1 and 2 are correct
2 and 3 are correct
1 and 3 are correct
1, 2 and 3 are correct
A. 1 and 2 are correct
1500 m and 600 m
2100 m and 750 m
1500 m and 750 m
2100 m and 600 m
Atmosphere pressure
Air density
Reduced level
All the above
Wings
Engines
Air screw
None of these
145 m
152.5 m
162.5 m
172.5 m
32°C
35.5°C
48°C
25°C
L.M.M. (low powered middle marker)
V.H.F, (very high frequency)
L.O.M. (low powered outer marker)
All the above
1, 2, 3 and 4
1, 3 and 4
2 and 3
1, 2 and 4
60 m
120 m
180 m
240 m
Passengers chamber
Pilot's cabin
Tail of aircraft
All the above
1 and 2 are correct
2 and 3 are correct
1 and 3 are correct
1, 2 and 3 are correct
Landing speed is directly proportional to the wing loading
Wing loading remaining constant, the take off distance is directly proportional to the powder loading
Neither (a) nor (b)
Both (a) and (b)
22.5 m × 22.5 m
30 m × 30 m
22.5 m × 30 m
60 m × 120 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.
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
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
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
Longest line on wind rose diagram
Shortest line on the wind rose diagram
Line clear of wind rose diagram
None of these
1.0, 1.5 and 1.5
1.0, 1.5 and 2.0
1.5, 1.5 and 2.0
2.0, 2.0 and 2.0
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
50 m
100 m
150 m
250 m
15 kmph
25 kmph
35 kmph
45 kmph
Air screw converts the energy given by the engine into speed
The propellers which are driven by turbine engines, are technically called turboprops
The aircrafts which obtain the thrust directly from turbine engine, are called turbo-jets
All the above
78 m
150 m
300 m
450 m
Asphaltic concrete
Rubberised tar concrete
Plain concrete
All the above
1 aircraft per hour
2 aircrafts per hour
4 aircrafts per hour
16 aircrafts per hour
0.1 %
0.2 %
0.3 %
0.4 %
Master plan
Topographic plan
Grading plan
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
Strength of winds
Direction of winds
Height of air-crafts
None of these
Control tower
Highest point of the landing area
Lowest point of the landing area
None of these