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Airport Engineering

Airport Engineering
Beaufort scale is used to determine

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

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Airport Engineering
The width and interval of transverse centre line bars along the extended centre line of runway, in approach lighting system are

3 m and 45 m
4.2 m and 30 m
3 m and 30 m
4.2 m and 50 m

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Airport Engineering
Geometric design of holding apron of these statements

1 and 3 are correct
1 alone is correct
1 and 2 are correct
2 and 3 are correct

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Airport Engineering
The main disadvantage of angle nose out parking configuration of aircraft is that the

Hot blast is directed towards the terminal building
All listed here
Overall apron area required is more
Aircraft rear loading door is far away from terminal building

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Airport Engineering
The length of a runway under standard atmospheric conditions is 1800 m. If the actual reduced level of the site is 1200 m, the design length of the runway is

2560 m
2360 m
2460 m
2660 m

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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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