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PRIVATE PILOT TEST GUIDE (CHAPTER 3) QUESTIONS WITH EXPLANATIONS OF ANSWERS.
Typology: Exams
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line of the wing and the relative wind." "(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 degree banked turn while maintaining
Less stable at ALL speeds."
airborne before reaching recommended takeoff speed."
over the curved upper surface of an airfoil causes lower pressure on the top surface."
Aerodynamic balance and controllability."
control."
Drag."
blade on the left."
location of the Center of Gravity (CG) with respect to the center of lift."
During unaccelerated flight."
angles of attack." "What causes an airplane (except a T-tail) to pitch nose down when power is reduced and
propeller slipstream is reduced and elevator effectiveness is reduced."
"(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 degree banked turn while maintaining
"An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One
"What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-
Stalled." "(Refer to Figure 2.) If an airplane weights 4,500 pounds, what approximate weight would the airplane structure be required to support during a 45 degree banked turn while maintaining
stalled."