1.
Zero fuel weight of an aircraft is
A
equal to empty operating weight
B
equal to maximum landing weight
C
less than empty operating weight
D
equal to sum of empty operating weight and the maximum pay load
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Zero fuel weight of an aircraft is
equal to empty operating weight
equal to maximum landing weight
less than empty operating weight
equal to sum of empty operating weight and the maximum pay load
Which of the following is used for servicing and repairs of the aircraft ?
Apron
Hanger
Terminal building
holding apron
Which of the following is an example of failure in flexible pavements ?
Alligator cracking
Mud pumping
Warping cracks
Shrinkage cracks
The width and interval of transverse centre line bars along the extended centre line of runway, in approach lighting system are
3 m and 30 m
4.2 m and 30 m
4.2 m and 50 m
3 m and 45 m
The minimum width of safety area for instrumental runway as per ICAO specifications should be
78 m
150 m
300 m
450 m
The minimum width of clearway is
50 m
100 m
150 m
250 m
The engine failure case for determining the basic runway length may require
only clearway
only stop way
either a clearway or a stopway
either a clearway or a stopway or both
The capacity of parallel runway pattern depends upon
weather conditions and navigational aids available
lateral spacing between two runways and weather conditions
lateral spacing between two runways and navigational aids available
lateral spacing between two runways, weather conditions and navigational aids available
Runway threshold is indicated by a series of parallel lines starting from a distance of
3 m from runway end
6 m from runway end
10 m from runway end
15m from runway end
Maximum gross take-off weight of an aircraft is
equal to the maximum structural landing weight
less than the maximum structural landing weight
more than the maximum structural landing weight
equal to the empty operating weight plus the payload
For supersonic transport aircraft, the minimum turning radius of taxiway is
60 m
120 m
180 m
240 m
Castor angle is defined as the angle
formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear
between the direction of wind and the longitudinal axis of the runway
between the true speed of the aircraft and the crosswind component
between the horizontal and the fuselage axis
Calm period is the percentage of time during which wind intensity is less than
4.8 kmph
6.4 kmph
8.0 kmph
9.6 kmph
As per ICAO, for airports serving big aircrafts, the crosswind component should not exceed
15 kmph
25 kmph
35 kmph
45 kmph
According to ICAO, all markings on the runways are
Yellow
White
Black
Red