Airport Engineering Beaufort scale is used to determine Direction of winds Strength of winds Height of air-crafts None of these Direction of winds Strength of winds Height of air-crafts None of these ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is 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 Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Load of the wings ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Pick up the component not applicable to aeroplanes None of these Wings Air screw Engines None of these Wings Air screw Engines 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 (8000, 7000) (61500, 5600) (6500, 6000) (5800, 5200) (8000, 7000) (61500, 5600) (6500, 6000) (5800, 5200) 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 2916 m 3016 m 2816 m 2716 m 2916 m 3016 m 2816 m 2716 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of runway is increased per 300 m rise above M.S.L. 0.04 0.07 0.05 0.03 0.04 0.07 0.05 0.03 ANSWER DOWNLOAD EXAMIANS APP
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