Airport Engineering Runway threshold is indicated by a series of parallel lines starting from a distance of 6 m from runway end 3 m from runway end 10 m from runway end 15 m from runway end 6 m from runway end 3 m from runway end 10 m from runway end 15 m from runway end ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Airport elevation is the reduced level above M.S.L. of Highest point of the landing area None of these Control tower Lowest point of the landing area Highest point of the landing area None of these Control tower Lowest point of the landing area ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Between the true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis Between the direction of wind and the longitudinal axis of the runway 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 horizontal and the fuselage axis Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO recommendation, the rate of change of longitudinal gradient per 30 m length of vertical curve for A and B type of airports is limited to a maximum of 0.003 0.002 0.001 0.004 0.003 0.002 0.001 0.004 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering A gradient of + 0.08% is followed by a gradient of - 0.07%. If the permissible rate of change of grade is 0.003 per 30 meters, the length of the transition curve, is 140 m 150 m 160 m 175 m 140 m 150 m 160 m 175 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The bearing of the longest line of a wind rose is S 45° E, the bearing of the runway will be numbered 135° 31 Both (C) and (D) 13 135° 31 Both (C) and (D) 13 ANSWER DOWNLOAD EXAMIANS APP