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 Subsonic Mach Sonic Super-sonic Subsonic Mach Sonic 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. 0.001 0.0065 0.0026 0.0043 0.001 0.0065 0.0026 0.0043 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Beaufort scale is used to determine Height of air-crafts Direction of winds Strength of winds None of these Height of air-crafts Direction of winds Strength of winds None of these ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of clear zone for none instrument runway of a small aircraft is 150 m 600 m 300 m 750 m 150 m 600 m 300 m 750 m 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 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 From the end of an instrumental runway, the approach surface rises outwards 1 in 30 1 in 50 1 in 20 1 in 40 1 in 30 1 in 50 1 in 20 1 in 40 ANSWER DOWNLOAD EXAMIANS APP
EXAMIANS