Subsonic
Sonic
Super-sonic
Mach
B. Sonic
20°
30°
45°
60°
2845 m
2910 m
3030 m
3130 m
Green
Red
White
Yellow
1 and 2 are correct
2 and 3 are correct
1 and 3 are correct
1, 2 and 3 are correct
A 1
B 2
B 3
G 7
450 kmph and 500 kmph
500 kmph and 450 kmph
450 kmph and 450 kmph
500 kmph and 500 kmph
Yellow
White
Black
Red
Seven English alphabets
Last Seven English alphabets
First Seven English alphabets
First seven natural numbers
Only clearway
Only stop way
Either a clearway or a stop-way
Either a clearway or a stop-way or both
Along the extended centre line of runway end
About 1 km. ahead of the runway threshold
At the runway threshold
About 7 km. ahead of the runway threshold
1 : 2
1 : 5
1 : 8
1 : 40
L.M.M. (low powered middle marker)
V.H.F, (very high frequency)
L.O.M. (low powered outer marker)
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
10°
20°
30°
40°
Channelization of pavement is caused by constant use of tri-cycle gears of aircraft
Blast pads are used over cohesionless soils to resist erosion due to tremendous speed of the jet blast
Over-run areas of at least 300 m length on either side of the runway are provided
None of these
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
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
3 %
4 %
5 %
7 %
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)
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
Control tower
Highest point of the landing area
Lowest point of the landing area
None of these
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
Wings
Engines
Air screw
None of these
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
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
12.30 m
11.30 m
10.30 m
9.30 m
Apron
Hanger
Terminal building
Holding apron
Black
Red
Yellow
Green
40 %
50 %
60 %
75 %
Passengers chamber
Pilot's cabin
Tail of aircraft
All the above