Airport Engineering The bearing of the longest line of a wind rose is S 45° E, the bearing of the runway will be numbered 135° 31 13 Both (C) and (D) 135° 31 13 Both (C) and (D) ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Assertion A : The ratio of arriving and departing aircrafts influences the airport capacity: Reason R : Landing operation is generally given priority over the taking off operation. Select your answer based on the coding system given below: Both A and R is true and R is the correct explanation of A Both A and R is true and R is not the correct explanation of A A is true but R is false A is false but R is true Both A and R is true and R is the correct explanation of A Both A and R is true and R is not the correct explanation of A A is true but R is false A is false but R is true ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering International Civil Aviation Organization (I.C.A.O.) was set up at Montreal (Canada), in 1929 1950 1947 1939 1929 1950 1947 1939 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO recommendation, the rate of change of longitudinal gradient per 30 m length of vertical curve for A and B type of airports is limited to a maximum of 0.003 0.004 0.002 0.001 0.003 0.004 0.002 0.001 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The capacity of parallel runway pattern depends upon Lateral spacing between two runways and navigational aids available Lateral spacing between two runways, weather conditions and navigational aids available. Lateral spacing between two runways and weather conditions Weather conditions and navigational aids available Lateral spacing between two runways and navigational aids available Lateral spacing between two runways, weather conditions and navigational aids available. Lateral spacing between two runways and weather conditions Weather conditions and navigational aids available 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 Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area Load of the wings ANSWER DOWNLOAD EXAMIANS APP
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