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g) Throttle Curve Setting „Throttle Curve“
In a proportional remote control unit the control stick and the cor-
responding servo maintain linear reactions (also see second fi-
gure from the top in image 40a). This means: Moving the control 
element from one side to the other results in the corresponding 
servo arm moving from one side to the other.
If the throttle/pitch control stick (or stick) on the transmitter is 
in the lowest position (L), the throttle flap must be almost fully
closed. 
If the control stick is then moved to the middle position (2), the 
throttle flap should be approx. 50% open.
If the control stick is in the uppermost position (H), the carburet-
tor should be fully open so that the motor can run at full power. 
The throttle curve thus corresponds to a straight line (see the 
adjacent sketch).
With the throttle curve setting, the shape of the throttle curve can be changed specifically in 5 points and the settings
can be saved. 
Setting the throttle curve:
•  Switch on the transmitter and call the function setting menu.
•  Move the cursor arrow to the menu item „Throttle Curve“ with
the two buttons „UP“ and „DOWN“.
•  Briefly push the button „OK“ to activate the menu item.
  The display shows the indications for the percentage setting 
values for the five points of the throttle curve (L, 1, 2, 3 and H),
the control curve chart and the flight condition „Normal“. (the
switch „SWB“ must be in the front position for this).
  The vertical dash in the chart marks the current position of the 
throttle control stick. 
 In the flight condition „normal“, the throttle curve should be set
for the combustion engine to run at the lowest speed when 
the control stick is in the idle position. In helicopter models, 
the centre part of the throttle curve may be a little flattened to
permit a fine hover flight.
•  Pushing the buttons „UP“ or „DOWN“ selects the percentage
input value for the bottom point of the throttle curve in the flight
condition „normal“. If the button „OK“ is pushed and held, the 
factory parameters are called.
Figure 41
Figure 42a