<?xml version="1.0" encoding="ISO-8859-1"?>

<!-- Bell Boeing V22 Osprey :    2007 Maik JUSTUS
                    Updated :    2010 Oliver Thurau
                    Updated :    2014 Emmanuel BARANGER
                    Updated : 03/2022 Emmanuel BARANGER
                    Updated : 05/2024 Emmanuel BARANGER

     sources            : https://www.wikiwand.com/en/Bell_Boeing_V-22_Osprey

     wingspan           :  45 ft 10   in ( 13.97  m )
     length             :  57 ft  4   in ( 17.48  m )
     Width              :  84 ft  6.8 in ( 25.776 m ) including rotors
     Width folded       :  18 ft  5   in (  5.61  m )
     Height             :  22 ft  1   in (  6.73  m ) engine nacelles vertical
     Height folded      :  18 ft  1   in (  5.51  m )
     max speed          :   566 km/h (   306 kt     )
     Empty weight       : 31818 lb   ( 14432 kg     )
     Max takeoff weight : 60500 lb   ( 27442 kg     )
     engine             : 2 Rolls-Royce T406-AD-400 turboprop/turboshaft engines ( 6150 hp ) each maximum at 15000 rpm at sea level
     fuel tank          : 250 gal (946 L) internal; up to 3 - 150 gal (568 L) external drop tanks
     Maximum speed      :   275 kn   (   509 km/h   )
     Stall speed        :   110 kn   (   200 km/h   )
-->
<airplane mass="31818" version="YASIM_VERSION_CURRENT" mtow-lbs="60500">

  <approach speed="85" aoa="6">
    <control-setting axis="/sim/model/v22/solver_throttle" value="0.2"/>
    <control-setting axis="/sim/model/v22/tilt"            value="90"/>
  </approach>

  <cruise speed="275" alt="15000">
    <control-setting axis="/sim/model/v22/solver_throttle" value="1"/>
    <control-setting axis="/sim/model/v22/tilt"            value="90"/>
  </cruise>

  <cockpit x="5.820" y="-0.570" z="-0.900"/>

  <!-- main fuselage front-->
  <fuselage ax=" 8.1" ay=" 0.00" az="-1.90" bx=" 5.80" by=" 0.00" bz="-1.40" width="2.20" taper="0.25" midpoint="1.0" cx="0.150" cy="0.15" cz="0.35" idrag="0"/>
  <!-- main fuselage center -->
  <fuselage ax=" 6.0" ay=" 0.00" az="-1.40" bx="-2.50" by=" 0.00" bz="-1.40" width="2.30" taper="0.95" midpoint="0.5" cx="0.350" cy="1.60" cz="0.35" idrag="0"/>

  <!-- top fuselage -->
  <fuselage ax=" 1.0" ay=" 0.00" az="-0.80" bx="-2.50" by=" 0.00" bz="-0.80" width="2.30" taper="0.40" midpoint="0.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
  <fuselage ax=" 3.0" ay=" 0.00" az="-0.80" bx=" 1.00" by=" 0.00" bz="-0.80" width="2.30" taper="1.00" midpoint="0.5" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
  <fuselage ax=" 4.0" ay=" 0.00" az="-0.80" bx=" 3.00" by=" 0.00" bz="-0.80" width="2.30" taper="0.40" midpoint="1.0" cx="0.150" cy="0.15" cz="0.35" idrag="0"/>

  <!-- top fuselage right wingbase-->
  <fuselage ax=" 3.2" ay="-0.20" az=" 0.00" bx=" 2.20" by="-0.70" bz=" 0.00" width="0.50" taper="0.40" midpoint="1.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
  <fuselage ax=" 2.2" ay="-0.70" az=" 0.00" bx=" 0.00" by="-0.70" bz=" 0.00" width="0.50" taper="1.00" midpoint="0.5" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
  <fuselage ax=" 0.0" ay="-0.70" az=" 0.00" bx="-1.20" by="-0.20" bz="-0.20" width="0.50" taper="0.40" midpoint="0.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>

  <fuselage ax=" 3.2" ay="-0.50" az=" 0.00" bx=" 2.20" by="-1.00" bz=" 0.00" width="0.50" taper="0.40" midpoint="1.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
  <fuselage ax=" 2.2" ay="-1.00" az=" 0.00" bx=" 0.00" by="-1.00" bz=" 0.00" width="0.50" taper="1.00" midpoint="0.5" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
  <fuselage ax=" 0.0" ay="-1.00" az=" 0.00" bx="-1.20" by="-0.40" bz="-0.20" width="0.50" taper="0.40" midpoint="0.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>

