<airplane mass="3903"> <approach speed="70" aoa="16"> <control-setting axis="/controls/throttle[0]" value="0.4"/> <control-setting axis="/controls/throttle[1]" value="0.4"/> <control-setting axis="/controls/mixture[0]" value="1.0"/> <control-setting axis="/controls/mixture[1]" value="1.0"/> <control-setting axis="/controls/propeller-pitch[0]" value="0.5"/> <control-setting axis="/controls/propeller-pitch[1]" value="0.5"/> <control-setting axis="/controls/flaps" value="1.0"/> <control-setting axis="/controls/gear-down" value="1"/> </approach> <cruise speed="223" alt="20000"> <control-setting axis="/controls/throttle[0]" value="1.0"/> <control-setting axis="/controls/throttle[1]" value="1.0"/> <control-setting axis="/controls/mixture[0]" value="1.0"/> <control-setting axis="/controls/mixture[1]" value="1.0"/> <control-setting axis="/controls/propeller-pitch[0]" value="1.0"/> <control-setting axis="/controls/propeller-pitch[1]" value="1.0"/> <control-setting axis="/controls/flaps" value="0.0"/> <control-setting axis="/controls/gear-down" value="0"/> </cruise> <cockpit x="-2.78" y="0.26" z="0.95"/> <fuselage ax="0.00" ay="0" az="0" bx="-9.50" by="0" bz="0" width="1.5" taper="0" midpoint="0.4"/> <wing x="-3.65" y="0.62" z="-0.18" length ="4.68" chord ="1.68" sweep="0" dihedral="5" taper="0.8" camber="0.1"> <stall aoa="16" width="4" peak="1.5"/> <flap0 start="0" end=".5" lift="1.5" drag="1.2"/> <flap1 start=".55" end=".94" lift="1.3" drag="1.2"/> <control-input axis="/controls/flaps" control="FLAP0"/> <control-speed control="FLAP0" transition-time="5"/> <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/> <control-input axis="/controls/aileron" control="FLAP1" split="true"/> <control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/> <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="-8.33" y="0.22" z="0.07" length ="2.34" chord ="1.24" sweep="0" dihedral="0" taper="0.6"> <stall aoa="16" width="4" peak="1.5"/> <flap0 start="0" end="1" lift="1.68" 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="-8.26" y="0.00" z="0.26" length ="2.16" chord ="1.61" sweep="36" taper="0.5"> <stall aoa="16" width="4" peak="1.5"/> <flap0 start="0" end="1" lift="1.3" drag="1.2"/> <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"/> </vstab> <!-- Late model 310's had 50 gallon tip tanks, and 31.5 gallon wing tanks. Some also had nacelle tanks, but those aren't modeled here --> <tank x="-3.62" y="5.30" z="0.44" capacity="300"/> <tank x="-3.62" y="1.02" z="-0.15" capacity="189"/> <tank x="-3.62" y="-1.02" z="-0.15" capacity="189"/> <tank x="-3.62" y="-5.30" z="0.44" capacity="300"/> <gear x="0.00" y="0.00" z="-1.35" compression=".5" retract-time="7"> <control-input axis="/controls/rudder" control="STEER"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-speed control="EXTEND" transition-time="7"/> <control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/> </gear> <gear x="-4.02" y="1.32" z="-1.35" compression=".5" retract-time="7"> <control-input axis="/controls/brakes[0]" control="BRAKE"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-speed control="EXTEND" transition-time="6.2"/> <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/> </gear> <gear x="-4.02" y="-1.32" z="-1.35" compression=".5" retract-time="7"> <control-input axis="/controls/brakes[1]" control="BRAKE"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-speed control="EXTEND" transition-time="6"/> <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/> </gear> <propeller x="-2.56" y="1.83" z="0.07" mass="800" moment="12" radius="1.0" eng-power="285" eng-rpm="2700" turbo-mul="2" wastegate-mp="40" cruise-power="157" cruise-speed="195" cruise-rpm="2100" cruise-alt="20000" min-rpm="1600" max-rpm="2700"> <actionpt x="-1.53" y="1.83" z="0.07"/> <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"/> <control-input axis="/controls/propeller-pitch[0]" control="ADVANCE"/> </propeller> <propeller x="-2.56" y="-1.83" z="0.07" mass="800" moment="12" radius="1.0" eng-power="285" eng-rpm="2700" turbo-mul="2" wastegate-mp="40" cruise-power="157" cruise-speed="195" cruise-rpm="2100" cruise-alt="20000" min-rpm="1600" max-rpm="2700"> <actionpt x="-1.53" y="-1.83" z="0.07"/> <control-input axis="/controls/throttle[1]" control="THROTTLE"/> <control-input axis="/controls/starter[1]" control="STARTER"/> <control-input axis="/controls/magnetos[1]" control="MAGNETOS"/> <control-input axis="/controls/mixture[1]" control="MIXTURE"/> <control-input axis="/controls/propeller-pitch[1]" control="ADVANCE"/> </propeller> <ballast x="-2.78" y="0.26" z="0.0" mass="180"/> <!-- pilot --> <ballast x="-2.2" y="0" z="0.0" mass="240"/> <!-- cockpit --> <weight x="-4.24" y="0" z="0" mass-prop="/yasim/c310/passenger-lbs"/> </airplane>