The runway orientation is made so that landing and takeoff are

The landing and takeoff of the air craft is made against the direction of wind. In no case the centre line of the runway should make an angle with the wind direction exceeding

A

10°

B

20°

C

30°

D

40°

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 %

The centre to centre spacing of heliport lighting along the periphery of landing and takeoff area should be

A

2.5 m

B

5.0 m

C

7.5 m

D

10.0 m

The power available for takeoff and climb in case of turbojet engine as compared to reciprocating engine is

A

Less

B

More

C

Same

D

May be less or more depending on ambient conditions

Maximum gross takeoff 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

Choose the appropriate word for the blanks. The plane ....... the runway ....... a few yards and - crashed into the paddy field.

A

Missed, about

B

Hit, beyond

C

Missed, by

D

Crossed, beyond

Total correction for elevation, temperature and gradient for a runway should not be more than

A

15 %

B

20 %

C

25 %

D

35 %

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

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

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

The runway orientation is made so that landing and takeoff are

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