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Airport Engineering

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

0.15
0.25
0.2
0.35

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Airport Engineering
The size of landing area for multi engine helicopters operating under 1 FR conditions is

22.5 m × 30 m
30 m × 30 m
60 m × 120 m
22.5 m × 22.5 m

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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
As per ICAO, for A, B, and C type of airports, maximum effective, transverse and longitudinal grades in percentage respectively are

1.0, 1.5 and 1.5
2.0, 2.0 and 2.0
1.5, 1.5 and 2.0
1.0, 1.5 and 2.0

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Airport Engineering
The strength of winds is measured with the help of

None of these
Barometers
Beaufort scale
Wind indicator

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Airport Engineering
For Class ‘A’ Air port the difference of reduced levels of higher and lower edges of the conical surface, is

75 m
50 m
25 m
100 m

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