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
Airport Engineering The engine failure case for determining the basic runway length may require Only stop way Either a clearway or a stop-way or both Either a clearway or a stop-way Only clearway Only stop way Either a clearway or a stop-way or both Either a clearway or a stop-way Only clearway ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The landing and takeoff of the air craft is made against the direction of wind. In no case the centre line of the runway should make an angle with the wind direction exceeding 10° 40° 20° 30° 10° 40° 20° 30° ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The slope of the transitional surface for A, B and C type of runway shall be 0.046527777777778 0.048611111111111 0.05 0.045138888888889 0.046527777777778 0.048611111111111 0.05 0.045138888888889 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/ load of the wings Load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings Load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/total available H.P of engines ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The maximum length and pavement strength of the runway is that of G 7 B 2 A 1 B 3 G 7 B 2 A 1 B 3 ANSWER DOWNLOAD EXAMIANS APP
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