Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/total available H.P of engines Load of the wings Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/total available H.P of engines Load of the wings Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The reduced level of the proposed site of an air port is 2500 m above M.S.L. If the recommended length by I.C.A.O. for the runway at sea level is 2500 m, the required length of the runway is 2500 m 3725 m 3250 m 3000 m 2500 m 3725 m 3250 m 3000 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Airport elevation is the reduced level above M.S.L. of Control tower Lowest point of the landing area None of these Highest point of the landing area Control tower Lowest point of the landing area None of these Highest point of the landing area ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Which of the following is an example of failure in flexible pavements? Shrinkage cracks Alligator cracking Mud pumping Warping cracks Shrinkage cracks Alligator cracking Mud pumping Warping cracks ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The distance between main gears is 10 m, and the distance of nose gear from centre of main gears is 30 m. If the angle of turning is 60°, the distance of centre of rotation from the nearer main gear, is 12.30 m 11.30 m 10.30 m 9.30 m 12.30 m 11.30 m 10.30 m 9.30 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For supersonic transport aircraft, the minimum turning radius of taxiway is 120 m 240 m 60 m 180 m 120 m 240 m 60 m 180 m ANSWER DOWNLOAD EXAMIANS APP
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