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 Between the horizontal and the fuselage axis 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 true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, the minimum basic runway length for A and E type of airport will be 1500 m and 600 m 2100 m and 750 m 2100 m and 600 m 1500 m and 750 m 1500 m and 600 m 2100 m and 750 m 2100 m and 600 m 1500 m and 750 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The total length of a runway is 1000 m. The elevation at distance 0,200 m, 400 m, 600 m, 800 m and 1000 m are 100.0 m, 99.2 m, 101.0 m, 101.8 m, 101.4 m and 101.0 m respectively. The effective gradient of runway will be. 0.0026 0.001 0.0043 0.0065 0.0026 0.001 0.0043 0.0065 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to I.C.A.O. the slope of transitional surface at right angles to the centre line of runway, is kept 1 in 5 1 in 4 1 in 6 1 in 7 1 in 5 1 in 4 1 in 6 1 in 7 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The thickness design of the pavement, is decided on the load carried by All listed here Tail wheel Main gears Nose wheel All listed here Tail wheel Main gears Nose wheel 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° 10° 30° 40° 20° 10° 30° 40° ANSWER DOWNLOAD EXAMIANS APP
EXAMIANS