Airport Engineering The strength of winds is measured with the help of Barometers None of these Beaufort scale Wind indicator Barometers None of these Beaufort scale Wind indicator ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Less than empty operating weight Equal to maximum landing weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load Less than empty operating weight Equal to maximum landing weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of runway is increased per 300 m rise above M.S.L. 0.03 0.04 0.05 0.07 0.03 0.04 0.05 0.07 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the direction of wind and the longitudinal axis of the runway Between the horizontal and the fuselage axis 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 direction of wind and the longitudinal axis of the runway Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component 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 20° 30° 40° 10° 20° 30° 40° 10° ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Load of the wings Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ wing area ANSWER DOWNLOAD EXAMIANS APP
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