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Airport Engineering

Airport Engineering
The thickness design of the pavement, is decided on the load carried by

Nose wheel
All listed here
Tail wheel
Main gears

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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
100 m
25 m

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Airport Engineering
For the proposed air port, the survey project provides

Topographic plan
All listed here
Master plan
Grading plan

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Airport Engineering
Zero fuel weight of an aircraft is:

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

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Airport Engineering
Beaufort scale is used to determine

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

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Airport Engineering
For determining the basic runway length, the landing case requires that aircraft should come to a stop within p % of the landing distance. The value of p is

0.4
0.6
0.75
0.5

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