Only clearway
Only stop way
Either a clearway or a stop-way
Either a clearway or a stop-way or both
D. Either a clearway or a stop-way or both
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
150 m
140 m
160 m
175 m
3 %
4 %
5 %
7 %
Yellow
White
Black
Red
12.30 m
11.30 m
10.30 m
9.30 m
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
Atmosphere pressure
Air density
Reduced level
All the above
Improper compaction of sub-grade
Impact of heavy wheel loads
Punching effect
All the above
2500 m
3725 m
3000 m
3250 m
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
Sea level elevation
Standard sea level temperature (15°C)
Effective gradient percentage
All the above
A 1
B 2
B 3
G 7
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
1 in 10
1 in 15
1 in 20
1 in 25
1 m
3 m
4 m
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
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
775 knots
75 knots
850 knots
675 knots
N 70° W
290°
29°
W 20° N
0.1 %
0.2 %
0.3 %
0.4 %
50 m
100 m
150 m
250 m
Master plan
Topographic plan
Grading plan
All the above
2845 m
2910 m
3030 m
3130 m
3 m from runway end
6 m from runway end
10 m from runway end
15 m from runway end
15 %
20 %
25 %
35 %
Strength of winds
Direction of winds
Height of air-crafts
None of these
Beaufort scale
Wind indicator
Barometers
None of these
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
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
1 : 2
1 : 5
1 : 8
1 : 40