Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 22.5 m × 30 m 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 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The runway length after correcting for elevation and temperature is 2845 m. If the effective gradient on runway is 0.5 percent then the revised runway length will be 2910 m 2845 m 3030 m 3130 m 2910 m 2845 m 3030 m 3130 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Geometric design of holding apron of these statements 2 and 3 are correct 1 and 3 are correct 1 and 2 are correct 1 alone is correct 2 and 3 are correct 1 and 3 are correct 1 and 2 are correct 1 alone is correct ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Equal to maximum landing weight Equal to sum of empty operating weight and the maximum pay load Less than empty operating weight Equal to empty operating weight Equal to maximum landing weight Equal to sum of empty operating weight and the maximum pay load Less than empty operating weight Equal to empty operating weight ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering An aircraft is flying in an atmosphere of 30°C with a speed of 1260 kmph. Its speed is known as Sonic Subsonic Super-sonic Mach Sonic Subsonic Super-sonic Mach ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The centre to centre spacing of heliport lighting along the periphery of landing and takeoff area should be 10.0 m 2.5 m 5.0 m 7.5 m 10.0 m 2.5 m 5.0 m 7.5 m ANSWER DOWNLOAD EXAMIANS APP
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