Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 22.5 m × 30 m 30 m × 30 m 22.5 m × 22.5 m 60 m × 120 m 22.5 m × 30 m 30 m × 30 m 22.5 m × 22.5 m 60 m × 120 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The fuse large includes Tail of aircraft Pilot's cabin All listed here Passengers chamber Tail of aircraft Pilot's cabin All listed here Passengers chamber ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Between the direction of wind and the longitudinal axis of the runway Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component 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 horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to ICAO, all markings on the runways are Yellow White Red Black Yellow White Red Black ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering If lift off distance of an craft is 2000 m, the clear way at the end of the runway should not be less than 152.5 m 145 m 172.5 m 162.5 m 152.5 m 145 m 172.5 m 162.5 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering To cope up high temperature of 196°C, the taxi ways and aprons are constructed with All listed here Asphaltic concrete Rubberised tar concrete Plain concrete All listed here Asphaltic concrete Rubberised tar concrete Plain concrete ANSWER DOWNLOAD EXAMIANS APP
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