Airport Engineering Zero fuel weight of an aircraft is: Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load Equal to maximum landing weight Less than empty operating weight Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load Equal to maximum landing weight Less than empty operating weight ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In Instrumental landing system, the middle markers are located About 1 km. ahead of the runway threshold At the runway threshold About 7 km. ahead of the runway threshold Along the extended centre line of runway end About 1 km. ahead of the runway threshold At the runway threshold About 7 km. ahead of the runway threshold Along the extended centre line of runway end ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Which of the following is an example of failure in flexible pavements? Alligator cracking Warping cracks Shrinkage cracks Mud pumping Alligator cracking Warping cracks Shrinkage cracks Mud pumping ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering An aircraft is flying in an atmosphere of 30°C with a speed of 1260 kmph. Its speed is known as Sonic Super-sonic Subsonic Mach Sonic Super-sonic Subsonic Mach ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The height of the pilot's eye above the runway surface is assumed 5 m 3 m 4 m 1 m 5 m 3 m 4 m 1 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 22.5 m × 30 m 60 m × 120 m 22.5 m × 22.5 m 30 m × 30 m 22.5 m × 30 m 60 m × 120 m 22.5 m × 22.5 m 30 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
EXAMIANS