  <!-- top fuselage left wingbase-->
  <fuselage ax=" 3.2" ay=" 0.20" az=" 0.00" bx=" 2.20" by=" 0.70" bz=" 0.00" width="0.50" taper="0.40" midpoint="1.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
  <fuselage ax=" 2.2" ay=" 0.70" az=" 0.00" bx=" 0.00" by=" 0.70" bz=" 0.00" width="0.50" taper="1.00" midpoint="0.5" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
  <fuselage ax=" 0.0" ay=" 0.70" az=" 0.00" bx="-1.20" by=" 0.20" bz="-0.20" width="0.50" taper="0.40" midpoint="0.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>

  <fuselage ax=" 3.2" ay=" 0.50" az=" 0.00" bx=" 2.20" by=" 1.00" bz=" 0.00" width="0.50" taper="0.40" midpoint="1.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
  <fuselage ax=" 2.2" ay=" 1.00" az=" 0.00" bx=" 0.00" by=" 1.00" bz=" 0.00" width="0.50" taper="1.00" midpoint="0.5" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
  <fuselage ax=" 0.0" ay=" 1.00" az=" 0.00" bx="-1.20" by=" 0.40" bz="-0.20" width="0.50" taper="0.40" midpoint="0.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>

  <!-- side fuselage right-->
  <fuselage ax=" 3.0" ay="-0.75" az="-2.10" bx=" 1.00" by="-1.75" bz="-2.10" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>

  <fuselage ax=" 1.2" ay="-1.70" az="-2.10" bx="-1.50" by="-1.70" bz="-2.10" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
  <fuselage ax=" 1.7" ay="-1.00" az="-2.10" bx="-1.50" by="-1.00" bz="-2.10" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>

  <fuselage ax="-1.3" ay="-1.70" az="-2.10" bx="-3.80" by="-0.70" bz="-1.60" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>

  <!-- side fuselage left-->
  <fuselage ax=" 3.0" ay=" 0.75" az="-2.10" bx=" 1.00" by=" 1.75" bz="-2.10" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>

  <fuselage ax=" 1.2" ay=" 1.70" az="-2.10" bx="-1.50" by=" 1.70" bz="-2.10" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
  <fuselage ax=" 1.7" ay=" 1.00" az="-2.10" bx="-1.50" by=" 1.00" bz="-2.10" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>

  <fuselage ax="-1.3" ay=" 1.70" az="-2.10" bx="-3.80" by=" 0.70" bz="-1.60" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>

  <!-- back fuselage -->
  <fuselage ax="-2.3" ay=" 0.00" az="-1.40" bx="-5.00" by="-0.45" bz="-1.03" width="2.20" taper="0.55" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
  <fuselage ax="-2.3" ay=" 0.00" az="-1.40" bx="-5.00" by=" 0.00" bz="-1.03" width="2.20" taper="0.55" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
  <fuselage ax="-2.3" ay=" 0.00" az="-1.40" bx="-5.00" by=" 0.45" bz="-1.03" width="2.20" taper="0.55" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>

  <fuselage ax="-4.8" ay="-0.45" az="-1.05" bx="-6.50" by="-0.75" bz="-0.50" width="1.30" taper="0.35" midpoint="0.0" cx="0.015" cy="2.00" cz="0.35" idrag="0"/>
  <fuselage ax="-4.8" ay=" 0.00" az="-1.05" bx="-6.50" by=" 0.00" bz="-0.50" width="1.30" taper="0.35" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
  <fuselage ax="-4.8" ay=" 0.45" az="-1.05" bx="-6.50" by=" 0.75" bz="-0.50" width="1.30" taper="0.35" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>

  <fuselage ax="-6.4" ay="-0.75" az="-0.51" bx="-7.70" by="-0.75" bz="-0.40" width="0.45" taper="0.35" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
  <fuselage ax="-6.4" ay=" 0.00" az="-0.51" bx="-7.70" by=" 0.00" bz="-0.40" width="0.45" taper="0.35" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
  <fuselage ax="-6.4" ay=" 0.75" az="-0.51" bx="-7.70" by=" 0.75" bz="-0.40" width="0.45" taper="0.35" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>

