Airport Engineering Maximum gross takeoff weight of an aircraft is Less than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload More than the maximum structural landing weight Less than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload More than the maximum structural landing weight ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/total available H.P of engines 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 Both (C) and (D) 13 31 135° Both (C) and (D) 13 31 135° ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The lift off distance is the distance along the centre of the runway between the starting point and Point where air craft attains a height of 10.7 m Point where air craft becomes air borne End of the runway End of stop-way Point where air craft attains a height of 10.7 m Point where air craft becomes air borne End of the runway End of stop-way ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In an airport, if 4 groups of 5 gates each located well separated are considered for traffic and the future to present traffic ratio is 3, then the total requirement of future gates will be 44 68 36 32 44 68 36 32 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Pick up the component not applicable to aeroplanes None of these Air screw Engines Wings None of these Air screw Engines Wings ANSWER DOWNLOAD EXAMIANS APP
EXAMIANS