1. As per ICAO recommendation,
minimum width of safety area for instrumental runway should be a) 78 m
b) 150
m
c) 300
m
d) 450
m
Ans: c
2. As per ICAO, for A, B, and C type of airports, maximum
effective, transverse and longitudinal grades in percentage respectively are
a)
1.0, 1.5 and 1.5
b) 1.0,
1.5 and 2.0
c) 1.5,
1.5 and 2.0
d) 2.0,
2.0 and 2.0
Ans: a
3. As per ICAO recommendation, the rate of change of
longitudinal gradient per 30 m length of vertical curve for A and B type of
airports is limited to a maximum of
a) 0.1 %
b) 0.2%
c) 0.3
%
d) 0.4%
Ans: a
4. Assertion A : The ratio of arriving and departing
aircrafts influences the airport capacity: Reason R :Landing operation is
generally given priority over the taking off operation. Select your answer
based on the coding system given below:
a) Both
A and R are true and R is the correct explanation of A
b) Both
A and R are true and R is not the correct explanation of A
c) A
is true but R is false.
d) A is
false but R is true.
Ans: a
5. An airport has 4 gates. If the weighted average
gate occupancy time is 30 minutes and gate utilisation factor is 0.5, then the
capacity of the gate will be
a) 1 aircraft per hour
b) 2
aircrafts per hour
c) 4
aircrafts per hour
d) 16
aircrafts per hour
Ans: c
7. The capacity of parallel runway pattern depends upon
a) weather
conditions and navigational aids available
b) lateral
spacing between two runways and weather conditions
c) lateral
spacing between two runways and navigational aids available
d) lateral
spacing between two runways, weather conditions and navigational aids
available.
Ans: d
8. The engine failure case for determining the basic
runway length may require
a) only clearway
b) only
stop way ,
c) either
a clearway or a stopway
d) either
a clearway or a stopway or both
Ans: d
9. The minimum width of clearway is
a) 50
m
b) 100
m
c) 150
m
d) 250
m
Ans: c
10. If the monthly mean of average daily temperature
for the hottest month of the year is 25° C and the monthly mean of the maximum
daily temperature of the same month of the year is 46° C, the airport reference
temperature is
a) 32°C
b) 35.5°C
c) 48°C
d) 25°C
Ans: c
11. Consider the following statements regarding iCAO
recommendation for correction to basic runway length
1.The basic runway length should be increased at
the rate of 7 percent per 300 m rise in elevation above the mean sea level.
2.The basic runway length after having been
corrected for elevation should be further increased at the rate of 1 percent
for every 1°C rise in airport reference temperature above the standard
atmospheric temperature at that elevation.
3.The runway length after having been corrected
for elevation and temperature should be further increased at the rate of 20%
for every 1 percent of effective gradient.
Of these statements
a) 1
and 2 are correct
b) 2
and 3 are correct
c) 1
and 3 are correct
d) 1,2
and 3 are correct
Ans: a
12. The total length of a runway is 1000 m.
The elevation at distance 0,200 m, 400 m, 600 m, 800 m and 1000 m are 100.0 m,
99.2 m, 101.0 m, 101.8 m, 101.4 m and 101.0 m respectively. The effective
gradient of runway will be.
a) 0.10%
b) 0.26%
c) 0.43
%
d) 0.65%
Ans: b
13. The length of runway under standard conditions is
2000 m. The elevation of airport site is 300 m. Its reference temperature is
33.05°C. If the runway is to be constructed with an effective gradient of 0.25
percent, the corrected runway length will be
a) 2500 m
b) 2600
m
c) 2700
m
d) 2800
m
Ans: c
14. As per ICAO, the minimum basic runway length for
A and E type of airport will be
a) 1500 m and 600 m
b) 2100
m and 750 m
c) 1500
m and 750 m
d) 2100
m and 600 m
Ans: d
15. Zero fuel weight of an aircraft is:
a) equal
to empty operating weight
b) equal
to maximum landing weight
c) less
than empty operating weight
d) equal
to sum of empty operating weight and the maximum pay load.
Ans: d
17. The cruising speed of the aircraft is 500 kmph. If
there is a head wind of 50 kmph, then the air speed and ground speed of the
aircraft respectively will be
a) 450 kmph and 500 kmph
b) 500
kmph and 450 kmph
c) 450
kmph and 450 kmph
d) 500
kmph and 500 kmph
Ans: a
19. As per ICAO, for airports serving big aircrafts,
the crosswind component should not exceed
a) 15 kmph
b) 25
kmph
c) 35
kmph
d) 45
kmph
Ans: c
20. Calm period is the percentage of time during
which wind intensity is less than
a) 4.8 kmph
b) 6.4
kmph
c) 8.0
kmph
d) 9.6
kmph
Ans: b
21. For determining the basic runway.length, the
landing case requires that aircraft should come to a stop within p % of the
landing distance. The value of p is
a) 40 %
b) 50%
c) 60%
d) 75%
Ans: c
22. According to ICAO, all markings on the runways are
a) Yellow
b) White
c) Black
d) Red
Ans: b
23. Runway threshold is indicated by a series of
parallel lines starting from a distance of
a) 3 m from runway end
b) 6 m
from runway end
c) 10
m from runway end
d) 15m
from runway end
Ans: b
24. The width and interval of transverse centre line
bars along the extended centre line of runway, in approach lighting system are
a) 3
m and 30 m
b) 4.2
m and 30 m
c) 4.2
m and 50 m
d) 3 m
and 45 m
Ans: b
25. In Intrumental landing system, the middle markers are
located
a) along
the extended centre
line of runway end
b) about 1 km.
