4 m wide
1 m clear space between adjacent
Placed symmetrically on either side of the runway centre line
All the above
D. All the above
40 %
50 %
60 %
75 %
135°
31
13
Both (c) and (d)
1929
1939
1947
1950
Only clearway
Only stop way
Either a clearway or a stop-way
Either a clearway or a stop-way or both
1 and 2 are correct
2 and 3 are correct
1 and 3 are correct
1, 2 and 3 are correct
1500 m and 600 m
2100 m and 750 m
1500 m and 750 m
2100 m and 600 m
60 m
120 m
180 m
240 m
Minimum turning radius of aircrafts decides the size of the apron and the radius of the curves at taxi-ends
Take off and landing distances for an aircraft, determine the minimum runway length
The length of the normal haul of the air craft decides the frequency of operation
All the above
15 kmph
25 kmph
35 kmph
45 kmph
1 in 10
1 in 15
1 in 20
1 in 25
1 in 4
1 in 5
1 in 6
1 in 7
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
3070 m
3060 m
3075 m
3015 m
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
450 kmph and 500 kmph
500 kmph and 450 kmph
450 kmph and 450 kmph
500 kmph and 500 kmph
Both A and R is true and R is the correct explanation of A
Both A and R is true and R is not the correct explanation of A
A is true but R is false
A is false but R is true
Beaufort scale
Wind indicator
Barometers
None of these
1 and 2 are correct
2 and 3 are correct
1 and 3 are correct
1 alone is correct
775 knots
75 knots
850 knots
675 knots
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
10°
20°
30°
40°
Master plan
Topographic plan
Grading plan
All the above
Zero
300
3000
Unrestricted
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
Ends of the runway
Point of intersection of the obstruction clearance line and the extended plane of the runway surface, and the other end of the runway
Point of intersection of the glide path and the extended plane of the runway surface and the other end of the runway
Ends of the clear way on either side
The basic length of a runway is increased at a rate of 7% per 300 m of elevation of M.S.L.
The standard temperature at the site is obtained by reducing the standard sea level temperature of 15°C at the rate of 6.5°C per 1000 m rise in elevation
The aerodrome reference temperature is the monthly mean of the mean daily temperature for the hottest month of the year
All the above
Passengers chamber
Pilot's cabin
Tail of aircraft
All the above
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
A 1
B 2
B 3
G 7