Airport Engineering Castor angle is defined as the angle Between the direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the horizontal and the fuselage axis Between the direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the horizontal and the fuselage axis 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 22.5 m × 22.5 m 60 m × 120 m 30 m × 30 m 22.5 m × 30 m 22.5 m × 22.5 m 60 m × 120 m 30 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Which of the following is an example of failure in flexible pavements? Mud pumping Shrinkage cracks Alligator cracking Warping cracks Mud pumping Shrinkage cracks Alligator cracking Warping cracks ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: 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 Equal to empty operating weight Equal to sum of empty operating weight and the maximum pay load ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering To cope up high temperature of 196°C, the taxi ways and aprons are constructed with All listed here Plain concrete Rubberised tar concrete Asphaltic concrete All listed here Plain concrete Rubberised tar concrete Asphaltic concrete 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° 13 31 Both (C) and (D) 135° 13 31 Both (C) and (D) ANSWER DOWNLOAD EXAMIANS APP
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