Airport Engineering For supersonic transport aircraft, the minimum turning radius of taxiway is 120 m 60 m 180 m 240 m 120 m 60 m 180 m 240 m 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 Which of the following factors are taken into account for estimating the runway length required for aircraft landing?1. Normal maximum temperature2. Airport elevation3. Maximum landing weight4. Effective runway gradientSelect the correct answer using the codes given below Codes: 1,2,3 and 4 1,2 and 4 1,3, and 4 2 and 3 1,2,3 and 4 1,2 and 4 1,3, and 4 2 and 3 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to the International Civil Aviation Organization (I.C.A.O.), the runway lengths of aerodromes, have been coded by First Seven English alphabets Last Seven English alphabets Seven English alphabets First seven natural numbers First Seven English alphabets Last Seven English alphabets Seven English alphabets First seven natural numbers ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering In Instrumental landing system, the middle markers are located At the runway threshold About 7 km. ahead of the runway threshold Along the extended centre line of runway end About 1 km. ahead of the runway threshold At the runway threshold About 7 km. ahead of the runway threshold Along the extended centre line of runway end About 1 km. ahead of the runway threshold 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 Equal to the maximum structural landing weight Less than the maximum structural landing weight More than the maximum structural landing weight Equal to the empty operating weight plus the payload Equal to the maximum structural landing weight Less than the maximum structural landing weight ANSWER DOWNLOAD EXAMIANS APP
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