<?xml version="1.0" encoding="UTF-8"?>

<!-- Farman III (19010-1912) LesterBoffo
     
     wingspan     : 10.50 m         (33.83 ft)
     length       : 12.67 m         (38.28 ft)
     Empty weight : 460 kg          (840 lb)
     Engine       : 1 x Gnome 50 cv 
     Speed        : 57 km/h         (35 kts)
-->
     
<airplane mass="840">

  <approach speed="24" aoa="5">
    <control-setting axis="/controls/engines/engine[0]/throttle" value="0.35"/>
    <control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
  </approach>
  
  <cruise speed="42" alt="0">
    <control-setting axis="/controls/engines/engine[0]/throttle" value="0.85"/>
    <control-setting axis="/controls/engines/engine[0]/mixture" value="0.99"/>
    <control-setting axis="/controls/flight/elevator-trim" value="0.1"/>
  </cruise>

  <cockpit x="2.092" y="0" z="0.630"/>

  <fuselage ax="-0.158" ay="-1.23" az="-0.159" bx="-5.0" by="-1.02" bz="-0.109" width="0.030" taper="1" midpoint="0.5"/>
<fuselage ax="-0.158" ay="1.23" az="-0.159" bx="-5.0" by="1.02" bz="-0.109" width="0.030" taper="1" midpoint="0.5"/>
<fuselage ax="-0.158" ay="-1.23" az="1.33" bx="-5.0" by="-1.02" bz="1.089" width="0.030" taper="1" midpoint="0.5"/>
<fuselage ax="-0.158" ay="1.23" az="1.33" bx="-5.0" by="1.02" bz="1.089" width="0.030" taper="1" midpoint="0.5"/>
<fuselage ax="1.11" ay="-1.23" az="1.37" bx="3.76" by="-1.23" bz="0.589" width="0.030" taper="1" midpoint="0.5"/>
<fuselage ax="1.11" ay="1.23" az="1.37" bx="3.76" by="1.23" bz="0.589" width="0.030" taper="1" midpoint="0.5"/>
<fuselage ax="1.11" ay="-1.23" az="-0.237" bx="3.76" by="-1.23" bz="0.589" width="0.030" taper="1" midpoint="0.5"/>
<fuselage ax="1.11" ay="1.23" az="-0.237" bx="3.76" by="1.23" bz="0.589" width="0.030" taper="1" midpoint="0.5"/>

  <wing x="0.30" y="0.000" z="1.409"
        chord="1.769" 
        length="4.67"
        incidence="1.0" 
        taper="1.0" 
        camber="0.09">
        effectiveness="1.4" 
        <stall aoa="11" width="3" peak="1.7"/>
        <flap0 start="0.70" end="1.0" lift="1.5" drag="1.4"/>

        <control-input axis="/controls/flight/aileron" control="FLAP0" split="true"/>
        <control-input axis="/controls/flight/aileron-trim" control="FLAP0" split="true"/>

        <control-output control="FLAP0" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
        <control-output control="FLAP0" side="right" prop="/surface-positions/right-aileron-pos-norm"/>
  </wing>

  <mstab x="0.30" y="0.000" z="-0.22" 
         chord="1.769" 
         length="4.76" 
         taper="1.0" 
         incidence="1.0"  
         camber="0.09">
         effectiveness="1.4"
         <stall aoa="11" width="3" peak="1.7"/>
  </mstab>

  <hstab x="-5.581" y="0.000" z="1.15" 
         chord="1.7" 
         length="1.29" 
         incidence="2.9" 
         taper="1.0" 
         camber="0.09">
         <stall aoa="16" width="4" peak="1.5"/>
         <flap0 start="0" end="1" lift="1.6" drag="1.2"/> 

         <control-input axis="/controls/flight/elevator" control="FLAP0"/>
         <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>

         <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
  </hstab>

  <mstab x="-5.581" y="0.000" z="-0.14" 
         chord="1.7" 
         length="1.29" 
         incidence="2.9" 
         taper="1.0" 
         camber="0.09">
         <stall aoa="16" width="4" peak="1.5"/>
  </mstab>

       <mstab x="3.681" y="0.000" z="0.354" 
         chord="0.902" 
         length="2.030" 
         incidence="0.0" 
         taper="1.0"
         camber="-0.015">
         <stall aoa="16" width="2.0" peak="1.0"/>
         <flap0 start="0" end="1" lift="1.55" drag="1.2"/> 

         <control-input axis="/controls/flight/elevator" control="FLAP0" invert="true"/>
         <control-input axis="/controls/flight/elevator-trim" control="FLAP0" invert="true"/>

         <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm" min="1.15" max="-1.12"/>
  </mstab>

  <vstab x="-6.291" y="1.07" z="0.36" 
         chord="0.94" 
         length="1.190" 
         taper="0.80">
         <stall aoa="14" width="4" peak="1.5"/>
         <flap0 start="0" end="1" lift="1.5" drag="1.12"/>

         <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
         <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>

         <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm" min="1" max="-1"/>
  </vstab>

  <vstab x="-6.291" y="-1.07" z="0.36" 
         chord="0.94" 
         length="1.190" 
         taper="0.80">
         <stall aoa="14" width="4" peak="1.5"/>
         <flap0 start="0" end="1" lift="1.5" drag="1.12"/>

         <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
         <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>

         <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm" min="1" max="-1"/>
 </vstab>

  <propeller  x="-0.63" 
	        y="0" 
	        z="0.0"
              radius="1.108"
	        cruise-speed="35"
	        cruise-rpm="1170"
              cruise-alt="1000" 
	        cruise-power="47"
              takeoff-power="50" 
	        takeoff-rpm="1200"
	        mass="135" 
	        moment="24">
           <actionpt x="-0.45" y="0" z="0.0"/>
             <piston-engine eng-rpm="1200"
                            eng-power="50"
                            displacement="488.5"
                            bore="4.3"
                            stroke="4.7" 
                            min-throttle="0.03"
                            compression="3.86"/>
           <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
           <control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
           <control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/>
           <control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
</propeller>

  

  <!-- leftgears -->
  <gear x="0.90" y="1.212" z="-1.649"
        compression="0.09">
        <control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
  </gear>

  <!-- rightgears -->
  <gear x="0.90" y="-1.212" z="-1.649"
        compression="0.09">
        <control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
  </gear>

<!-- tailwheel -->
  <gear x="-4.89" y="0" z="-0.665"
        compression="0.02">
  </gear>

  <!-- fueltank -->
  <tank x="0.39" y="0" z="0.213" capacity="162"/>

  <ballast x="4.0" y="0" z="-1.52" mass="200"/>

</airplane>
