Airport Engineering In instrument landing system L.O.M. and L.M.M. are installed on one side and Localizer antenna on the other side None of these L.O.M. and Localizer are installed on one side and L.M.M. on the other side Localizer and L.M.M. are installed on one side and L.O.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 L.O.M. and Localizer are installed on one side and L.M.M. on the other side Localizer and L.M.M. are installed on one side and L.O.M. on the other side ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The reduced level of the proposed site of an air port is 2500 m above M.S.L. If the recommended length by I.C.A.O. for the runway at sea level is 2500 m, the required length of the runway is 3250 m 2500 m 3000 m 3725 m 3250 m 2500 m 3000 m 3725 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Total correction for elevation, temperature and gradient for a runway should not be more than 0.15 0.25 0.35 0.2 0.15 0.25 0.35 0.2 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The best direction of a runway is along the direction of Line clear of wind rose diagram None of these Longest line on wind rose diagram Shortest line on the wind rose diagram Line clear of wind rose diagram None of these Longest line on wind rose diagram Shortest line on the wind rose diagram 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
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