Civil Engineering MCQs

Page No. 110

According to ICAO, all markings on the runways are___________________?


aYellow


bWhite


cBlack


dRed


View Answer White

The width and interval of transverse centre line bars along the extended centre line of runway, in approach lighting system are_________________?


a3 m and 30 m


b4.2 m and 30 m


c4.2 m and 50 m


d 3 m and 45 m


View Answer 4.2 m and 30 m

The slope of the obstruction clearance line from the boundary of the heliport should be________________?


a1:2


b1:5


c1:8


d 1:40


View Answer 1:8

The size of landing area for multiengined helicopters operating under 1FR conditions is______________?


a 22.5 m x 22.5 m


b30 m x 30 m


c22.5 m x 30 m


d 60 mx 120 m


View Answer 60 mx 120 m

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?


aBoth A and R are true and R is the correct explanation of A


bBoth A and R are true but R is not the correct explanation of A


cA is true but R is false


d A is false but R is true



For supersonic transport aircraft, the minimum turning radius of taxiway is________________?


a60 m


b120 m


c180 m


d240 m


View Answer 180 m

Which of the following is an example of failure in flexible pavements ?


aAlligator cracking


bMud pumping


cWarping cracks


dShrinkage cracks


View Answer Alligator cracking

Which of the following is used for servicing and repairs of the aircraft ?


aApron


bHanger


cTerminal building


dholding apron


View Answer Hanger

Maximum gross take-off weight of an aircraft is__________________?


aequal to the maximum structural landing weight


bless than the maximum structural landing weight


c more than the maximum structural landing weight


d equal to the empty operating weight plus the payload



Castor angle is defined as the angle______________?


aformed by the longitudinal axis of the aircraft and the direction of movement of the nose gear


b between the direction of wind and the longitudinal axis of the runway


cbetween the true speed of the aircraft and the crosswind component


dbetween the horizontal and the fuselage axis



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