1 in 10
1 in 15
1 in 20
1 in 25
C. 1 in 20
Both A and R is true and R is the correct explanation of A
Both A and R is true but R is not the correct explanation of A
A is true but R is false
A is false but R is true
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
450 kmph and 500 kmph
500 kmph and 450 kmph
450 kmph and 450 kmph
500 kmph and 500 kmph
Strength of winds
Direction of winds
Height of air-crafts
None of these
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
L.M.M. (low powered middle marker)
V.H.F, (very high frequency)
L.O.M. (low powered outer marker)
All the above
1 m
3 m
4 m
5 m
135°
31
13
Both (c) and (d)
775 knots
75 knots
850 knots
675 knots
1500 m
1200 m
1000 m
800 m
20°
30°
45°
60°
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
Seven English alphabets
Last Seven English alphabets
First Seven English alphabets
First seven numbers
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
20 m
30 m
45 m
51 m
Sound at 0°C is 1190 kmph
Sound varies 2.4 kmph per degree centigrade rise in temperature
Sound at 0°C is called one Mach
All the above
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
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
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
3070 m
3060 m
3075 m
3015 m
2.5 m
5.0 m
7.5 m
10.0 m
1 in 4
1 in 5
1 in 6
1 in 7
1 and 2 are correct
2 and 3 are correct
1 and 3 are correct
1 alone is correct
3 m and 30 m
4.2 m and 30 m
4.2 m and 50 m
3 m and 45 m
Only clearway
Only stop way
Either a clearway or a stop-way
Either a clearway or a stop-way or both
3 m from runway end
6 m from runway end
10 m from runway end
15 m from runway end
4 m wide
1 m clear space between adjacent
Placed symmetrically on either side of the runway centre line
All the above
Apron
Hanger
Terminal building
Holding apron
Beaufort scale
Wind indicator
Barometers
None of these
1 in 20
1 in 30
1 in 40
1 in 50