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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: 3.8 2.5 6.0 4.4

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: Chord line Relative wind/airflow Longitudinal axis Horizon

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? 78 KCAS 91 KCAS 57 KCAS 67 KCAS

10 - Which of the following aeroplane parts affect induced drag most? Wing root junction Engine cowling Landing gear Wing tip

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