Airport Engineering Castor angle is defined as the angle 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 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 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For determining the basic runway length, the landing case requires that aircraft should come to a stop within p % of the landing distance. The value of p is 0.6 0.75 0.5 0.4 0.6 0.75 0.5 0.4 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The width and interval of transverse centre line bars along the extended centre line of runway, in approach lighting system are 4.2 m and 50 m 4.2 m and 30 m 3 m and 45 m 3 m and 30 m 4.2 m and 50 m 4.2 m and 30 m 3 m and 45 m 3 m and 30 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The thickness design of the pavement, is decided on the load carried by All listed here Main gears Nose wheel Tail wheel All listed here Main gears Nose wheel Tail wheel ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The slope of the transitional surface for A, B and C type of runway shall be 0.046527777777778 0.048611111111111 0.05 0.045138888888889 0.046527777777778 0.048611111111111 0.05 0.045138888888889 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The runway length after correcting for elevation and temperature is 2845 m. If the effective gradient on runway is 0.5 percent then the revised runway length will be 2910 m 2845 m 3030 m 3130 m 2910 m 2845 m 3030 m 3130 m ANSWER DOWNLOAD EXAMIANS APP
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