Airport Engineering An aircraft is flying in an atmosphere of 30°C with a speed of 1260 kmph. Its speed is known as Super-sonic Sonic Mach Subsonic Super-sonic Sonic Mach Subsonic ANSWER DOWNLOAD EXAMIANS APP
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 true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis 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 true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The minimum width of clearway is 100 m 250 m 150 m 50 m 100 m 250 m 150 m 50 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The slope of the transitional surface for A, B and C type of runway shall be 0.045138888888889 0.05 0.048611111111111 0.046527777777778 0.045138888888889 0.05 0.048611111111111 0.046527777777778 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering From the end of an instrumental runway, the approach surface rises outwards 1 in 40 1 in 20 1 in 30 1 in 50 1 in 40 1 in 20 1 in 30 1 in 50 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 2845 m 3130 m 2910 m 3030 m 2845 m 3130 m 2910 m 3030 m ANSWER DOWNLOAD EXAMIANS APP
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