Airport Engineering For Class ‘A’ Air port the difference of reduced levels of higher and lower edges of the conical surface, is 50 m 25 m 75 m 100 m 50 m 25 m 75 m 100 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In Instrumental landing system, the middle markers are located At the runway threshold About 7 km. ahead of the runway threshold Along the extended centre line of runway end About 1 km. ahead of the runway threshold At the runway threshold About 7 km. ahead of the runway threshold Along the extended centre line of runway end About 1 km. ahead of the runway threshold ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is 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 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 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, for airports serving big aircrafts, the crosswind component should not exceed 15 kmph 25 kmph 35 kmph 45 kmph 15 kmph 25 kmph 35 kmph 45 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Beaufort scale is used to determine Strength of winds Height of air-crafts Direction of winds None of these Strength of winds Height of air-crafts Direction of winds None of these ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For the proposed air port, the survey project provides Topographic plan All listed here Master plan Grading plan Topographic plan All listed here Master plan Grading plan ANSWER DOWNLOAD EXAMIANS APP
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