Airport Engineering International Civil Aviation Organization (I.C.A.O.) was set up at Montreal (Canada), in 1929 1939 1947 1950 1929 1939 1947 1950 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 not the correct explanation of A A is true but R is false Both A and R is true and R is the correct explanation of A A is false but R is true Both A and R is true and R is not the correct explanation of A A is true but R is false Both A and R is true and R is the correct explanation of A A is false but R is true ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Assertion A : Airport capacity during IFR conditions is usually less than that during VFR conditions.Reason R: During clear weather condition (VFR), the aircrafts on final approach to runway can be spaced closer during poor visibility conditions.Select your answer based on the coding system given below: A is false but R is true Both A and R is true but R is not the correct explanation of A Both A and R is true and R is 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 but R is not the correct explanation of A Both A and R is true and R is the correct explanation of A A is true but R is false ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to ICAO, all markings on the runways are Black Yellow White Red Black Yellow White Red ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 60 m × 120 m 22.5 m × 22.5 m 22.5 m × 30 m 30 m × 30 m 60 m × 120 m 22.5 m × 22.5 m 22.5 m × 30 m 30 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is 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 Gross total weight of the aircraft/total available H.P of engines ANSWER DOWNLOAD EXAMIANS APP
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