Channelization of pavement is caused by constant use of tri-cycle gears of aircraft
Blast pads are used over cohesionless soils to resist erosion due to tremendous speed of the jet blast
Over-run areas of at least 300 m length on either side of the runway are provided
None of these
D. None of these
The speed of the aircraft relative to the ground, is called cruising speed
The speed of the aircraft relative to wind, is called air speed
When wind is blowing the direction of the flight, air speed is less than cruising speed
All the above
Against the wind direction
Along the wind direction
Perpendicular to wind direction
None of these
Along the extended centre line of runway end
About 1 km. ahead of the runway threshold
At the runway threshold
About 7 km. ahead of the runway threshold
Apron
Hanger
Terminal building
Holding apron
Black
Red
Yellow
Green
Longest line on wind rose diagram
Shortest line on the wind rose diagram
Line clear of wind rose diagram
None of these
Yellow
White
Black
Red
15 %
20 %
25 %
35 %
1 : 5
1 : 7
1 : 10
1 : 12
20 m
30 m
45 m
51 m
20°
30°
45°
60°
4.8 kmph
6.4 kmph
8.0 kmph
9.6 kmph
Sound at 0°C is 1190 kmph
Sound varies 2.4 kmph per degree centigrade rise in temperature
Sound at 0°C is called one Mach
All the above
The distance between the points of intersection of the extreme tangents to the transition curve is kept greater than 7500 m × sum of grade changes at the point of intersection
The rate of change of grade is limited to 0.3% per 30 m length of the curve
According to I.C.A.O. the maximum longitudinal gradient along a runway is limited to 1.5%
All the above
Sea level elevation
Standard sea level temperature (15°C)
Effective gradient percentage
All the above
L.M.M. (low powered middle marker)
V.H.F, (very high frequency)
L.O.M. (low powered outer marker)
All the above
32
36
44
68
F.I.R. stands for flight information regions
Radius of control area is 160 km
Radius of control zone is 40 km
All the above
Asphaltic concrete
Rubberised tar concrete
Plain concrete
All the above
1929
1939
1947
1950
The maximum longitudinal grade is 3%
The permissible rate of change of grade is 1%
The permissible transverse grade is 1.5%
All the above
2360 m
2460 m
2560 m
2660 m
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
Alligator cracking
Mud pumping
Warping cracks
Shrinkage cracks
775 knots
75 knots
850 knots
675 knots
Seven English alphabets
Last Seven English alphabets
First Seven English alphabets
First seven natural numbers
Green
Red
White
Yellow
150 m
300 m
600 m
750 m
1 m
3 m
4 m
5 m
The centre line of the approach area coincides with that of the runway
Approach areas are measured in horizontal surfaces
Obstruction clearance surface and approach surface are same
All the above