  <!-- main wing -->
  <wing x="0.90" y="0.4" z="0.30"
        chord="2.65"
        chord_real="2.65"
        taper="1"
        length_real="6.1"
        length="6.1"
        dihedral="1.8"
        incidence="3.5"
        camber="0.2"
        sweep="-8">
        <stall width="8"   aoa="35"   peak="1.5"/>
        <flap0  drag="1.6" end="0.5"  lift="2" start="0.02"/>
        <flap1  drag="1.6" end="0.97" lift="2" start="0.5"/>

        <control-input  control="FLAP0" axis="/sim/model/v22/wing/flap"/>
        <control-input  control="FLAP1" axis="/sim/model/v22/wing/flap"/>
        <control-input  control="FLAP1" axis="sim/model/v22/wing/aileron" split="true"/>

        <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
        <control-output control="FLAP1" prop="/surface-positions/left-aileron-pos-norm"  side="left"/>
        <control-output control="FLAP1" prop="/surface-positions/right-aileron-pos-norm" side="right"/>
  </wing>

  <mstab x="-8.40" y="0.0" z="-0.45"
         taper="1"
         length="2.50"
         chord="2.30"
         sweep="0"
         incidence="-0.5">
         <stall  aoa="16" width="4" peak="1.5"/>
         <flap0 drag="1.2"  end="1" lift="1.9" start="0"/>

         <control-input  control="FLAP0" axis="/sim/model/v22/wing/elevator"/>
         <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
  </mstab>

  <!-- Vertical wing - rudder -->
  <vstab x="-7.90" y="2.52" z="-1.39"
         taper="0.4"
         length="3.20"
         chord="2.72"
         sweep="15"
         incidence="0">
         <stall aoa="16" width="4" peak="1.5"/>
         <flap0 drag="1.2" end="1" lift="1.4" start="0.4"/>

         <control-input  control="FLAP0" axis="/sim/model/v22/wing/rudder"         invert="true"/>
         <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm" min="1" max="-1"/>
  </vstab>

  <vstab x="-7.90" y="-2.52" z="-1.39"
         taper="0.4"
         length="3.20"
         chord="2.72"
         sweep="15"
         incidence="0">
         <stall aoa="16" width="4" peak="1.5"/>
         <flap0 drag="1.2" end="1" lift="1.4" start="0.4"/>

         <control-input  control="FLAP0" axis="/sim/model/v22/wing/rudder"         invert="true"/>
         <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm" min="1" max="-1"/>
  </vstab>

  <!-- main == right rotor (name=main for mp-protocol) -->
  <!-- tail ==  left rotor (name=tail for mp-protocol) -->
  <rotor name="main"
         x="1.57" y="-7.041" z="2.550"
         nx="0" ny="0" nz="1"
         fx="1" fy="0" fz="0"
         ccw="1"
         maxcollective="180" mincollective="-180"
         mincyclicele="-90" maxcyclicele="90"
         mincyclicail="-90" maxcyclicail="90"
         mintiltpitch="-180" maxtiltpitch="180"
         tiltcenterx="1.75" tiltcentery="-2.1" tiltcenterz="0.30"
         mintiltroll="-90" maxtiltroll="90"
         diameter="11.58"
         numblades="3"
         weightperblade="675"
         twist="-47.5"
         chord="0.81"
         rpm="412"
         relbladecenter="0.5"
         dynamic="1"
         rellenflaphinge="0.13"
         delta3="-0.26"
         delta="0.25"
         pitch-a="10" pitch-b="15"
         flapmin="-15" flapmax="15"
         flap0="-2"
         flap0factor="0"
         notorque="0"
         dragfactor="0.30"
         translift-ve="20"
         translift-maxfactor="1.3"
         ground-effect-constant="0.1"
         taper="1"
         number-of-segments="8"
         number-of-parts="8"
         rel-len-where-incidence-is-measured="0.6"
         rel-len-blade-start="0.16"
         airfoil-lift-coefficient="3.15"
         airfoil-drag-coefficient0="0.38"
         airfoil-drag-coefficient1="5.5"
         incidence-stall-zero-speed="65"
         incidence-stall-half-sonic-speed="55.0"
         lift-factor-stall="0.45"
         stall-change-over="11"
         drag-factor-stall="4.0"
         cyclic-factor="0.8"
         rotor-correction-factor="1.7"
         balance="1"
         downwashfactor="0.3"
         phi0="95">
         <control-input control="TILTPITCH"  axis="/sim/model/v22/tilt"                   src0="-180" src1="180" dst0=" 1" dst1="-1"/>
         <control-input control="CYCLICELE"  axis="/sim/model/v22/rotor/right/elevator"   src0=" -90" src1=" 90" dst0="-1" dst1=" 1"/>
         <control-input control="COLLECTIVE" axis="/sim/model/v22/rotor/right/collective" src0="-180" src1="180" dst0="-1" dst1=" 1"/>
  </rotor>

