight? - ✔✔turns
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[3301] What force makes an airplane turn? - ✔✔the horizontal component of lift.
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[3316] During an approach to a stall, an increased load factor will cause the airplane to
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_______ - ✔✔stall at a higher airspeed.
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[3202-1] select the ForeFlight fundamentals involved in maneuvering an aircraft -
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✔✔Straight and level flight, turns, clients, and decents.
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[3202-4] if an emergency situation requires a downwind landing, pilots should expect a
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faster _________ - ✔✔Groundspeed at touchdown, a longer ground roll, and the likelihood
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of overshooting the desired touchdown point.
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[3202-5] when executing an emergency approach to land in a single engine airplane, it is
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important to maintain a constant glide speed because variations in glides speed ________ -
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✔✔Notify all tenants at accuracy in judgment of gliding distance and landing spot
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[3263] as altitude increases, the indicated airspeed at which a given airplane stalls in a
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particular configuration will ___________ - ✔✔Remain the same regardless of altitude
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[2233] The direct cause of every stall is excessive _________ - ✔✔Angle of attack
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[3309] in what flight condition must an aircraft be placed in order to spin? - ✔✔Stalled
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[3310] during a spin to the left, which wing is stalled? - ✔✔Both wings are stalled
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