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
Related Mcqs:
- 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 - The minimum width of clearway is_______________?
A. 50 m
B. 100 m
C. 150 m
D. 250 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 ICAO, for airports serving big aircrafts, the crosswind component should not exceed_________________?
A. 15 kmph
B. 25 kmph
C. 35 kmph
D. 45 kmph - 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 - 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 - 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 - For supersonic transport aircraft, the minimum turning radius of taxiway is________________?
A. 60 m
B. 120 m
C. 180 m
D. 240 m - 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 - 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
