<airplane mass="1480"> <!-- Approach configuration --> <approach speed="43" aoa="17"> <control-setting axis="/controls/throttle[0]" value="0.3"/> <control-setting axis="/controls/mixture[0]" value="1.0"/> <control-setting axis="/controls/flaps" value="1.0"/> </approach> <!-- Cruise configuration --> <cruise speed="122" alt="0"> <control-setting axis="/controls/throttle[0]" value="1.0"/> <control-setting axis="/controls/mixture[0]" value="1.0"/> <control-setting axis="/controls/flaps" value="0.0"/> </cruise> <cockpit x="-2.5" y=".33" z="0.6"/> <fuselage ax="0.5" ay="0" az="0" bx="-7.75" by="0" bz="0" width="1.5" taper="0.2" midpoint="0.3"/> <wing x="-2.75" y="0.6" z="-0.75" taper="0.65" length="4.5" chord="1.65" sweep="0" dihedral="5" camber="0.1"> <stall aoa="16" width="6" peak="1.5"/> <flap0 start="0" end="0.5" lift="1.3" drag="1.5"/> <flap1 start="0.5" end="1.0" lift="1.2" drag="1.2"/> <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-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"/> </wing> <hstab x="-6.5" y="0.00" z=".15" taper="1.0" effectiveness="2" length="1.9" chord="0.9" sweep="0"> <stall aoa="18" width="4" peak="1.5"/> <flap0 start="0" end="1" lift="2.0" 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="-6.25" y="0" z=".3" taper=".5" length="1.2" chord="1.2" sweep="10"> <stall aoa="16" width="4" peak="1.5"/> <flap0 start="0" end="1" lift="1.3" drag="1.1"/> <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> <propeller radius="1.0" cruise-speed="125" cruise-rpm="2665" cruise-alt="8000" cruise-power="120" takeoff-power="140.8" takeoff-rpm="2200" eng-power="160" eng-rpm="2800" x="-1" y="0" z="0" mass="400" moment="8"> <actionpt x="0" y="0" z="0"/> <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"/> </propeller> <gear x="-1" y="0" z="-1.3" compression=".05"> <!-- nose --> <control-input axis="/controls/rudder" control="STEER" src0="-1.0" src1="1.0" dst0="-0.1" dst1="0.1"/> </gear> <gear x="-2.8" y="1.5" z="-1.3" compression=".05"> <!-- left main --> <control-input axis="/controls/brakes[0]" control="BRAKE" split="true"/> <control-input axis="/controls/parking-brake" control="BRAKE" split="true"/> </gear> <gear x="-2.8" y="-1.5" z="-1.3" compression=".05"> <!-- left main --> <control-input axis="/controls/brakes[1]" control="BRAKE" split="true"/> <control-input axis="/controls/parking-brake" control="BRAKE" split="true"/> </gear> <tank x="-2.5" y="1.5" z="-0.25" capacity="144"/> <tank x="-2.5" y="-1.5" z="-0.25" capacity="144"/> <ballast x="-2.0" y="0" z="0" mass="400"/> <!-- cockpit --> <weight x="-2.5" y=".33" z="0" mass-prop="/yasim/pa28/pilot-lb"/> <weight x="-2.5" y="-.33" z="0" mass-prop="/yasim/pa28/copilot-lb"/> </airplane>