Airport Engineering For Class ‘A’ Air port the difference of reduced levels of higher and lower edges of the conical surface, is 25 m 50 m 75 m 100 m 25 m 50 m 75 m 100 m ANSWER DOWNLOAD EXAMIANS APP
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 runway orientation is made so that landing and takeoff are None of these Against the wind direction Perpendicular to wind direction Along the wind direction None of these Against the wind direction Perpendicular to wind direction Along the wind direction 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 First seven numbers Last Seven English alphabets Seven English alphabets First Seven English alphabets First seven numbers Last Seven English alphabets Seven English alphabets First Seven English alphabets ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The main disadvantage of angle nose out parking configuration of aircraft is that the Hot blast is directed towards the terminal building Overall apron area required is more Aircraft rear loading door is far away from terminal building All listed here Hot blast is directed towards the terminal building Overall apron area required is more Aircraft rear loading door is far away from terminal building All listed here ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For determining the basic runway length, the landing case requires that aircraft should come to a stop within p % of the landing distance. The value of p is 0.4 0.6 0.75 0.5 0.4 0.6 0.75 0.5 ANSWER DOWNLOAD EXAMIANS APP
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