Airport Engineering The length of clear zone for none instrument runway of a small aircraft is 750 m 150 m 600 m 300 m 750 m 150 m 600 m 300 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Effective length of a runway is the distance between Ends of the runway Ends of the clear way on either side Point of intersection of the glide path and the extended plane of the runway surface and the other end of the runway Point of intersection of the obstruction clearance line and the extended plane of the runway surface, and the other end of the runway Ends of the runway Ends of the clear way on either side Point of intersection of the glide path and the extended plane of the runway surface and the other end of the runway Point of intersection of the obstruction clearance line and the extended plane of the runway surface, and the other end of the runway ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Speed of Sound varies 2.4 kmph per degree centigrade rise in temperature All listed here Sound at 0°C is called one Mach Sound at 0°C is 1190 kmph Sound varies 2.4 kmph per degree centigrade rise in temperature All listed here Sound at 0°C is called one Mach Sound at 0°C is 1190 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For supersonic transport aircraft, the minimum turning radius of taxiway is 240 m 120 m 180 m 60 m 240 m 120 m 180 m 60 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Calm period is the percentage of time during which wind intensity is less than 6.4 kmph 9.6 kmph 8.0 kmph 4.8 kmph 6.4 kmph 9.6 kmph 8.0 kmph 4.8 kmph 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 horizontal and the fuselage axis 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 direction of wind and the longitudinal axis of the runway 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 true speed of the aircraft and the crosswind component ANSWER DOWNLOAD EXAMIANS APP
EXAMIANS