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
A. 1.0, 1.5 and 1.5
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
Subsonic
Sonic
Super-sonic
Mach
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
15 %
20 %
25 %
35 %
50 m
100 m
150 m
250 m
4.8 kmph
6.4 kmph
8.0 kmph
9.6 kmph
2845 m
2910 m
3030 m
3130 m
Seven English alphabets
Last Seven English alphabets
First Seven English alphabets
First seven natural numbers
Equal to the maximum structural landing weight
Less than the maximum structural landing weight
More than the maximum structural landing weight
Equal to the empty operating weight plus the payload
4 m wide
1 m clear space between adjacent
Placed symmetrically on either side of the runway centre line
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
1 : 5
1 : 7
1 : 10
1 : 12
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
1 in 4
1 in 5
1 in 6
1 in 7
145 m
152.5 m
162.5 m
172.5 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
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
150 m
140 m
160 m
175 m
32
36
44
68
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
Yellow
White
Black
Red
Runway edge from the landing side, is called threshold
Localizer indicates to the pilot his position with respect to the proposed alignment
The glide slope indicates the correct angle of descent
All the above
25 m
50 m
75 m
100 m
Atmosphere pressure
Air density
Reduced level
All the above
0.1 %
0.2 %
0.3 %
0.4 %
Only clearway
Only stop way
Either a clearway or a stop-way
Either a clearway or a stop-way or both
15 kmph
25 kmph
35 kmph
45 kmph
1 in 20
1 in 30
1 in 40
1 in 50
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.