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Students > equipment : Helicopter flight controls.the collective lever is so named because ?

Question 30-1 : It alters the pitch of all main rotor blades at the same time it allows to invert the pitch of all the main rotor blades it changes the pitch of the main and tail rotor blades at the same time it increases or decreases the rotational speed of the rotors

exemple 30 it alters the pitch of all main rotor blades at the same time.it alters the pitch of all main rotor blades at the same time.

Helicopter flight controls.to put into a forward flight motion a rpas helicopter ?

Question 30-2 : You have to tilt the main rotor plane of rotation ahead you have to tilt the main rotor plane of rotation backwards the tail rotor must generated a motion to the right the tail rotor must generated a motion to the left

exemple 34 you have to tilt the main rotor plane of rotation ahead.you have to tilt the main rotor plane of rotation ahead.

Helicopter flight controls.for a remotely piloted aircraft system rpas ?

Question 30-3 : Control the rotation of the airframe on the yaw axis increase available power for the main rotor while hovering allow lateral motions while hovering allow the control of the flight around the roll axis

exemple 38 control the rotation of the airframe on the yaw axis.control the rotation of the airframe on the yaw axis.

Flight controls.rolling is the rotation of the aeroplane about the ?

Question 30-4 : Longitudinal axis vertical axis lateral axis wing axis

exemple 42 longitudinal axis.longitudinal axis.

Flight controls.rotation about the lateral axis is called ?

Question 30-5 : Pitching yawing rolling slipping

exemple 46 pitching.pitching.

Flight controls.rotation around the longitudinal axis is called ?

Question 30-6 : Rolling yawing pitching slipping

exemple 50 rolling.rolling.

Flight controls.rotation around the normal vertical axis is called ?

Question 30-7 : Yawing rolling pitching slipping

exemple 54 yawing.yawing.

Design of the wing.aspect ratio of a wing is the ratio between ?

Question 30-8 : Wing span and mean chord line wing span and dihedral angle wing span and wing root chord wing root chord line and wing tip chord line


Design of the wing.leading edge is ?

Question 30-9 : The foremost edge of a wing the rear edge of a wing the underside of the wing the tip of a wing


Design of the wing.trailing edge is ?

Question 30-10 : The rear edge of a wing the underside of the wing the foremost edge of a wing the tip of a wing


Define the term 'wing cord' ?

Question 30-11 : The straight line between the leading edge and the trailing edge the straight line between the extrados and the lower wing surface the straight line between the leading edge is the upper wing surface the straight line between the trailing edge and the upper wing surface


Multi rotor aircraft dynamics.during a flight under gps stabilize mode your ?

Question 30-12 : I'm taking back manual flight control under attitude stabilized mode i stop the engines i let it do the system will automatically come back to the route i reset my remote control unit

exemple 74 i'm taking back manual flight control under attitude stabilized mode.i'm taking back manual flight control under attitude stabilized mode.

Multi rotor aircraft dynamics.as a multi rotor or a'helicopter' accelerates the ?

Question 30-13 : Nose down nose up level nose up or nose down depending on the kind of aircraft

exemple 78 nose down.nose down.

Multi rotor aircraft dynamics.for a remotely piloted aircraft system multi ?

Question 30-14 : Engines located on the same axis must turn faster engines located on the right must be reduced engines located on the left must be reduced engines located at the front must spin faster

exemple 82 engines located on the same axis must turn faster.engines located on the same axis must turn faster.

Multi rotor aircraft dynamics.for a remotely piloted aircraft system multi ?

Question 30-15 : Engines located on the right must be reduced engines located on the left must be reduced engines located at the front must spin faster engines located at the back must spin faster

exemple 86 engines located on the right must be reduced.engines located on the right must be reduced.


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434 Free Training Exam Other source study: Ulm theorique examen 30