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)
D. Both (a) and (b)
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
Load of the wings
Gross total weight of the aircraft/ load of the wings
Gross total weight of the aircraft/ wing area
Gross total weight of the aircraft/total available H.P of engines
15 kmph
25 kmph
35 kmph
45 kmph
450 kmph and 500 kmph
500 kmph and 450 kmph
450 kmph and 450 kmph
500 kmph and 500 kmph
1 in 10
1 in 15
1 in 20
1 in 25
22.5 m × 22.5 m
30 m × 30 m
22.5 m × 30 m
60 m × 120 m
150 m
300 m
600 m
750 m
40 %
50 %
60 %
75 %
775 knots
75 knots
850 knots
675 knots
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 aircraft per hour
2 aircrafts per hour
4 aircrafts per hour
16 aircrafts per hour
20 m
30 m
45 m
51 m
Only clearway
Only stop way
Either a clearway or a stop-way
Either a clearway or a stop-way or both
Longest line on wind rose diagram
Shortest line on the wind rose diagram
Line clear of wind rose diagram
None of these
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
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
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
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)
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.
Master plan
Topographic plan
Grading plan
All the above
Green
Red
White
Yellow
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
2.5 m
5.0 m
7.5 m
10.0 m
150 m
140 m
160 m
175 m
1929
1939
1947
1950
2500 m
3725 m
3000 m
3250 m
50 m
100 m
150 m
250 m
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 m
3 m
4 m
5 m