  <rotor name="tail"
         x="1.57" y="7.041" z="2.550"
         nx="0" ny="0" nz="1"
         fx="1" fy="0" fz="0"
         ccw="0"
         maxcollective="180" mincollective="-180"
         mincyclicele="-90" maxcyclicele="90"
         mincyclicail="-90" maxcyclicail="90"
         mintiltpitch="-180" maxtiltpitch="180"
         tiltcenterx="1.75" tiltcentery="2.1" tiltcenterz="0.30"
         mintiltroll="-90" maxtiltroll="90"
         diameter="11.58"
         numblades="3"
         weightperblade="675"
         twist="-47.5"
         chord="0.81"
         rpm="412"
         relbladecenter="0.5"
         dynamic="1"
         rellenflaphinge="0.13"
         delta3="-0.26"
         delta="0.25"
         pitch-a="10" pitch-b="15"
         flapmin="-15" flapmax="15"
         flap0="-2"
         flap0factor="0"
         notorque="0"
         dragfactor="0.30"
         translift-ve="20"
         translift-maxfactor="1.3"
         ground-effect-constant="0.1"
         taper="1"
         number-of-segments="8"
         number-of-parts="8"
         rel-len-where-incidence-is-measured="0.6"
         rel-len-blade-start="0.16"
         airfoil-lift-coefficient="3.15"
         airfoil-drag-coefficient0="0.38"
         airfoil-drag-coefficient1="5.5"
         incidence-stall-zero-speed="65"
         incidence-stall-half-sonic-speed="55"
         lift-factor-stall="0.45"
         stall-change-over="11"
         drag-factor-stall="4.0"
         cyclic-factor="0.8"
         rotor-correction-factor="1.7"
         balance="1"
         downwashfactor="0.3"
         phi0="95">
         <control-input control="TILTPITCH"  axis="/sim/model/v22/tilt"                  src0="-180" src1="180" dst0=" 1" dst1="-1"/>
         <control-input control="CYCLICELE"  axis="/sim/model/v22/rotor/left/elevator"   src0=" -90" src1=" 90" dst0="-1" dst1=" 1"/>
         <control-input control="COLLECTIVE" axis="/sim/model/v22/rotor/left/collective" src0="-180" src1="180" dst0="-1" dst1=" 1"/>
  </rotor>

  <rotorgear max-power-engine-real="9172"
             max-power-engine="131720"
             max-power-rotor-brake="4850"
             rotorgear-friction="30"
             engine-prop-factor="0.015"
             engine-accel-limit="4"
             yasimdragfactor="270"
             yasimliftfactor="28">
             <control-input control="ROTORGEARENGINEON"       axis="/controls/engines/engine[0]/magnetos"/>
             <control-input control="ROTORBRAKE"              axis="/controls/rotor/brake"        src0="0" src1="1" dst0="0" dst1="1"/>
             <control-input control="ROTORRELTARGET"          axis="/controls/rotor/reltarget"    src0="0" src1="2" dst0="0" dst1="2"/>
             <control-input control="ROTORENGINEMAXRELTORQUE" axis="/controls/rotor/maxreltorque" src0="0" src1="2" dst0="0" dst1="2"/>
  </rotorgear>

  <!-- front gear -->
  <gear x="7.428" y="0" z="-2.949"
        compression="0.2"
        spring="0.65"
        damp="0.4"
        stiction="1">
        <control-input  control="BRAKE"  axis="/controls/gear/brake-right"   split="true"/>
        <control-input  control="BRAKE"  axis="/controls/gear/brake-left"    split="true"/>
        <control-input  control="BRAKE"  axis="/controls/gear/brake-parking" split="true"/>
        <control-input  control="STEER"  axis="/controls/flight/rudder"      square="true" src0="-1.0" src1="1.0" dst0="-0.8" dst1="0.8"/>
        <control-input  control="EXTEND" axis="/controls/gear/gear-down"/>

        <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>

        <control-speed  control="EXTEND" transition-time="5"/>
  </gear>

  <!-- left gear -->
  <gear x="0.467" y="2.101" z="-2.949"
        compression="0.2"
        spring="0.65"
        damp="0.4"
        stiction="1">
        <control-input  control="BRAKE"  axis="/controls/gear/brake-left"    split="true"/>
        <control-input  control="BRAKE"  axis="/controls/gear/brake-parking" split="true"/>
        <control-input  control="EXTEND" axis="/controls/gear/gear-down"/>

