All other factors of importance remaining constant when speed is increased ? Obtaining > radio

exemple question 5


To put in a forward motion an unmanned multi rotor aircraft ?

exemple question 6
To put in a forward motion an unmanned multi rotor aircraft Speed of rotation of front rotors must be reduced.


to yaw to the left or to the right an unmanned multi rotor aircraft ?

exemple question 7
To yaw to left or to right an unmanned multi rotor aircraft Engines located on same axis must turn faster.


exemple question 8
To generate a roll to left on an unmanned multi rotor aircraft Engines located on left must be reduced.


exemple question 9
To generate a roll to right on an unmanned multi rotor aircraft Engines located on right must be reduced.


exemple question 10
In hovering flight with an unmanned multi rotor aircraft All engines must spin at same speed.


exemple question 11
For an unmanned multi rotor aircraft flight stability Provided reverting direction rotation of propellers.


8
As a multi rotor or a 'rotary wing' unmanned aircraft accelerates its attitude becomes Provided reverting direction rotation of propellers.


9
The movement of an unmanned aircraft about its lateral axis known as Provided reverting direction rotation of propellers.


10
The movement of an unmanned aircraft about its normal vertical axis known as Provided reverting direction rotation of propellers.


11
Rolling the rotation of aircraft about its Provided reverting direction rotation of propellers.


12
For an unmanned aircraft manoeuvrability Usually depends on its payload distribution. Too much stability will affect manoeuvrability if positioning of a camera or any load carried not correctly done manoeuvrability will be affected.


13
The statement that defines authorized maximum take off mass mtom Maximum take off mass authorized the manufacturer of an aircraft at take off. Too much stability will affect manoeuvrability if positioning of a camera or any load carried not correctly done manoeuvrability will be affected.


14
When lateral distance limitations do not apply no pilot shall operate a small remotely piloted aircraft at a ground speed of more than There no restriction on speed this level of operations. Too much stability will affect manoeuvrability if positioning of a camera or any load carried not correctly done manoeuvrability will be affected.


15
The risk of losing visual line of sight of your unmanned aircraft increased when you are operating There no restriction on speed this level of operations. Too much stability will affect manoeuvrability if positioning of a camera or any load carried not correctly done manoeuvrability will be affected.


16
No pilot shall transfer control of an rpa from one control station to another control station in flight unless There a procedure in place to mitigate risk of loss of control. Too much stability will affect manoeuvrability if positioning of a camera or any load carried not correctly done manoeuvrability will be affected.


17
Altitude defined as vertical distance separating an aircraft from There a procedure in place to mitigate risk of loss of control. Altitude = vertical distance separating an aircraft from mean sea level height = vertical distance separating an aircraft from ground.


18
Height defined as vertical distance separating an aircraft from There a procedure in place to mitigate risk of loss of control. Height = vertical distance separating an aircraft from ground altitude = vertical distance separating an aircraft from mean sea level.


19
Complete maintenance of an unmanned aircraft must be performed According to manufacturer's recommendation. Height = vertical distance separating an aircraft from ground altitude = vertical distance separating an aircraft from mean sea level.


20
Turbulence windshear icing lightning and heavy precipitation are associated with cumulonimbus clouds which of following statements true All of hazards can be avoided not flying in vicinity of cloud. Height = vertical distance separating an aircraft from ground altitude = vertical distance separating an aircraft from mean sea level.



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