1. The threshold markings are
a) 4 m wide
b) 1 m clear space between adjacents
c) 45 m in length
d) all the above.
a) 4 m wide
b) 1 m clear space between adjacents
c) 45 m in length
d) all the above.
a) 135°
b) 13
c) 31
d) both (c) and (b)
a) 2716 m
b) 2816 m
c) 2916 m
d) 3016 m
a) Landing speed is directly proportional to the wing loading
b) Wing loading remaining constant, the take off distance is directly proportional to the powder loading
c) Neither (a) nor (b)
d) Both (a) and (b)
a) Approach zone survey is carried out to determine the elevations of the protruding obstructions above horizontal, conical and transitional surfaces
b) The wind data of an air port is depicted in the form of a chart known as wind rose
c) The landing and take off of the air craft is made against the wind direction
d) All the above.
a) end of the runway
b) end of stopway
c) point where air craft becomes air borne
d) none of these.
a) Approximate geometric centre of the landing area, is called air port reference point
b) The boundaries of horizontal surface and conical surface are marked with reference to air port reference point
c) The location of the air port on a map is the position of air port reference point
d) All the above.
a) against the wind direction
b) along the wind direction
c) perpendicular to wind direction
d) none of these.
a) subsonic
b) sonic
c) super-sonic
d) Mach.
a) 1 in 4
b) 1 in 5
c) 1 in 6
d) 1 in 7
a) improper compaction of subgrade
b) impact of heavy wheel loads
c) punching effect
d) all the above.
a) In single engine aeroplanes, the engine is provided in the nose of the aircraft
b) In double engine aeroplanes, one engine on either wing is placed symmetrically
c) In three engine aeroplanes, two engines are placed on both wings and one engine is placed in the tail
d) None of these.
a) The speed of the aircraft relative to the ground, is called cruising speed
b) The speed of the aircraft relative to wind, is called air speed
c) When wind is blowing the direction of the flight, air speed is less than cruising speed
d) All the above.
a) control tower
b) highest point of the landing area
c) lowest point of the landing area
d) none of these.
a) 2500 m
b) 3725 m
c) 3000 m
d) 3250 m
a) sea level elevation
b) standard sea level temperature (15°C)
c) effective gradient percentage
d) all the above.
a) The basic length of a runway is increased at a rate of 7% per 300 m of elevation of M.S.L.
b) 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
c) The aerodrome reference temperature is the monthly mean of the mean daily temperature for the hottest month of the year
d) All the above.
a) atmosphere pressure
b) air density
c) reduced level
d) all the above.
a) The distance between the points of intersection of the extreme tangents to the transition curve is kept greater than 7500 m x sum of grade changes at the point of intersection
b) The rate of change of grade is limited to 0.3% per 30 m length of the curve
c) According to I.C.A.O. the maximum longitudinal gradient along a runway is limited to 1.5%
d) All the above.
a) 1 in 10
b) 1 in 15
c) 1 in 20
d) 1 in 25
a) main gears
b) nose wheel
c) tail wheel
d) all the above.
a) 25 m
b) 50 m
c) 75 m
d) 100 m
a) strength of winds
b) direction of winds
c) height of air-crafts
d) none of these.
a) passengers chamber
b) pilot's cabin
c) tail of aircraft
d) all the above.
a) Air screw converts the energy given by the engine into speed
b) The propellers which are driven by turbine engines, are technically called turboprops
c) The aircraft which is filled with a fan infront of turbo-jet engine, is called turbofan propelled aeroplane
d) All the above.
a) 12.30 m
b) 11.30 m
c) 10.30 m
d) 9.30 m
a) asphaltic concrete
b) rubberised tar concrete
c) plain concrete
d) all the above.
a) I.L.S. (instrument landing system)
b) V.H.F, (very high frequency)
c) L.O.M. (low powered outer marker)
d) All the above
a)
b)
c)
d) None of these.
a) Channelization of pavement is caused by constant use of tri-cycle gears of aircraft
b) Blast pads are used over cohesionless soils to resist erosion due to tremendous speed of the jet blast
c) Over-run areas of at least 300 m length on either side of the runway are provided
d) None of these.
