Airport Engineering Pick up the component not applicable to aeroplanes None of these Air screw Wings Engines None of these Air screw Wings Engines 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 Mach Super-sonic Subsonic Sonic Mach Super-sonic Subsonic ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the maximum structural landing weight Equal to the empty operating weight plus the payload 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 A is true but R is false Both A and R is true and R is the correct explanation of A Both A and R is true but R is not 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 the correct explanation of A Both A and R is true but R is not the correct explanation of A ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, the minimum basic runway length for A and E type of airport will be 2100 m and 600 m 1500 m and 600 m 2100 m and 750 m 1500 m and 750 m 2100 m and 600 m 1500 m and 600 m 2100 m and 750 m 1500 m and 750 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Conical surface of the approach area rises outwards 1 in 10 1 in 15 1 in 25 1 in 20 1 in 10 1 in 15 1 in 25 1 in 20 ANSWER DOWNLOAD EXAMIANS APP