Airport Engineering As per ICAO, for airports serving big aircrafts, the crosswind component should not exceed 25 kmph 45 kmph 15 kmph 35 kmph 25 kmph 45 kmph 15 kmph 35 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The capacity of parallel runway pattern depends upon Lateral spacing between two runways and navigational aids available Weather conditions and navigational aids available Lateral spacing between two runways and weather conditions Lateral spacing between two runways, weather conditions and navigational aids available. Lateral spacing between two runways and navigational aids available Weather conditions and navigational aids available Lateral spacing between two runways and weather conditions Lateral spacing between two runways, weather conditions and navigational aids available. 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: A is false but R is true Both A and R is true and R is the correct explanation of A A is true but R is false Both A and R is true but R is not the correct explanation of A A is false but R is true Both A and R is true and R is the correct explanation of A A is true but R is false Both A and R is true but R is not the correct explanation of A ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For the proposed runway stated in if the aerodrome reference temperature is 17.2°, the net designed length of the runway is 2716 m 3016 m 2916 m 2816 m 2716 m 3016 m 2916 m 2816 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The coordinates of the ends of a runway are (5000, 5000) and (8000, 7000). The co-ordinates of another runway are (4600, 5100) and (7000, 5300). The co-ordinates of the A.R.P. are (5800, 5200) (61500, 5600) (8000, 7000) (6500, 6000) (5800, 5200) (61500, 5600) (8000, 7000) (6500, 6000) 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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