a) 1 in 20
b) 1 in 30
c) 1 in 40
d) 1 in 50
a) sound at 0°C is 1190 km p.h.
b) sound varies 2.4 km p.h. per degree centrigrade rise in temperature
c) sound at 0°C is called one Mach
d) All the above.
a) The centre line of the approach area coincides with that of the runway
b) Approach areas are measured in horizontal surfaces
c) The imaginary inclined plane which is directly above the approach area is called approach surface
d) All the above.
a) (6500, 6000)
b) (5800, 5200)
c) (61500, 5600)
d) (8000, 7000)
a) 150 m
b) 140 m
c) 160 m
d) 175 m
a) F.I.R. stands for flight information regions
b) F.I.C. stands for flight information centre
c) Radius of control area is 160 km
d) All the above.
a) N 70° W
b) 290°
c) 29°
d) W 20° N
a) longest line on wind rose diagram
b) shortest line on the wind rose diagram
c) line clear of wind rose diagram
d) none of these.
a) 1929
b) 1939
c) 1947
d) 1950
a) 775 knots
b) 75 knots
c) 850 knots
d) 675 knots
a) The maximum longitudinal grade is 3%
b) The permissible rate of change of grade is 1%
c) The permissible transverse grade is 1.5%
d) All the above.
a) Runway edge from the landing side, is called threshold
b) Localizer indicates to the pilot his position with respect to the proposed alignment
c) The glide slope indicates the correct angle of descent
d) All the above.
a) A 1
b) B 2
c) B 3
d) G 7
a) Seven English alphabets
b) Last Seven English alphabets
c) First Seven English alphabets
d) First seven natural numbers.
a) L.O.M. is installed at 7.2 km from the threshold
b) L.M.M. is installed at 1.0 km from the threshold
c) Glide slope antenna is installed at the centre of the runway about 150 m on one side
d) None of these.
a) Seven English alphabets
b) Last Seven English alphabets
c) First seven numbers
d) None of these.
a) Benfort scale
b) Wind indicator
c) Barometres
d) None of these.
a) 10°
b) 20°
c) 30°
d) 40°
a) black
b) red
c) yellow
d) green
a) 1500 m
b) 1200 m
c) 1000 m
d) 800 m
a) 3070 m
b) 3060 m
c) 3075 m
d) none of these.
a) 1 m
b) 3 m
c) 4 m
d) 5 m
a) Minimum turning radius of aircrafts decides the size of the apron and the radius of the curves at taxi-ends
b) Take off and landing distances for an aircraft, determine the minimum runway length
c) The length of the normal haul of the air craft decides the frequency of operation
d) All the above.
a) green
b) red
c) white
d) yellow
a) wings
b) engines
c) air screw
d) none of these.
a) ends of the runway
b) point of intersection of the obstruction clearance line and the extended plane of the runway surface, and the other end of the runway
c) point of intersection of the glide path and the extended plane of the runway surface and the other end of the runway
d) ends of the clear way on either side.
a) master plan
b) topograhic plan
c) grading plan
d) all the above.
a) 20°
b) 30°
c) 45°
d) 60°
a) 15%
b) 20%
c) 25%
d) 35%
a) L-shape
b) T-shape
c) X-shape
d) All the above.
a) 3%
b) 4%
c) 5%
d) 7%
a) 145 m
b) 152.5 m
c) 162.5 m
d) 172.5 m
a) L.O.M. and L.M.M. are installed on one side and Localizer antenna on the other side
b) L.O.M. and Localizer are installed on one side and L.M.M. on the other side
c) Localizer and L.M.M. are installed on one side and L.O.M. on the other side
d) None of these.
a) Tar concrete pavements are suitable if fuel spillage occurs
b) Rubberised tar concrete hot blast as well as spillage
c) Epoxy asphalt concrete resists the jet fuels and provides more elastic pavement
d) All the above.
a) 2360 m
b) 2460 m
c) 2560 m
d) 2660 m