Airport Engineering The fuse large includes Passengers chamber Tail of aircraft All listed here Pilot's cabin Passengers chamber Tail of aircraft All listed here Pilot's cabin ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, for A, B, and C type of airports, maximum effective, transverse and longitudinal grades in percentage respectively are 1.5, 1.5 and 2.0 2.0, 2.0 and 2.0 1.0, 1.5 and 2.0 1.0, 1.5 and 1.5 1.5, 1.5 and 2.0 2.0, 2.0 and 2.0 1.0, 1.5 and 2.0 1.0, 1.5 and 1.5 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle 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 Between the direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Assertion A : The ratio of arriving and departing aircrafts influences the airport capacity:Reason R : Landing operation is generally given priority over the taking off operation.Select your answer based on the coding system given below: A is true but R is false Both A and R is true and R is not the correct explanation of A Both A and R is true and R is the correct explanation of A A is false but R is true A is true but R is false Both A and R is true and R is not the correct explanation of A Both A and R is true and R is the correct explanation of A A is false but R is true ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is 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 Equal to the maximum structural landing weight ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Equal to empty operating weight Equal to maximum landing weight Equal to sum of empty operating weight and the maximum pay load Less than empty operating weight Equal to empty operating weight Equal to maximum landing weight Equal to sum of empty operating weight and the maximum pay load Less than empty operating weight ANSWER DOWNLOAD EXAMIANS APP
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