1, 2, 3 and 4
1, 3 and 4
2 and 3
1, 2 and 4
D. 1, 2 and 4
Strength of winds
Direction of winds
Height of air-crafts
None of these
Asphaltic concrete
Rubberised tar concrete
Plain concrete
All the above
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
1 and 2 are correct
2 and 3 are correct
1 and 3 are correct
1 alone is correct
50 m
100 m
150 m
250 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
Improper compaction of sub-grade
Impact of heavy wheel loads
Punching effect
All the above
32
36
44
68
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
20°
30°
45°
60°
12.30 m
11.30 m
10.30 m
9.30 m
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)
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
Seven English alphabets
Last Seven English alphabets
First Seven English alphabets
First seven natural numbers
3 %
4 %
5 %
7 %
775 knots
75 knots
850 knots
675 knots
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
Main gears
Nose wheel
Tail wheel
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
L.M.M. (low powered middle marker)
V.H.F, (very high frequency)
L.O.M. (low powered outer marker)
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
2716 m
2816 m
2916 m
3016 m
1 m
3 m
4 m
5 m
3070 m
3060 m
3075 m
3015 m
1 : 5
1 : 7
1 : 10
1 : 12
2500 m
2600 m
2700 m
2800 m
Against the wind direction
Along the wind direction
Perpendicular to wind direction
None of these
1500 m
1200 m
1000 m
800 m
A 1
B 2
B 3
G 7
78 m
150 m
300 m
450 m