Airport Engineering Maximum gross takeoff weight of an aircraft is Equal to the empty operating weight plus the payload More than the maximum structural landing weight Equal to the maximum structural landing weight Less than the maximum structural landing weight Equal to the empty operating weight plus the payload More than the maximum structural landing weight Equal to the maximum structural landing weight Less than the maximum structural landing weight ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The engine failure case for determining the basic runway length may require Either a clearway or a stop-way Only clearway Either a clearway or a stop-way or both Only stop way Either a clearway or a stop-way Only clearway Either a clearway or a stop-way or both Only stop way ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The meteorological condition which influences the size and location of an air port is Reduced level Air density All listed here Atmosphere pressure Reduced level Air density All listed here Atmosphere pressure ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Beaufort scale is used to determine None of these Height of air-crafts Direction of winds Strength of winds None of these Height of air-crafts Direction of winds Strength of winds 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 A is false but R is true A is true but R is false Both A and R is true and R is not the correct explanation of A Both A and R is true and R is the correct explanation of A A is false but R is true A is true but R is false Both A and R is true and R is not the correct explanation of A ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Load of the wings Gross total weight of the aircraft/total available H.P of engines ANSWER DOWNLOAD EXAMIANS APP
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