fgdata/Aircraft-yasim/pa28-161.xml

<airplane mass="1480">

<!-- Approach configuration -->
<approach speed="43" aoa="17">
  <control-setting axis="/controls/throttle[0]" value="0.3"/>
  <control-setting axis="/controls/mixture[0]" value="1.0"/>
  <control-setting axis="/controls/flaps" value="1.0"/>
</approach>

<!-- Cruise configuration -->
<cruise speed="122" alt="0">
  <control-setting axis="/controls/throttle[0]" value="1.0"/>
  <control-setting axis="/controls/mixture[0]" value="1.0"/>
  <control-setting axis="/controls/flaps" value="0.0"/>
</cruise>

<cockpit x="-2.5" y=".33" z="0.6"/>

<fuselage ax="0.5" ay="0" az="0" bx="-7.75" by="0" bz="0"
          width="1.5" taper="0.2" midpoint="0.3"/>

<wing x="-2.75" y="0.6" z="-0.75" taper="0.65"
      length="4.5" chord="1.65" sweep="0" dihedral="5" camber="0.1">
  <stall aoa="16" width="6" peak="1.5"/>
  <flap0 start="0" end="0.5" lift="1.3" drag="1.5"/>
  <flap1 start="0.5" end="1.0" lift="1.2" drag="1.2"/>
  <control-input axis="/controls/flaps" control="FLAP0"/>
  <control-input axis="/controls/aileron" control="FLAP1" split="true"/>
  <control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/>
  <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
  <control-output control="FLAP1" side="left"
		  prop="/surface-positions/left-aileron-pos-norm"/>
  <control-output control="FLAP1" side="right"
		  prop="/surface-positions/right-aileron-pos-norm"/>
</wing>

<hstab x="-6.5" y="0.00" z=".15" taper="1.0" effectiveness="2"
       length="1.9" chord="0.9" sweep="0">
  <stall aoa="18" width="4" peak="1.5"/>
  <flap0 start="0" end="1" lift="2.0" drag="1.2"/>
  <control-input axis="/controls/elevator" control="FLAP0"/>
  <control-input axis="/controls/elevator-trim" control="FLAP0"/>
  <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab>

<vstab x="-6.25" y="0" z=".3" taper=".5"
       length="1.2" chord="1.2" sweep="10">
  <stall aoa="16" width="4" peak="1.5"/>
  <flap0 start="0" end="1" lift="1.3" drag="1.1"/>
  <control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
  <control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/>
  <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
		  min="1" max="-1"/>
</vstab>

<propeller radius="1.0"
	   cruise-speed="125" cruise-rpm="2665"
           cruise-alt="8000" cruise-power="120"
           takeoff-power="140.8" takeoff-rpm="2200"
           eng-power="160" eng-rpm="2800"
           x="-1" y="0" z="0" mass="400" moment="8">
  <actionpt x="0" y="0" z="0"/>
  <control-input axis="/controls/throttle[0]" control="THROTTLE"/>
  <control-input axis="/controls/starter[0]" control="STARTER"/>
  <control-input axis="/controls/magnetos[0]" control="MAGNETOS"/>
  <control-input axis="/controls/mixture[0]" control="MIXTURE"/>
</propeller>

<gear x="-1" y="0" z="-1.3" compression=".05"> <!-- nose -->
  <control-input axis="/controls/rudder" control="STEER"
                 src0="-1.0" src1="1.0"
                 dst0="-0.1" dst1="0.1"/>
</gear>

<gear x="-2.8" y="1.5" z="-1.3" compression=".05"> <!-- left main -->
  <control-input axis="/controls/brakes[0]" control="BRAKE" split="true"/>
  <control-input axis="/controls/parking-brake" control="BRAKE" split="true"/>
</gear>

<gear x="-2.8" y="-1.5" z="-1.3" compression=".05"> <!-- left main -->
  <control-input axis="/controls/brakes[1]" control="BRAKE" split="true"/>
  <control-input axis="/controls/parking-brake" control="BRAKE" split="true"/>
</gear>

<tank x="-2.5" y="1.5" z="-0.25" capacity="144"/> 
<tank x="-2.5" y="-1.5" z="-0.25" capacity="144"/> 

<ballast x="-2.0" y="0" z="0" mass="400"/> <!-- cockpit -->

<weight x="-2.5" y=".33" z="0" mass-prop="/yasim/pa28/pilot-lb"/>
<weight x="-2.5" y="-.33" z="0" mass-prop="/yasim/pa28/copilot-lb"/>

</airplane>