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Use the following URL to download acompletelist of associated supplement books:[http://www.faa.gov/education_research/testing/airmen/](http://www.faa.gov/education_research/testing/airmen/)[ ](http://www.faa.gov/education_research/testing/airmen/)[test_questions/media/supplements.pdf](test_questions/media/supplements.pdf)  \n1. PLT309 PVT  \nWhich basic flight maneuver increases the load factor on an airplane as compared to straight-andlevel flight?  \nA) Climbs.  \nB) Turns.  \nC) Stalls.  \n2. PLT309 PVT  \n(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?  \nA) 2,300 pounds.  \nB) 3,400 pounds.  \nC) 4,600 pounds.  \n3. PLT168 PVT The term 'angle of attack' is defined as the angle  \nA) between the wing chord line and the relative wind.  \nB) between the airplane's climb angle and the horizon.  \nC) formed by the longitudinal axis of the airplane and the chord line of the wing.  \n4. PLT242 PVT The four forces acting on an airplane in flight are  \nA) lift, weight, thrust, and drag.  \nB) lift, weight, gravity, and thrust.  \nC) lift, gravity, power, and friction.  \n5. PLT134 PVT How will frost on the wings of an airplane affect takeoff performance?  \nA) Frost will disrupt the smooth flow of air over the wing, adversely affecting its lifting capability.  \nB) Frost will change the camber of the wing, increasing its lifting capability.  \nC) Frost will cause the airplane to become airborne with a higher angle of attack, decreasing the stall speed.  \n6. PLT242 PVT What force makes an airplane turn?  \nA) The horizontal component of lift.  \nB) The vertical component of lift.  \nC) Centrifugal force.  \n7. PLT243 PVT  \nIn what flight condition is torque effect the greatest in a single-engine airplane?  \nA) Low airspeed, high power, high angle of attack.  \nB) Low airspeed, low power, low angle of attack.  \nC) High airspeed, high power, high angle of attack.  \n8. PLT243 PVT  \nThe left turning tendency of an airplane caused by P-factor is the result of the A) clockwise rotation of the engine and the propeller turning the airplane counter-clockwise.  \nB) propeller blade descending on the right, producing more thrust than the ascending blade on the left.  \nC) gyroscopic forces applied to the rotating propeller blades acting 90° in advance of the point the force was applied.  \n9. PLT351 PVT  \nWhat causes an airplane (except a T-tail) to pitch nosedown when power is reduced and controls are not adjusted?  \nA) The CG shifts forward when thrust and drag are reduced.  \nB) The downwash on the elevators from the propeller slipstream is reduced and elevator effectiveness is reduced.  \nC) When thrust is reduced to less than weight, lift is also reduced and the wings can no longer support the weight.  \n10. PLT213 PVT What determines the longitudinal stability of an airplane?  \nA) The location of the CG with respect to the center of lift.  \nB) The effectiveness of the horizontal stabilizer, rudder, and rudder trim tab.  \nC) The relationship of thrust and lift to weight and drag.  \n11. PLT213 PVTAn airplane said to be inherently stable will  \nA) be difficult to stall.  \nB) require less effort to control.  \nC) not spin.  \n12. PLT245 PVTIn what flight condition must an aircraft be placed in order to spin?  \nA) Partially stalled with one wing low.  \nB) In a steep diving spiral.  \nC) Stalled.  \n13. PLT477 PVT  \nAs altitude increases, the indicated airspeed at which a given airplane stalls in a particular configuration will  \nA) decrease as the true airspeed decreases.  \nB) decrease as the true airspeed in","cbCaijlEXHiYhtt6","https://ap.wps.com/l/cbCaijlEXHiYhtt6","pdf",176809,103,"English","# Question Bank Overview\n## Flight Maneuvers, Forces, and Angle of Attack\n## Frost, Turning, and Torque Effects\n## Stability, Spin, and Stalls\n## ATC Advisory and Performance Calculations","[{\"question\":\"What publication support does the FAA testing system rely on for test items?\",\"answer\":\"A series of supplement publications provides the graphics, legends, and maps needed to respond to certain test items.\"},{\"question\":\"How is the “angle of attack” defined in these questions?\",\"answer\":\"It is defined as the angle between the wing chord line and the relative wind.\"},{\"question\":\"What determines whether an airplane can be placed in a spin?\",\"answer\":\"An aircraft must be placed in the appropriate flight condition described in the questions; for example, one option states the aircraft must be stalled.\"}]","Airman Knowledge Test Question Bank - Private Pilot | PDF",1790766546,260]