Airport Engineering As per ICAO, for airports serving big aircrafts, the crosswind component should not exceed 15 kmph 25 kmph 35 kmph 45 kmph 15 kmph 25 kmph 35 kmph 45 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The fuse large includes Passengers chamber Pilot's cabin Tail of aircraft All listed here Passengers chamber Pilot's cabin Tail of aircraft All listed here ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The cruising speed of the aircraft is 500 kmph. If there is a head wind of 50 kmph, then the air speed and ground speed of the aircraft respectively will be 500 kmph and 500 kmph 500 kmph and 450 kmph 450 kmph and 450 kmph 450 kmph and 500 kmph 500 kmph and 500 kmph 500 kmph and 450 kmph 450 kmph and 450 kmph 450 kmph and 500 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Beaufort scale is used to determine Direction of winds Height of air-crafts Strength of winds None of these Direction of winds Height of air-crafts Strength of winds None of these ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In Instrumental landing system, the middle markers are located Along the extended centre line of runway end About 7 km. ahead of the runway threshold At the runway threshold About 1 km. ahead of the runway threshold Along the extended centre line of runway end About 7 km. ahead of the runway threshold At the runway threshold About 1 km. ahead of the runway threshold ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The main disadvantage of angle nose out parking configuration of aircraft is that the Hot blast is directed towards the terminal building Overall apron area required is more Aircraft rear loading door is far away from terminal building All listed here Hot blast is directed towards the terminal building Overall apron area required is more Aircraft rear loading door is far away from terminal building All listed here ANSWER DOWNLOAD EXAMIANS APP
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