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767-300ER.xml
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767-300ER.xml
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<?xml version="1.0" encoding="UTF-8" ?>
<!--
Boeing 767-300ER with GE CF6-80C2 engines for FlightGear YASim FDM
By John Williams (aka Tikibar)
-->
<airplane version="YASIM_VERSION_32" mass="198440">
<approach speed="155" aoa="2.2" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.5" />
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.5" />
<control-setting axis="/controls/flight/flaps" value="1.0" />
<control-setting axis="/controls/gear/gear-down" value="1.0" />
<solve-weight idx="0" weight="450" />
<solve-weight idx="1" weight="60000" />
</approach>
<cruise speed="505" alt="35000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.95" />
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.95" />
<control-setting axis="/controls/flight/flaps" value="0.0" />
<control-setting axis="/controls/gear/gear-down" value="0.0" />
<solve-weight idx="0" weight="450" />
<solve-weight idx="1" weight="60000" />
</cruise>
<cockpit x="24.0" y="0.0" z="-0.5" />
<!-- FUSELAGE -->
<!-- 3D Model nose cone at 26.466. Main gear at -0.360, -1.861 (mid -1.110) -->
<!-- Proper nose cone loc: 26.200, tail at -27.631 -->
<!-- z fuselage at -0.021, z global at -1.789 -->
<!-- Nose cone -->
<fuselage ax="26.200" ay="0.0" az="-1.066" bx="19.887" by="0.0" bz="-1.066" cx="1.076" cy="1.076" cz="1.0" width="5.030" taper="0.2" midpoint="1.0" />
<!-- Main fuselage -->
<fuselage ax="19.887" ay="0.0" az="-1.066" bx="-15.924" by="0.0" bz="-1.066" cx="1.076" cy="1.076" cz="1.0" width="5.030" taper="1.0" midpoint="1.0" />
<!-- Rear cone -->
<fuselage ax="-15.924" ay="0.0" az="-1.066" bx="-27.631" by="0.0" bz="0.134" cx="1.076" cy="1.076" cz="1.0" width="5.030" taper="0.25" midpoint="0.0" />
<!-- WINGS -->
<wing x="2.728" y="2.515" z="-3.581" length="24.946" chord="9.527" sweep="31.5" taper="0.240" dihedral="10.5" camber="0.1" incidence="2.0" twist="-3.0" idrag="1.12">
<stall aoa="8.0" width="3" peak="1.5" />
<flap0 start="0.01" end="0.72" lift="1.4" drag="1.3" />
<flap1 start="0.745" end="0.985" lift="1.6" drag="1.4" />
<slat start="0.02" end="0.985" aoa="3.0" drag="1.4" />
<spoiler start="0.11" end="0.7" lift="0.5" drag="1.6" />
<control-input axis="/controls/flight/flaps" control="FLAP0" />
<control-input axis="/controls/flight/flaps" control="SLAT" src0="0.0" src1="0.177" dst0="0.0" dst1="1.0" />
<control-input axis="/controls/flight/aileron-pos" control="FLAP1" split="true" />
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true" />
<control-input axis="/controls/flight/fdm-speedbrake" control="SPOILER" />
<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" />
<control-output control="SLAT" prop="/surface-positions/slats" />
<control-output control="SPOILER" prop="/surface-positions/speedbrake-pos-norm" />
<control-speed control="FLAP0" transition-time="64.0" />
<control-speed control="SLAT" transition-time="15.0" />
<control-speed control="SPOILER" transition-time="1.5" />
</wing>
<!-- ELEVATORS -->
<hstab x="-23.384" y="1.894" z="-1.066" length="8.183" chord="5.854" twist="0.0" taper="0.411" sweep="25.0" camber="0.1">
<stall aoa="20" width="7" peak="1.5" />
<flap0 start="0.0" end="1.0" lift="1.6" drag="1.4" />
<control-input axis="/controls/flight/elevator-pos" control="FLAP0" />
<control-input axis="/controls/flight/elevator-trim" control="FLAP0" />
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm" />
</hstab>
<!-- TAIL -->
<vstab x="-21.547" y="0.00" z="1.639" chord="8.264" length="9.777" taper="0.375" sweep="33.0" effectiveness="1.5">
<stall aoa="15" width="2" peak="1.3" />
