Airport Engineering Pick up the component not applicable to aeroplanes Air screw None of these Wings Engines Air screw None of these Wings Engines ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: 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 Equal to empty operating weight 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 1.0, 1.5 and 2.0 1.5, 1.5 and 2.0 1.0, 1.5 and 1.5 2.0, 2.0 and 2.0 1.0, 1.5 and 2.0 1.5, 1.5 and 2.0 1.0, 1.5 and 1.5 2.0, 2.0 and 2.0 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Assertion A : Airport capacity during IFR conditions is usually less than that during VFR conditions.Reason R: During clear weather condition (VFR), the aircrafts on final approach to runway can be spaced closer during poor visibility conditions.Select your answer based on the coding system given below: A is false but R is true Both A and R is true but R is not the correct explanation of A A is true but R is false Both A and R is true and R is the correct explanation of A A is false but R is true Both A and R is true but R is not the correct explanation of A A is true but R is false Both A and R is true and R is the correct explanation of A 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 Runway threshold is indicated by a series of parallel lines starting from a distance of 6 m from runway end 10 m from runway end 3 m from runway end 15 m from runway end 6 m from runway end 10 m from runway end 3 m from runway end 15 m from runway end ANSWER DOWNLOAD EXAMIANS APP
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