Airport Engineering An aircraft is flying in an atmosphere of 30°C with a speed of 1260 kmph. Its speed is known as Sonic Super-sonic Subsonic Mach Sonic Super-sonic Subsonic Mach ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For Class ‘A’ Air port the difference of reduced levels of higher and lower edges of the conical surface, is 25 m 100 m 75 m 50 m 25 m 100 m 75 m 50 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The height of the pilot's eye above the runway surface is assumed 1 m 5 m 4 m 3 m 1 m 5 m 4 m 3 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per UK design criteria, if LCN of aircraft is between 1.25 to 1.5 times the LCN of pavement, then the number of movements allowed are Zero 300 Unrestricted 3000 Zero 300 Unrestricted 3000 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings Load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings Load of the wings Gross total weight of the aircraft/ wing area ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 30 m × 30 m 22.5 m × 22.5 m 60 m × 120 m 22.5 m × 30 m 30 m × 30 m 22.5 m × 22.5 m 60 m × 120 m 22.5 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
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