Airport Engineering Castor angle is defined as the angle Between the direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the horizontal and the fuselage axis Between the direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the horizontal and the fuselage axis ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The slope of the transitional surface for A, B and C type of runway shall be 0.05 0.046527777777778 0.045138888888889 0.048611111111111 0.05 0.046527777777778 0.045138888888889 0.048611111111111 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The engine failure case for determining the basic runway length may require Only clearway Either a clearway or a stop-way or both Either a clearway or a stop-way Only stop way Only clearway Either a clearway or a stop-way or both Either a clearway or a stop-way Only stop way ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The strength of winds is measured with the help of Barometers Beaufort scale Wind indicator None of these Barometers Beaufort scale Wind indicator None of these ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The landing and takeoff of the air craft is made against the direction of wind. In no case the centre line of the runway should make an angle with the wind direction exceeding 40° 20° 10° 30° 40° 20° 10° 30° ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Airport elevation is the reduced level above M.S.L. of None of these Control tower Highest point of the landing area Lowest point of the landing area None of these Control tower Highest point of the landing area Lowest point of the landing area ANSWER DOWNLOAD EXAMIANS APP
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