2500 m
3725 m
3000 m
3250 m
B. 3725 m
1 in 20
1 in 30
1 in 40
1 in 50
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
0.10 %
0.26 %
0.43 %
0.65 %
Aircraft rear loading door is far away from terminal building.
Hot blast is directed towards the terminal building
Overall apron area required is more
All the above
Approach zone survey is carried out to determine the elevations of the protruding obstructions above horizontal, conical and transitional surfaces
The wind data of an air port is depicted in the form of a chart known as wind rose
The landing and takeoff of the air craft is made against the wind direction
All the above
Sea level elevation
Standard sea level temperature (15°C)
Effective gradient percentage
All the above
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
The centre line of the approach area coincides with that of the runway
Approach areas are measured in horizontal surfaces
Obstruction clearance surface and approach surface are same
All the above
Longest line on wind rose diagram
Shortest line on the wind rose diagram
Line clear of wind rose diagram
None of these
25 m
50 m
75 m
100 m
Apron
Hanger
Terminal building
Holding apron
20 m
30 m
45 m
51 m
60 m
120 m
180 m
240 m
1 m
3 m
4 m
5 m
Control tower
Highest point of the landing area
Lowest point of the landing area
None of these
150 m
300 m
600 m
750 m
Master plan
Topographic plan
Grading plan
All the above
1 and 2 are correct
2 and 3 are correct
1 and 3 are correct
1, 2 and 3 are correct
50 m
100 m
150 m
250 m
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)
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
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
Strength of winds
Direction of winds
Height of air-crafts
None of these
1929
1939
1947
1950
135°
31
13
Both (c) and (d)
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 %
20 %
25 %
35 %
2845 m
2910 m
3030 m
3130 m
L.M.M. (low powered middle marker)
V.H.F, (very high frequency)
L.O.M. (low powered outer marker)
All the above
2716 m
2816 m
2916 m
3016 m