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Airport Engineering

Airport Engineering
International Civil Aviation Organization (I.C.A.O.) was set up at Montreal (Canada), in

1929
1947
1939
1950

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Airport Engineering
Total correction for elevation, temperature and gradient for a runway should not be more than

0.2
0.35
0.15
0.25

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Airport Engineering
Zero fuel weight of an aircraft is:

Equal to empty operating weight
Equal to sum of empty operating weight and the maximum pay load
Equal to maximum landing weight
Less than empty operating weight

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Airport Engineering
The distance between main gears is 10 m, and the distance of nose gear from centre of main gears is 30 m. If the angle of turning is 60°, the distance of centre of rotation from the nearer main gear, is

9.30 m
11.30 m
12.30 m
10.30 m

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Airport Engineering
The thickness design of the pavement, is decided on the load carried by

Main gears
All listed here
Tail wheel
Nose wheel

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Airport Engineering
The total length of a runway is 1000 m. The elevation at distance 0,200 m, 400 m, 600 m, 800 m and 1000 m are 100.0 m, 99.2 m, 101.0 m, 101.8 m, 101.4 m and 101.0 m respectively. The effective gradient of runway will be.

0.0026
0.0065
0.0043
0.001

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