Airport Engineering For Class ‘A’ Air port the difference of reduced levels of higher and lower edges of the conical surface, is 100 m 75 m 25 m 50 m 100 m 75 m 25 m 50 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In instrument landing system None of these Localizer and L.M.M. are installed on one side and L.O.M. on the other side L.O.M. and Localizer are installed on one side and L.M.M. on the other side L.O.M. and L.M.M. are installed on one side and Localizer antenna on the other side None of these Localizer and L.M.M. are installed on one side and L.O.M. on the other side L.O.M. and Localizer are installed on one side and L.M.M. on the other side L.O.M. and L.M.M. are installed on one side and Localizer antenna on the other side 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: Both A and R is true but 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 but 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 The best direction of a runway is along the direction of None of these Shortest line on the wind rose diagram Longest line on wind rose diagram Line clear of wind rose diagram None of these Shortest line on the wind rose diagram Longest line on wind rose diagram Line clear of wind rose diagram ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Beaufort scale is used to determine None of these Direction of winds Height of air-crafts Strength of winds None of these Direction of winds Height of air-crafts Strength of winds 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 Gross total weight of the aircraft/total available H.P of engines Load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Load of the wings ANSWER DOWNLOAD EXAMIANS APP
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