A Good Pilot is Always Learning

Private Pilot Written Test Questions 2011 Bank

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Airman Knowledge Test Question Bank file:///T|/AFSMigration/training_testing/testing/airmen/test_questions/media/PVT.htm[2/14/2011 3:36:30 PM] 01/31/2011 Bank: (Private Pilot) Airman Knowledge Test Question Bank The FAA computer-assisted testing system is supported by a series of supplement publications. These publications, available through several aviation publishers, include the graphics, legends, and maps that are needed to successfully respond to certain test items. Use the following URL to download a complete list of associated supplement books: http://www.faa.gov/training_testing/testing/airmen/test_questions/ The Learning Statement Reference Guide for Airman Knowledge Testing contains listings of learning statements with their associated codes. It can be located at: http://www.faa.gov/training_testing/testing/airmen/media/LearningStatementReferenceGuide.pdf 1. PLT309 PVT (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? A) 2,300 pounds. B) 3,400 pounds. C) 4,600 pounds. 2. PLT134 PVT How will frost on the wings of an airplane affect takeoff performance? A) Frost will disrupt the smooth flow of air over the wing, adversely affecting its lifting capability. B) Frost will change the camber of the wing, increasing its lifting capability. C) Frost will cause the airplane to become airborne with a higher angle of attack, decreasing the stall speed. 3. PLT242 PVT What force makes an airplane turn? A) The horizontal component of lift. B) The vertical component of lift. C) Centrifugal force. 4. PLT243 PVT In what flight condition is torque effect the greatest in a single-engine airplane? A) Low airspeed, high power, high angle of attack. B) Low airspeed, low power, low angle of attack. C) High airspeed, high power, high angle of attack. 5. PLT213 PVT What determines the longitudinal stability of an airplane? A) The location of the CG with respect to the center of lift. B) The effectiveness of the horizontal stabilizer, rudder, and rudder trim tab. C) The relationship of thrust and lift to weight and drag. 6. PLT245 PVT In what flight condition must an aircraft be placed in order to spin? A) Partially stalled with one wing low. B) In a steep diving spiral. C) Stalled.

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