2500 m
2600 m
2700 m
2800 m
C. 2700 m
N 70° W
290°
29°
W 20° N
Tar concrete pavements are suitable if fuel spillage occurs
Rubberised tar concrete hot blast as well as spillage
Epoxy asphalt concrete sets in very small time
All the above
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
1 in 20
1 in 30
1 in 40
1 in 50
Strength of winds
Direction of winds
Height of air-crafts
None of these
Seven English alphabets
Last Seven English alphabets
First Seven English alphabets
First seven natural numbers
40 %
50 %
60 %
75 %
150 m
140 m
160 m
175 m
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
Sea level elevation
Standard sea level temperature (15°C)
Effective gradient percentage
All the above
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
2.5 m
5.0 m
7.5 m
10.0 m
In single engine aeroplanes, the engine is provided in the nose of the aircraft
In double engine aeroplanes, one engine on either wing is placed symmetrically
In three engine aeroplanes, two engines are placed on both wings and one engine is placed in the tail
None of these
3 m from runway end
6 m from runway end
10 m from runway end
15 m from runway end
Main gears
Nose wheel
Tail wheel
All the above
3 m and 30 m
4.2 m and 30 m
4.2 m and 50 m
3 m and 45 m
4 m wide
1 m clear space between adjacent
Placed symmetrically on either side of the runway centre line
All the above
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
2716 m
2816 m
2916 m
3016 m
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
L.M.M. (low powered middle marker)
V.H.F, (very high frequency)
L.O.M. (low powered outer marker)
All the above
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
2360 m
2460 m
2560 m
2660 m
20 m
30 m
45 m
51 m
Longest line on wind rose diagram
Shortest line on the wind rose diagram
Line clear of wind rose diagram
None of these
Beaufort scale
Wind indicator
Barometers
None of these
1 m
3 m
4 m
5 m
End of the runway
End of stop-way
Point where air craft becomes air borne
Point where air craft attains a height of 10.7 m
0.10 %
0.26 %
0.43 %
0.65 %