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Principles of Flight - ATPL - Airline Transport Pilot Licence
Test 10 domande Principles of Flight, tempo libero
1 - The manoeuvrability of an aeroplane is best when the:
Speed is low.
G. position is on the forward G. limit. G. is on the aft G. limit.
Flaps are down.
2 - The positive manoeuvring limit load factor for a light aeroplane in the utility category in the clean configuration is:
3 - Which statement is correct about a spring tab ?
At high IAS it behaves like a servo tab
Its main purpose is to increase stick force per g
At high IAS it behaves like a fixed extension of the elevator
At low IAS it behaves like a servo tab
4 - Extension of FOWLER type trailing edge lift augmentation devices, will produce:
A nose-up pitching moment
No pitching moment
A force which reduces drag
A nose-down pitching moment
5 - In which phase of the take-off is the aerodynamic effect of ice located on the wing leading edge most critical?
The last part of the rotation
All phases of the take-off are equally critical
During climb with all engines operating
The take-off run
6 - Drag is in the direction of - and lift is perpendicular to the:
7 - What is the purpose of an auto-slat system?
Provide automatically slat IN selection after take-off
Extend automatically when a certain value of angle of attack is exceeded
Assist the ailerons during rolling
Ensures that the slats are always extended when the ground/flight system is in the 'ground' position
8 - The angle between the aeroplane longitudinal axis and the chord line is the:
Angle of incidence
Climb path angle
Angle of attack
Glide path angle
9 - An aeroplane has a stall speed of 78 KCAS at its gross weight of 6850 lbs. What is the stall speed when the weight is 5000 lbs?
10 - Which of the following aeroplane parts affect induced drag most?
Wing root junction
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