A. 60 m
B. 120 m
C. 180 m
D. 240 m
Related Mcqs:
- 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 - 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 - 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 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 - 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 - 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 - 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 - 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 - 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 - Which of the following is used for servicing and repairs of the aircraft ?
A. Apron
B. Hanger
C. Terminal building
D. holding apron