Airport Engineering The maximum value of the angle of turning of the nose gear large jet aircrafts, is limited to 20° 45° 60° 30° 20° 45° 60° 30° ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The slope of the obstruction clearance line from the boundary of the heliport should be 0.047222222222222 0.045138888888889 0.069444444444444 0.043055555555556 0.047222222222222 0.045138888888889 0.069444444444444 0.043055555555556 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The fuse large includes Pilot's cabin All listed here Tail of aircraft Passengers chamber Pilot's cabin All listed here Tail of aircraft Passengers chamber 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 true speed of the aircraft and the crosswind component Between the direction of wind and the longitudinal axis of the runway 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 true speed of the aircraft and the crosswind component Between the direction of wind and the longitudinal axis of the runway Between the horizontal and the fuselage axis ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For Class ‘A’ Air port the difference of reduced levels of higher and lower edges of the conical surface, is 25 m 100 m 75 m 50 m 25 m 100 m 75 m 50 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 22.5 m × 22.5 m 60 m × 120 m 30 m × 30 m 22.5 m × 30 m 22.5 m × 22.5 m 60 m × 120 m 30 m × 30 m 22.5 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
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