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 500 kmph 450 kmph and 450 kmph 500 kmph and 500 kmph 500 kmph and 450 kmph 450 kmph and 500 kmph 450 kmph and 450 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of runway is increased per 300 m rise above M.S.L. 0.07 0.03 0.04 0.05 0.07 0.03 0.04 0.05 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 30 m 4.2 m and 30 m 3 m and 45 m 4.2 m and 50 m 3 m and 30 m 4.2 m and 30 m 3 m and 45 m 4.2 m and 50 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 60 m × 120 m 22.5 m × 22.5 m 22.5 m × 30 m 30 m × 30 m 60 m × 120 m 22.5 m × 22.5 m 22.5 m × 30 m 30 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to the International Civil Aviation Organization (I.C.A.O.), the runway lengths of aerodromes, have been coded by First seven natural numbers Last Seven English alphabets Seven English alphabets First Seven English alphabets First seven natural numbers Last Seven English alphabets Seven English alphabets First Seven English alphabets ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload ANSWER DOWNLOAD EXAMIANS APP
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