<airplane mass="400000"> <!-- Approach configuration --> <approach speed="136" aoa="7"> <control-setting axis="/controls/throttle[0]" value="0.2"/> <control-setting axis="/controls/throttle[1]" value="0.2"/> <control-setting axis="/controls/flaps" value="1.0"/> <control-setting axis="/controls/slats" value="1.0"/> <control-setting axis="/controls/gear-down" value="1"/> </approach> <!-- Cruise configuration --> <cruise speed="490" alt="36000"> <control-setting axis="/controls/throttle[0]" value="0.75"/> <control-setting axis="/controls/throttle[1]" value="0.75"/> <control-setting axis="/controls/flaps" value="0.0"/> <control-setting axis="/controls/gear-down" value="0"/> </cruise> <cockpit x="-5.42" y="1.81" z="15.06"/> <fuselage ax="0" ay="0" az="0" bx="-69.86" by="0.00" bz="2.41" width="6" taper="0.3" midpoint="0.2"/> <wing x="-26.50" y="3.01" z="-1.45" length="33.72" chord="13.25" sweep="33" taper=".27" dihedral="7" camber="0.15" incidence="-0.7"> <stall aoa="15" width="2" peak="1.5"/> <flap0 start="0" end=".56" lift="1.8" drag="1.2"/> <flap1 start=".64" end=".88" lift="1.3" drag="1.2"/> <slat start="0" end="1" aoa="2" drag="1.1"/> <spoiler start="0.2" end="0.6" lift="0.3" drag="2.0"/> <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-input axis="/controls/slats" control="SLAT"/> <control-input axis="/controls/spoilers" 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-speed control="FLAP0" transition-time="10"/> </wing> <hstab x="-62.63" y="1.81" z="1.81" chord="8.43" length="10.84" taper=".29" sweep="28" dihedral="7" camber="-0.1" effectiveness="1.5"> <stall aoa="15" width="2" peak="1.5"/> <flap0 start="0" end="1" lift="1.6" 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="-62.63" y="0.00" z="3.61" chord="12.04" length="12.04" taper="0.3" sweep="33"> <stall aoa="15" width="2" peak="1.5"/> <flap0 start="0" end="1" lift="1.2" drag="1.3"/> <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> <!-- The CF6 engines are rated at 60000 lbs thrust, flat rated to 33 --> <!-- degrees C. Corrected to YASim's standard atmosphere temperature --> <!-- of 288.2 kelvins, that gives 63737 lbs of nominal thrust. --> <jet x="-34.93" y="16.26" z="-1.20" mass="8000" thrust="63737"> <control-input axis="/controls/throttle[0]" control="THROTTLE"/> </jet> <jet x="-26.50" y="12.65" z="-2.41" mass="8000" thrust="63737"> <control-input axis="/controls/throttle[0]" control="THROTTLE"/> </jet> <jet x="-26.50" y="-12.65" z="-2.41" mass="8000" thrust="63737"> <control-input axis="/controls/throttle[1]" control="THROTTLE"/> </jet> <jet x="-34.93" y="-16.26" z="-1.20" mass="8000" thrust="63737"> <control-input axis="/controls/throttle[1]" control="THROTTLE"/> </jet> <gear x="-5.42" y="0.00" z="-5.42" compression="2"> <!-- nose --> <control-input axis="/controls/rudder" control="STEER" square="true"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/> <control-speed control="EXTEND" transition-time="7"/> </gear> <gear x="-29.15" y="5.42" z="-5.42" compression="2"> <!-- fwd left main --> <control-input axis="/controls/brakes[0]" control="BRAKE"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/> <control-speed control="EXTEND" transition-time="7"/> </gear> <gear x="-31.32" y="1.81" z="-5.42" compression="2"> <!-- rear left main --> <control-input axis="/controls/brakes[0]" control="BRAKE"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/> <control-speed control="EXTEND" transition-time="7"/> </gear> <gear x="-31.32" y="-1.81" z="-5.42" compression="2"> <!-- rear right main --> <control-input axis="/controls/brakes[1]" control="BRAKE"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/> <control-speed control="EXTEND" transition-time="7"/> </gear> <gear x="-29.15" y="-5.42" z="-5.42" compression="2"> <!-- fwd right main --> <control-input axis="/controls/brakes[1]" control="BRAKE"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/> <control-speed control="EXTEND" transition-time="7"/> </gear> <tank x="-26.50" y="0" z="-1.45" jet="true" capacity="128000"/> <tank x="-30.10" y="8" z="-1.45" jet="true" capacity="128000"/> <tank x="-30.10" y="-8" z="-1.45" jet="true" capacity="128000"/> <ballast x="-6" y="0" z="2.4" mass="30000"/> <!-- hump --> <ballast x="-12" y="0" z="2.4" mass="40000"/> <!-- hump --> <ballast x="-18" y="0" z="2.4" mass="40000"/> <!-- hump --> <ballast x="-24" y="0" z="2.4" mass="30000"/> <!-- hump --> </airplane>