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Airport Engineering

Airport Engineering
Beaufort scale is used to determine

Direction of winds
None of these
Height of air-crafts
Strength of winds

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Airport Engineering
Conical surface of the approach area rises outwards

1 in 10
1 in 25
1 in 15
1 in 20

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

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

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Airport Engineering
The coordinates of the ends of a runway are (5000, 5000) and (8000, 7000). The co-ordinates of another runway are (4600, 5100) and (7000, 5300). The co-ordinates of the A.R.P. are

(8000, 7000)
(6500, 6000)
(61500, 5600)
(5800, 5200)

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Airport Engineering
The length of runway under standard conditions is 2000 m. The elevation of airport site is 300 m. Its reference temperature is 33.05°C. If the runway is to be constructed with an effective gradient of 0.25 percent, the corrected runway length will be

2500 m
2700 m
2600 m
2800 m

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Airport Engineering
For supersonic transport aircraft, the minimum turning radius of taxiway is

120 m
60 m
240 m
180 m

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