Airport Engineering Castor angle is defined as the angle Between the direction of wind and the longitudinal axis of the runway 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 true speed of the aircraft and the crosswind component Between the direction of wind and the longitudinal axis of the runway 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 true speed of the aircraft and the crosswind component ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The runway orientation is made so that landing and takeoff are Along the wind direction Against the wind direction Perpendicular to wind direction None of these Along the wind direction Against the wind direction Perpendicular to wind direction None of these ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering If lift off distance of an craft is 2000 m, the clear way at the end of the runway should not be less than 172.5 m 145 m 152.5 m 162.5 m 172.5 m 145 m 152.5 m 162.5 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The distance between main gears is 10 m, and the distance of nose gear from centre of main gears is 30 m. If the angle of turning is 60°, the distance of centre of rotation from the nearer main gear, is 9.30 m 11.30 m 12.30 m 10.30 m 9.30 m 11.30 m 12.30 m 10.30 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of runway is increased per 300 m rise above M.S.L. 0.04 0.05 0.03 0.07 0.04 0.05 0.03 0.07 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering From the end of an instrumental runway, the approach surface rises outwards 1 in 30 1 in 50 1 in 40 1 in 20 1 in 30 1 in 50 1 in 40 1 in 20 ANSWER DOWNLOAD EXAMIANS APP
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