        <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>

        <control-speed  control="EXTEND" transition-time="5.1"/>
  </gear>

  <!-- right gear -->
  <gear x="0.467" y="-2.101" z="-2.949"
        compression="0.2"
        spring="0.65"
        damp="0.4"
        stiction="1">
        <control-input  control="BRAKE"  axis="/controls/gear/brake-right"   split="true"/>
        <control-input  control="BRAKE"  axis="/controls/gear/brake-parking" split="true"/>
        <control-input  control="EXTEND" axis="/controls/gear/gear-down"/>

        <control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>

        <control-speed  control="EXTEND" transition-time="5.2"/>
  </gear>

  <!-- CRASH LANDING FX - left skid -->
  <gear x=" 6.00" y=" 1.000" z="-2.50" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
  <gear x="-2.40" y=" 1.000" z="-2.50" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>

  <!-- CRASH LANDING FX - left skid -->
  <gear x=" 6.00" y="-1.000" z="-2.50" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
  <gear x="-2.40" y="-1.000" z="-2.50" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>

  <!-- CRASH FX - right ruder skid -->
  <gear x="-7.50" y=" 2.500" z="-1.38" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
  <gear x="-9.00" y=" 2.500" z="-1.32" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>

  <!-- CRASH FX - left ruder skid -->
  <gear x="-7.50" y="-2.500" z="-1.38" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
  <gear x="-9.00" y="-2.500" z="-1.32" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>

  <!-- CRASH FX - right engine skid ax="1.57" ay="7.041" az="2.550" -->
  <gear x=" 2.52" y="-7.441" z="-1.87" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
  <gear x=" 1.40" y="-7.241" z="-1.87" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>

  <!-- CRASH FX - left engine skid ax="1.57" ay="7.041" az="2.550" -->
  <gear x=" 2.52" y="+7.441" z="-1.87" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
  <gear x=" 1.40" y="+7.241" z="-1.87" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>

  <!-- Forward sponson Fuel tank -->
  <tank x="1.70" y=" 1.4" z="-2.10" capacity="75"/>
  <tank x="1.70" y="-1.4" z="-2.10" capacity="75"/>

  <!-- Wing feeder tank -->
  <tank x="1.90" y=" 5.8" z=" 0.30" capacity="75"/>
  <tank x="1.90" y="-5.8" z=" 0.30" capacity="75"/>

  <!-- Wing aux tank -->
  <tank x="1.90" y=" 3.6" z=" 0.10" capacity="75"/>
  <tank x="1.90" y="-3.6" z=" 0.10" capacity="75"/>

  <!-- pilot -->
  <weight x="6.0" y=" 0.6" z="-1.3" mass-prop="/sim/weight[0]/weight-lb"/>
  <!-- co-pilot -->
  <weight x="6.0" y="-0.6" z="-1.3" mass-prop="/sim/weight[1]/weight-lb"/>
  <!-- right passenger -->
  <weight x="4.2" y=" 0.6" z="-1.5" mass-prop="/sim/weight[2]/weight-lb"/>
  <!-- left passenger -->
  <weight x="4.2" y="-0.6" z="-1.5" mass-prop="/sim/weight[3]/weight-lb"/>
  <!-- load -->
  <weight x="0.2" y=" 0.0" z="-1.9" mass-prop="/sim/weight[4]/weight-lb"/>

  <!-- pushback -->
  <thruster x="7.428" y="0" z="-2.949"
            vx="1" vy="0" vz="0"
            thrust="5200">
            <control-input control="THROTTLE" axis="/sim/model/pushback/target-speed-fps" src0="-1" src1="1" dst0="-1" dst1="1"/>
  </thruster>

  <hitch name="aerotow"
         x="-3.1" y="0" z="-2.525"
         force-is-calculated-by-other="0">
         <tow length="30"
              weight-per-meter="0.035"
              elastic-constant="9000"
              break-force="80000"
              mp-auto-connect-period="0"/>
         <winch max-tow-length="100"
                min-tow-length="30"
                initial-tow-length="30"/>
         <control-input control="FINDAITOW" axis="/controls/aerotow/find-aircraft"/>
  </hitch>

  <!-- Mass distribution -->
  <ballast x=" 8" y=" 0" z="-2" mass="9110"/>

</airplane>
