Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 30 m × 30 m 60 m × 120 m 22.5 m × 30 m 22.5 m × 22.5 m 30 m × 30 m 60 m × 120 m 22.5 m × 30 m 22.5 m × 22.5 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The width and interval of transverse centre line bars along the extended centre line of runway, in approach lighting system are 3 m and 45 m 3 m and 30 m 4.2 m and 50 m 4.2 m and 30 m 3 m and 45 m 3 m and 30 m 4.2 m and 50 m 4.2 m and 30 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Consider the following statements regarding ICAO recommendation for correction to basic runway length of these statements1. The basic runway length should be increased at the rate of 7 percent per 300 m rise in elevation above the mean sea level.2. The basic runway length after having been corrected for elevation should be further increased at the rate of 1 percent for every 1°C rise in airport reference temperature above the standard atmospheric temperature at that elevation.3. The runway length after having been corrected for elevation and temperature should be further increased at the rate of 20% for every 1 percent of effective gradient. 1 and 3 are correct 1, 2 and 3 are correct 1 and 2 are correct 2 and 3 are correct 1 and 3 are correct 1, 2 and 3 are correct 1 and 2 are correct 2 and 3 are correct ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of runway is increased per 300 m rise above M.S.L. 0.03 0.04 0.07 0.05 0.03 0.04 0.07 0.05 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For supersonic transport aircraft, the minimum turning radius of taxiway is 240 m 60 m 120 m 180 m 240 m 60 m 120 m 180 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Beaufort scale is used to determine Height of air-crafts None of these Strength of winds Direction of winds Height of air-crafts None of these Strength of winds Direction of winds ANSWER DOWNLOAD EXAMIANS APP
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