Airport Engineering Pick up the component not applicable to aeroplanes None of these Wings Engines Air screw None of these Wings Engines Air screw 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 Zero fuel weight of an aircraft is: Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load Equal to maximum landing weight Less than empty operating weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load Equal to maximum landing weight Less than empty operating weight ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to ICAO, all markings on the runways are White Black Red Yellow White Black Red Yellow ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The depressions and undulations in the pavement, are caused due to Punching effect Impact of heavy wheel loads Improper compaction of sub-grade All listed here Punching effect Impact of heavy wheel loads Improper compaction of sub-grade All listed here ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 60 m × 120 m 30 m × 30 m 22.5 m × 22.5 m 22.5 m × 30 m 60 m × 120 m 30 m × 30 m 22.5 m × 22.5 m 22.5 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
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