<!-- 727-230 yasim 



  wingspan     : 32.92 m

  lenght       : 46.69 m  

  height       :  10.36 m  

  Empty mass   : 45360 kg 

  Cruise speed : 965 km/h 

  

-->



<airplane mass="90106">



  <!-- Approach configuration -->

  <approach speed="100" aoa="8" fuel="0.7">

    <control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>

    <control-setting axis="/controls/engines/engine[1]/throttle" value="0.5"/>

    <control-setting axis="/controls/engines/engine[2]/throttle" value="0.5"/>

    <control-setting axis="/controls/flight/flaps" value="1.0"/>

    <control-setting axis="/surface-positions/flap-pos-norm" value="1.0"/>

    <control-setting axis="/controls/gear/gear-down" value="1"/>

  </approach>



  <!-- Cruise configuration -->

  <cruise speed="536" alt="36000" fuel="0.7">

    <control-setting axis="/controls/engines/engine[0]/throttle" value="0.75"/>

    <control-setting axis="/controls/engines/engine[1]/throttle" value="0.75"/>

       <control-setting axis="/controls/engines/engine[2]/throttle" value="0.75"/>

    <control-setting axis="/controls/flight/flaps" value="0.0"/>

    <control-setting axis="/controls/gear/gear-down" value="0"/>

  </cruise>



  <cockpit x="16.598" y="0.384" z="0.494"/>



  <fuselage ax="20.097" ay="0" az="-0.86" bx="-14.819" by="0" bz="0.824" width="3.76" taper="0.0" midpoint="1.0"/>



  <wing x="2.084" y="2.098" z="-0.6806"

        chord="7.7"

        length="16.254"

        taper=".47"

        sweep="32"

        dihedral="3"

        camber="0.00"

	incidence="3.0"

	twist="-2.0"

	effectiveness="2.0">

        <stall aoa="15" width="8" peak="1.5"/>

        <flap0 start="0" end=".56" lift="1.6" drag="1.2"/>

        <flap1 start=".64" end=".88" lift="1.6" drag="1.1"/>

        <slat start="0" end="1" aoa="2"  drag="1.2"/>

        <spoiler start="0.2" end="0.6" lift="0.3" drag="3.0"/>



        <control-input axis="/controls/flight/speedbrake" control="SPOILER"/>

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

        <control-input axis="/surface-positions/flap-pos-norm" control="SLAT"/>

        <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>

        <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>



        <control-output control="SPOILER" prop="/surface-positions/speedbrake-pos-norm"/>  

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

        <control-output control="FLAP0" prop="/surface-positions/slats"/>

        <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"/>



        <control-speed control="FLAP0" transition-time="60"/>

        <control-speed control="SPOILER" transition-time="1"/>

  </wing>



  <hstab x="-18.738" y="0" z="6.014"

         chord="4.8" 

         length="5.822" 

         taper=".46"

         sweep="33" 

	  camber="-0.1"

         dihedral="0"

	 incidence="-3"

	 effectiveness="2.5">

         <stall aoa="10" width="4" peak="1.5"/>

         <flap0 start="0" end="1" lift="1.5" drag="1.1"/>



         <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>



  <vstab x="-13.187" y="0.00" z="1.9" 

         chord="5.5" 

         length="7.3" 

         taper="0.30"

         sweep="33"

	 incidence="0"

	 effectiveness="2.5">>

         <stall aoa="16" width="2" peak="1.5"/>

         <flap0 start="0" end="1" lift="1.6" drag="1.1"/>



         <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>

 <mstab x="-7.5" y="1.3" z="0.691" length="1.0" chord="4.0" incidence="-2.0"></mstab>

    



  <!-- 3 x Rolls Royce's AVON 310R -->

  <jet x="-6.600" y="2.860"  z="0.685"

       mass="2990"

       thrust="17390"

       tsfc="0.65"

       epr="5.66">

       <actionpt x="-10.791" y="2.860"  z="0.685"/>

       <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>

  </jet>



  <jet x="-6.600" y="-2.860"  z="0.685"

       mass="2990"

       thrust="17390"

       tsfc="0.65"

       epr="5.66">

       <actionpt x="-10.791" y="-2.860"  z="0.685"/>

       <control-input axis="/controls/engines/engine[2]/throttle" control="THROTTLE"/>

  </jet>

  

  <jet x="-11.997" y="0"  z="0.412"

       mass="2990"

       thrust="17390"

       tsfc="0.65"

       epr="5.66">

       <actionpt x="-14.820" y="0"  z="0.412"/>

       <control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>

  </jet>



  <!-- nose -->

  <gear x="19.246"  y="0.00" z="-2.7"

        compression="0.50" 

        spring="0.5" 

        damp="4">

        <control-input axis="/controls/flight/rudder" control="STEER" square="true"/>

        <control-input axis="/controls/gear/gear-down" control="EXTEND"/>

       <control-output control="STEER" prop="/gear/gear[0]/steering-norm"/>



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



        <control-speed control="EXTEND" transition-time="7"/>

	<control-speed control="STEER" transition-time="0.5"/>

  </gear>



  <gear x="-0.434" y="2.914" z="-3.184" 

        compression="0.6" 

        spring="0.9"

	damp="4">>

        <control-input axis="/controls/gear/brake-left" control="BRAKE"/>

        <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>

        <control-input axis="/controls/gear/gear-down" control="EXTEND"/>



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



        <control-speed control="EXTEND" transition-time="7"/>

  </gear>



  <gear x="-0.434" y="-2.914" z="-3.184" 

        compression="0.6" 

        spring="0.9"

	damp="4">>

        <control-input axis="/controls/gear/brake-right" control="BRAKE"/>

        <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>

        <control-input axis="/controls/gear/gear-down" control="EXTEND"/>



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



        <control-speed control="EXTEND" transition-time="7"/>

  </gear>

  

  

<!--tank-->

  <tank x="6" y="0" z="0.2" jet="true" capacity="22212"/>

  

    <ballast x="8.5" y="0" z="0.2" mass="9000"/>

    

    <weight x="4.5" y="0" z="0.2" mass-prop="/sim/weight[0]/weight-lb"/>

    <weight x="17.5" y="0" z="0.4" mass-prop="/sim/weight[1]/weight-lb"/>

   

<!--idea by Gijs- Thanks!-->   

<thruster x="19.246"  y="0.00" z="-2.7" vx="1" vy="0" vz="0" thrust="7000">

  <control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE" 

  src0="-1" src1="1" dst0="-1" dst1="1"/>

  </thruster>

  





</airplane>

