Airport Engineering Geometric design of holding apron of these statements 1 alone is correct 1 and 2 are correct 2 and 3 are correct 1 and 3 are correct 1 alone is correct 1 and 2 are correct 2 and 3 are correct 1 and 3 are correct 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. 2 and 3 are correct 1 and 2 are correct 1 and 3 are correct 1, 2 and 3 are correct 2 and 3 are correct 1 and 2 are correct 1 and 3 are correct 1, 2 and 3 are correct ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per UK design criteria, if LCN of aircraft is between 1.25 to 1.5 times the LCN of pavement, then the number of movements allowed are 300 Unrestricted 3000 Zero 300 Unrestricted 3000 Zero ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, the minimum basic runway length for A and E type of airport will be 1500 m and 600 m 1500 m and 750 m 2100 m and 600 m 2100 m and 750 m 1500 m and 600 m 1500 m and 750 m 2100 m and 600 m 2100 m and 750 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Which of the following factors are taken into account for estimating the runway length required for aircraft landing?1. Normal maximum temperature2. Airport elevation3. Maximum landing weight4. Effective runway gradientSelect the correct answer using the codes given below Codes: 2 and 3 1,2 and 4 1,2,3 and 4 1,3, and 4 2 and 3 1,2 and 4 1,2,3 and 4 1,3, and 4 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is Less than the maximum structural landing weight Equal to the empty operating weight plus the payload More than the maximum structural landing weight Equal to the maximum structural landing weight Less than the maximum structural landing weight Equal to the empty operating weight plus the payload More than the maximum structural landing weight Equal to the maximum structural landing weight ANSWER DOWNLOAD EXAMIANS APP