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Airport Engineering

Airport Engineering
For Class ‘A’ Air port the difference of reduced levels of higher and lower edges of the conical surface, is

100 m
25 m
75 m
50 m

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Airport Engineering
The cruising speed of the aircraft is 500 kmph. If there is a head wind of 50 kmph, then the air speed and ground speed of the aircraft respectively will be

450 kmph and 500 kmph
500 kmph and 450 kmph
500 kmph and 500 kmph
450 kmph and 450 kmph

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Airport Engineering
The slope of the obstruction clearance line from the boundary of the heliport should be

0.045138888888889
0.047222222222222
0.069444444444444
0.043055555555556

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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

0.5
0.6
0.75
0.4

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Airport Engineering
As per ICAO recommendation, the rate of change of longitudinal gradient per 30 m length of vertical curve for A and B type of airports is limited to a maximum of

0.002
0.004
0.001
0.003

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Airport Engineering
The fuse large includes

Tail of aircraft
Pilot's cabin
Passengers chamber
All listed here

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MORE MCQ ON Airport Engineering

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