Airport Engineering The threshold markings are 1 m clear space between adjacent All listed here 4 m wide Placed symmetrically on either side of the runway centre line 1 m clear space between adjacent All listed here 4 m wide Placed symmetrically on either side of the runway centre line ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For supersonic transport aircraft, the minimum turning radius of taxiway is 60 m 120 m 240 m 180 m 60 m 120 m 240 m 180 m 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: 2 and 3 1,3, and 4 1,2,3 and 4 1,2 and 4 2 and 3 1,3, and 4 1,2,3 and 4 1,2 and 4 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 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 true but R is false A is false but R is true 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 true but R is false ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering If the width of the approach area near the runway end is 150 m, the width of the approach area at a distance of 3 kilometers from runway end will be 800 m 1200 m 1500 m 1000 m 800 m 1200 m 1500 m 1000 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/total available H.P of engines Load of the wings Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/total available H.P of engines Load of the wings Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area ANSWER DOWNLOAD EXAMIANS APP
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