Canadian CPL Test Questions and Answers 100% Solved
Canadian CPL Test Questions and Answers 100% Solved Load factor from angle of bank formula load factor = 1/cos(angle of bank) Normal category load factor limits +3.8g -1.52g Utility category load factor limits +4.4g -1.76g Aerobatic category load factor limits +6g -5g Definition of aircraft Machine capable of deriving support in the atmosphere from the reactions of the air Definition of aeroplane Power-driven heavier-than-air aircraft, deriving its lift in flight from aerodynamic reactions on surfaces that remain fixed under given conditions of flight Definition of airframe The aeroplane structure, excluding instruments and engine Aircraft classes - balloo
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