Against the wind direction
Along the wind direction
Perpendicular to wind direction
None of these
A. Against the wind direction
N 70° W
290°
29°
W 20° N
20 m
30 m
45 m
51 m
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
Atmosphere pressure
Air density
Reduced level
All the above
Seven English alphabets
Last Seven English alphabets
First Seven English alphabets
First seven natural numbers
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
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
Passengers chamber
Pilot's cabin
Tail of aircraft
All the above
20°
30°
45°
60°
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)
1 : 5
1 : 7
1 : 10
1 : 12
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
2845 m
2910 m
3030 m
3130 m
Main gears
Nose wheel
Tail wheel
All the above
Equal to empty operating weight
Equal to maximum landing weight
Less than empty operating weight
Equal to sum of empty operating weight and the maximum pay load
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
Only clearway
Only stop way
Either a clearway or a stop-way
Either a clearway or a stop-way or both
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.M.M. (low powered middle marker)
V.H.F, (very high frequency)
L.O.M. (low powered outer marker)
All the above
3070 m
3060 m
3075 m
3015 m
1 in 4
1 in 5
1 in 6
1 in 7
Black
Red
Yellow
Green
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
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
Master plan
Topographic plan
Grading plan
All the above
Improper compaction of sub-grade
Impact of heavy wheel loads
Punching effect
All the above
78 m
150 m
300 m
450 m
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
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
1 : 2
1 : 5
1 : 8
1 : 40