Airport Engineering The depressions and undulations in the pavement, are caused due to Punching effect Impact of heavy wheel loads Improper compaction of sub-grade All listed here Punching effect Impact of heavy wheel loads Improper compaction of sub-grade All listed here ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The fuse large includes All listed here Pilot's cabin Tail of aircraft Passengers chamber All listed here Pilot's cabin Tail of aircraft Passengers chamber 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: Both A and R is true but R is not the correct explanation of A Both A and R is true and R is 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 but R is not the correct explanation of A Both A and R is true and R is the correct explanation of A A is true but R is false A is false but R is true ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Two single runways may be arranged so as to have All listed here X-shape T-shape L-shape All listed here X-shape T-shape L-shape ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The threshold markings are Placed symmetrically on either side of the runway centre line 4 m wide All listed here 1 m clear space between adjacent Placed symmetrically on either side of the runway centre line 4 m wide All listed here 1 m clear space between adjacent ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Between the true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the direction of wind and the longitudinal axis of the runway Between the true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the direction of wind and the longitudinal axis of the runway ANSWER DOWNLOAD EXAMIANS APP
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