Airport Engineering According to I.C.A.O. the slope of transitional surface at right angles to the centre line of runway, is kept 1 in 6 1 in 5 1 in 4 1 in 7 1 in 6 1 in 5 1 in 4 1 in 7 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The depressions and undulations in the pavement, are caused due to Improper compaction of sub-grade All listed here Punching effect Impact of heavy wheel loads Improper compaction of sub-grade All listed here Punching effect Impact of heavy wheel loads ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The bearing of the longest line of a wind rose is S 45° E, the bearing of the runway will be numbered 31 13 Both (C) and (D) 135° 31 13 Both (C) and (D) 135° ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In instrument landing system 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 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 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 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 Both A and R is true but R is not the correct explanation of A A is true but R is false ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Equal to sum of empty operating weight and the maximum pay load Less than empty operating weight Equal to empty operating weight Equal to maximum landing weight Equal to sum of empty operating weight and the maximum pay load Less than empty operating weight Equal to empty operating weight Equal to maximum landing weight ANSWER DOWNLOAD EXAMIANS APP
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