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Airport Engineering

Airport Engineering
The bearing of the longest line of a wind rose is S 45° E, the bearing of the runway will be numbered

135°
31
Both (C) and (D)
13

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Airport Engineering
The bearing of the runway at threshold is 290°, the runway number is

W 20° N
29°
N 70° W
290°

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

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Airport Engineering
The engine failure case for determining the basic runway length may require

Only clearway
Either a clearway or a stop-way
Only stop way
Either a clearway or a stop-way or both

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Airport Engineering
The depressions and undulations in the pavement, are caused due to

Impact of heavy wheel loads
All listed here
Punching effect
Improper compaction of sub-grade

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Airport Engineering
In approach areas of runways equipped with instrumental landing facilities any object within 4.5 km distance from runway end shall be considered as an obstruction if its height is more than

20 m
30 m
51 m
45 m

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