Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Load of the wings ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of clear zone for none instrument runway of a small aircraft is 750 m 300 m 600 m 150 m 750 m 300 m 600 m 150 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For supersonic transport aircraft, the minimum turning radius of taxiway is 180 m 60 m 240 m 120 m 180 m 60 m 240 m 120 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The slope of the transitional surface for A, B and C type of runway shall be 0.05 0.048611111111111 0.045138888888889 0.046527777777778 0.05 0.048611111111111 0.045138888888889 0.046527777777778 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 Last Seven English alphabets First Seven English alphabets First seven natural numbers Seven English alphabets Last Seven English alphabets First Seven English alphabets First seven natural numbers Seven English alphabets ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering If lift off distance of an craft is 2000 m, the clear way at the end of the runway should not be less than 152.5 m 162.5 m 172.5 m 145 m 152.5 m 162.5 m 172.5 m 145 m ANSWER DOWNLOAD EXAMIANS APP
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