Airport Engineering Pick up the component not applicable to aeroplanes Wings Air screw None of these Engines Wings Air screw None of these Engines ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Less than empty operating weight Equal to maximum landing weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load Less than empty operating weight Equal to maximum landing weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering To cope up high temperature of 196°C, the taxi ways and aprons are constructed with Rubberised tar concrete All listed here Asphaltic concrete Plain concrete Rubberised tar concrete All listed here Asphaltic concrete Plain concrete 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 135° Both (C) and (D) 13 31 135° Both (C) and (D) 13 31 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 30 m × 30 m 22.5 m × 30 m 22.5 m × 22.5 m 60 m × 120 m 30 m × 30 m 22.5 m × 30 m 22.5 m × 22.5 m 60 m × 120 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Runway threshold is indicated by a series of parallel lines starting from a distance of 6 m from runway end 10 m from runway end 3 m from runway end 15 m from runway end 6 m from runway end 10 m from runway end 3 m from runway end 15 m from runway end ANSWER DOWNLOAD EXAMIANS APP
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