Airport Engineering Maximum gross takeoff weight of an aircraft is Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload 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 0.004 0.001 0.002 0.003 0.004 0.001 0.002 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The maximum value of the angle of turning of the nose gear large jet aircrafts, is limited to 30° 60° 20° 45° 30° 60° 20° 45° ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The depressions and undulations in the pavement, are caused due to Improper compaction of sub-grade Impact of heavy wheel loads Punching effect All listed here Improper compaction of sub-grade Impact of heavy wheel loads Punching effect All listed here ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For supersonic transport aircraft, the minimum turning radius of taxiway is 120 m 240 m 60 m 180 m 120 m 240 m 60 m 180 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 2845 m 3030 m 2910 m 3130 m 2845 m 3030 m 2910 m 3130 m ANSWER DOWNLOAD EXAMIANS APP
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