Airport Engineering According to the International Civil Aviation Organization (I.C.A.O.) the strength of runway pavements, have been coded by First seven numbers Seven English alphabets Last Seven English alphabets First Seven English alphabets First seven numbers Seven English alphabets Last Seven English alphabets First Seven English alphabets ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For determining the basic runway length, the landing case requires that aircraft should come to a stop within p % of the landing distance. The value of p is 0.5 0.4 0.6 0.75 0.5 0.4 0.6 0.75 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The centre to centre spacing of heliport lighting along the periphery of landing and takeoff area should be 5.0 m 10.0 m 7.5 m 2.5 m 5.0 m 10.0 m 7.5 m 2.5 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 2 are correct 1, 2 and 3 are correct 2 and 3 are correct 1 and 3 are correct 1 and 2 are correct 1, 2 and 3 are correct 2 and 3 are correct 1 and 3 are correct ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The bearing of the runway at threshold is 290°, the runway number is 29° 290° N 70° W W 20° N 29° 290° N 70° W W 20° N ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines ANSWER DOWNLOAD EXAMIANS APP
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