150 m
300 m
600 m
750 m
B. 300 m
4.8 kmph
6.4 kmph
8.0 kmph
9.6 kmph
Zero
300
3000
Unrestricted
L.M.M. (low powered middle marker)
V.H.F, (very high frequency)
L.O.M. (low powered outer marker)
All the above
Asphaltic concrete
Rubberised tar concrete
Plain concrete
All the above
Approximate geometric centre of the landing area, is called air port reference point
The boundaries of horizontal surface and conical surface are marked with reference to air port reference point
The location of the air port on a map is the position of air port reference point
All the above
Seven English alphabets
Last Seven English alphabets
First Seven English alphabets
First seven natural numbers
775 knots
75 knots
850 knots
675 knots
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
1500 m and 600 m
2100 m and 750 m
1500 m and 750 m
2100 m and 600 m
2500 m
2600 m
2700 m
2800 m
78 m
150 m
300 m
450 m
Master plan
Topographic plan
Grading plan
All the above
Passengers chamber
Pilot's cabin
Tail of aircraft
All the above
L.O.M. and L.M.M. are installed on one side and Localizer antenna on the other side
L.O.M. and Localizer are installed on one side and L.M.M. on the other side
Localizer and L.M.M. are installed on one side and L.O.M. on the other side
None of these
10°
20°
30°
40°
L.O.M. is installed at 7.2 km from the threshold
L.M.M. is installed at 1.0 km from the threshold
Localizer antenna is installed at 300 m from the other end of the runway
Glide slope antenna is installed at the centre of the runway about 150 m on one side
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
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
Control tower
Highest point of the landing area
Lowest point of the landing area
None of these
12.30 m
11.30 m
10.30 m
9.30 m
60 m
120 m
180 m
240 m
Load of the wings
Gross total weight of the aircraft/ load of the wings
Gross total weight of the aircraft/ wing area
Gross total weight of the aircraft/total available H.P of engines
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
135°
31
13
Both (c) and (d)
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
0.10 %
0.26 %
0.43 %
0.65 %
Aircraft rear loading door is far away from terminal building.
Hot blast is directed towards the terminal building
Overall apron area required is more
All the above
2716 m
2816 m
2916 m
3016 m
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.
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