Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 22.5 m × 30 m 60 m × 120 m 30 m × 30 m 22.5 m × 22.5 m 22.5 m × 30 m 60 m × 120 m 30 m × 30 m 22.5 m × 22.5 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The width and interval of transverse centre line bars along the extended centre line of runway, in approach lighting system are 3 m and 45 m 3 m and 30 m 4.2 m and 50 m 4.2 m and 30 m 3 m and 45 m 3 m and 30 m 4.2 m and 50 m 4.2 m and 30 m 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 450 kmph 450 kmph and 450 kmph 500 kmph and 500 kmph 450 kmph and 500 kmph 500 kmph and 450 kmph 450 kmph and 450 kmph 500 kmph and 500 kmph 450 kmph and 500 kmph ANSWER DOWNLOAD EXAMIANS APP
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 According to the International Civil Aviation Organization (I.C.A.O.) the strength of runway pavements, have been coded by Seven English alphabets First Seven English alphabets Last Seven English alphabets First seven numbers Seven English alphabets First Seven English alphabets Last Seven English alphabets First seven numbers ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Equal to empty operating weight Less than empty operating weight Equal to maximum landing weight Equal to sum of empty operating weight and the maximum pay load Equal to empty operating weight Less than empty operating weight Equal to maximum landing weight Equal to sum of empty operating weight and the maximum pay load ANSWER DOWNLOAD EXAMIANS APP
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