Airport Engineering The cruising speed of the aircraft is 500 kmph. If there is a head wind of 50 kmph, then the air speed and ground speed of the aircraft respectively will be 450 kmph and 500 kmph 450 kmph and 450 kmph 500 kmph and 500 kmph 500 kmph and 450 kmph 450 kmph and 500 kmph 450 kmph and 450 kmph 500 kmph and 500 kmph 500 kmph and 450 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The thickness design of the pavement, is decided on the load carried by All listed here Main gears Tail wheel Nose wheel All listed here Main gears Tail wheel Nose wheel 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 30 m × 30 m 60 m × 120 m 22.5 m × 22.5 m 22.5 m × 30 m 30 m × 30 m 60 m × 120 m 22.5 m × 22.5 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is Equal to the maximum structural landing weight More than the maximum structural landing weight Equal to the empty operating weight plus the payload Less than the maximum structural landing weight Equal to the maximum structural landing weight More than the maximum structural landing weight Equal to the empty operating weight plus the payload Less than the maximum structural landing weight ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: 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 Equal to empty operating weight ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For Class ‘A’ Air port the difference of reduced levels of higher and lower edges of the conical surface, is 100 m 50 m 25 m 75 m 100 m 50 m 25 m 75 m ANSWER DOWNLOAD EXAMIANS APP
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