Airport Engineering The thickness design of the pavement, is decided on the load carried by All listed here Nose wheel Tail wheel Main gears All listed here Nose wheel Tail wheel Main gears ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle 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 Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component 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 3030 m 2910 m 2845 m 3130 m 3030 m 2910 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, for airports serving big aircrafts, the crosswind component should not exceed 25 kmph 15 kmph 35 kmph 45 kmph 25 kmph 15 kmph 35 kmph 45 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to I.C.A.O. the recommended length of air ports is decided on All listed here Sea level elevation Effective gradient percentage Standard sea level temperature (15°C) All listed here Sea level elevation Effective gradient percentage Standard sea level temperature (15°C) ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The bearing of the longest line of a wind rose is S 45° E, the bearing of the runway will be numbered 31 13 Both (C) and (D) 135° 31 13 Both (C) and (D) 135° ANSWER DOWNLOAD EXAMIANS APP
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