<flap0 start="0.0" end="1.0" lift="1.4" drag="1.3" />
<control-input axis="/controls/flight/rudder-pos" 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>
<!-- ENGINES -->
<!-- Fuselage objects for nacelles -->
<fuselage ax="7.660" ay="7.920" az="-3.336" bx="5.099" by="7.920" bz="-3.321" cx="0.2" width="2.79" taper="0.9" midpoint="1.0" />
<fuselage ax="5.099" ay="7.920" az="-3.321" bx="2.636" by="7.920" bz="-3.352" cx="0.2" width="2.79" taper="0.65" midpoint="0.0" />
<fuselage ax="7.660" ay="-7.920" az="-3.336" bx="5.099" by="-7.920" bz="-3.321" cx="0.2" width="2.79" taper="0.9" midpoint="1.0" />
<fuselage ax="5.099" ay="-7.920" az="-3.321" bx="2.636" by="-7.920" bz="-3.352" cx="0.2" width="2.79" taper="0.65" midpoint="0.0" />
<!-- Actual engine definitions -->
<jet x="4.545" y="7.920" z="-3.336" mass="8900.0" thrust="62100.0" afterburner="0.0" rotate="0.0" n1-idle="44.0" n1-max="108.4" n2-idle="66.0" n2-max="98.0" tsfc="0.309" egt="810.0" exhaust-speed="1455.0" spool-time="3.0" epr-max="2.00">
<control-input axis="/controls/engines/engine[0]/throttle-lever" control="THROTTLE" />
<control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/surface-positions/left-reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="-22.038" y="6.48" z="-0.801" />
</jet>
<jet x="4.545" y="-7.920" z="-3.336" mass="8900.0" thrust="62100.0" afterburner="0.0" rotate="0.0" n1-idle="44.0" n1-max="108.4" n2-idle="66.0" n2-max="98.0" tsfc="0.309" egt="810.0" exhaust-speed="1455.0" spool-time="3.0" epr-max="2.00">
<control-input axis="/controls/engines/engine[1]/throttle-lever" control="THROTTLE" />
<control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/surface-positions/right-reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="-22.038" y="-6.48" z="-0.801" />
</jet>
<!-- LANDING GEARS -->
<!-- Pushback -->
<thruster x="21.650" y="0.0" z="-4.970" vx="1" vy="0" vz="0" thrust="24000">
<control-input axis="/sim/model/pushback/force" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1" />
</thruster>
<!-- Nose gear -->
<gear x="21.650" y="0.0" z="-5.47" compression="0.25" spring="0.7" damp="4.0" sfric="0.99">
<control-input axis="/controls/flight/rudder" control="STEER" square="true" />
<control-input axis="/controls/gear/gear-down" control="EXTEND" />
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm" />
<control-output control="STEER" prop="/gear/gear[0]/steering-norm" />
<control-speed control="EXTEND" transition-time="10.0" />
</gear>
<!-- Left main gear -->
<gear x="-1.110" y="4.650" z="-5.47" compression="0.6">
<control-input axis="/autopilot/autobrake/left-brake-output" 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="10.0" />
</gear>
<!-- Right main gear -->
<gear x="-1.110" y="-4.650" z="-5.47" compression="0.6">
<control-input axis="/autopilot/autobrake/right-brake-output" 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="10.0" />
</gear>
<!-- FUEL AND PAYLOAD -->
<!-- Total fuel capacity: 160,264 pounds -->
<!-- Left wing fuel tank -->
<tank x="0.260" y="7.92" z="-1.671" jet="true" capacity="40267" />
<!-- Right wing fuel tank -->
<tank x="0.260" y="-7.92" z="-1.671" jet="true" capacity="40267" />
<!-- Main fuel tank -->
<tank x="2.728" y="0.0" z="-3.171" jet="true" capacity="79730" />
<!-- -300 Center tank holds 29882 -->
<!-- Crew -->
<weight x="24" y="0.0" z="-0.5" mass-prop="/sim/weight[0]/weight-lb" size="0.0" solve-weight="0.0" idx="0" weight="600.0" />
<!-- PAX/Cargo -->
<weight x="2.055" y="0.0" z="-2.302" mass-prop="/sim/weight[1]/weight-lb" />
<!-- Ballast to adjust center of gravity -->
<ballast x="24.0" y="0.0" z="-2.116" mass="47500" />
<!--ballast x="-10.0" y="0.0" z="1.0" mass="700" /-->
</airplane>