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 For the proposed runway stated in if the aerodrome reference temperature is 17.2°, the net designed length of the runway is 3016 m 2716 m 2916 m 2816 m 3016 m 2716 m 2916 m 2816 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The fuse large includes Pilot's cabin Tail of aircraft All listed here Passengers chamber Pilot's cabin Tail of aircraft All listed here Passengers chamber ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Beaufort scale is used to determine Strength of winds None of these Direction of winds Height of air-crafts Strength of winds None of these Direction of winds Height of air-crafts ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For determining the basic runway length, the landing case requires that aircraft should come to a stop within p % of the landing distance. The value of p is 0.4 0.75 0.6 0.5 0.4 0.75 0.6 0.5 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis ANSWER DOWNLOAD EXAMIANS APP
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