ahead of the runway threshold
c) at
the runway threshold
d) about
7 km. ahead of the runway threshold
Ans: b
26. The size of landing area for multiengined
helicopters operating under 1FR conditions is
a) 22.5 m x 22.5 m
b) 30 m
x 30 m
c) 22.5
m x 30 m
d) 60
mx 120 m
Ans: d
27. The centre to centre spacing of heliport lighting along
the periphery of landing and take off area should be
a) 2.5
m
b) 5.0
m
c) 7.5
m
d) 10.0
m
Ans: c
28. The slope of the obstruction clearance line from
the boundary of the heliport should be
a) 1:2
b) 1:5
c) 1:8
d) 1:40
Ans: c
29. Assertion A :
Airport capacity during IFR conditions is usually less than that during
VFR conditions. Reason R: During clear weather condition (VFR), the aircrafts
on final approach to runway can be spaced closer during poor visibility
conditions.
Select your answer based on the coding system given below:
a) Both
A and R are true and R is the correct explanation of A
b) Both
A and R are true but R is not the correct explanation of A
c) A
is true but R is false
d) A is
false but R is true
Ans: a
30. Assertion A: The width of a taxiway is smaller than the
runway width. Reason R:The speed of the aircraft on a taxiway is greater than
that on runway. Select your answer
based on coding system given below
a) Both
A and R are true and R is the correct explanation of A
b) Both
A and R are true but R is not the correct explanation of A
c) A
is true but R is false
d) A is
false but R is true
Ans: c
31. For supersonic transport aircraft, the minimum
turning radius of taxiway is
a) 60 m
b) 120
m
c) 180
m
d) 240
m
Ans: c
33. As per UK design criteria, if LCN of aircraft is
between 1.25 to 1.5 times the LCN of pavement, then the number of movements
allowed are
a) Zero
b) 300
c) 3000
d) Unrestricted
Ans: b
34. Which of the following is an example of failure
in flexible pavements ?
a) Alligator cracking
b) Mud
pumping
c) Warping
cracks
d) Shrinkage
cracks
Ans: a
35. The main disadvantage of angle nose out parking
configuration of aircraft is that the
a) aircraft
rear loading door is far away from terminal building.
b) hot
blast is directed towards the terminal
building
c) overall
apron area required is more
d) all
the above
Ans: b
36. Which of the following is used for servicing and
repairs of the aircraft ?
a) Apron
b) Hanger
c) Terminal
building
d) holding
apron
Ans: b
37. The slope of the transitional surface for A, B
and C type of runway shall be
a) 1:5
b) 1:7
c) 1:10
d) 1:12
Ans: b
38. The length of clear zone for none instrument
runway of a small aircraft is
a) 150 m
b) 300
m
c) 600
m
d) 750
m
Ans: b
39. In approach areas of runways equipped with instrumental
landing facilities any object within 4.5 km distance from runway end shall be
considered as an obstruction if its height is more than
a) 20
m
b) 30 m
c) 45
m
d) 51 m
Ans: b
40. Maximum gross take-off weight of an aircraft is
a) equal to
the maximum structural landing weight
b) less than
the maximum structural landing weight
c) more
than the maximum structural landing
weight
d) equal
to the empty operating weight plus the payload
Ans: c
41. Consider the following statements: Wind rose diagram is
used for the purposes of
1. runway
orientation
2. estimating
the runway capacity
3. geometric
design of holding apron
Of these statements
a) 1
and 2 are correct
b) 2
and 3 are correct
c) 1
and 3 are correct
d) 1
alone is correct
Ans: d
42. Which of the following factors are taken into account
for estimating the runway length required for aircraft landing?
1. Normal
maximum temperature
2. Airport
elevation
3. Maximum
landing weight
4. Effective
runway gradient
Select the correct answer using the codes given below
Codes:
a) 1,2,3 and 4
b) 1,3,
and 4
c) 2
and 3
d) 1,2
and 4
Ans: d
43. In an airport, if 4 groups of 5 gates each located
well-separated are considered for traffic and the future to present traffic
ratio is 3, then the total requirement of future gates will be
a) 32
b) 36
c) 44
d) 68 Ans: b
44. Castor angle is defined as the angle
a) formed
by the longitudinal axis of the aircraft and the direction of movement of the
nose gear
b) between
the direction of wind and the longitudinal axis of the runway
c) between
the true speed of the aircraft and the crosswind component
d) between
the horizontal and the fuselage axis
Ans: a
45. The runway length after correcting for elevation and
temperature is 2845 m. If the effective gradient on runway is 0.5 percent then
the revised runway length will be
a) 2845 m
b) 2910 m
c) 3030 m
d) 3130 m
Ans: c
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