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Airport Engineering

Airport Engineering
From the end of an instrumental runway, the approach surface rises outwards

1 in 50
1 in 30
1 in 20
1 in 40

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Airport Engineering
Zero fuel weight of an aircraft is:

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

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

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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
Aircraft rear loading door is far away from terminal building
All listed here
Overall apron area required is more

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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

25 m
50 m
100 m
75 m

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

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

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