Unknown 2001-01-01 $Revision: 1.18 $ Piper PA-28 general aviation aircraft This model was created using publicly available data, publicly available technical reports, textbooks, and guesses. It contains no proprietary or restricted data. If this model has been validated at all, it would be only to the extent that it seems to "fly right", and that it possibly complies with published, publicly known, performance data (maximum speed, endurance, etc.). Thus, this model is meant for educational and entertainment purposes only. This simulation model is not endorsed by the manufacturer. This model is not to be sold. 160 30 5.25 24.4 12.9 11.4 0 102 0 -6 81.6 -9.6 21 88.32 0 0 1070 1249 2312 1650 88.32 0 0 180 81.6 -9.6 0 35.8 0 -50 0.8 0.5 0.02 1500 100 15 NONE 0 111.1 -60 -42.4 0.8 0.5 0.02 5000 150 360.0 LEFT 0 111.1 60 -42.4 0.8 0.5 0.02 5000 150 360.0 RIGHT 0 271.9 0 -1.6 0.2 0.2 0.2 20000 1000 0.0 NONE 0 264.3 0 70.4 0.2 0.2 0.2 20000 1000 0.0 NONE 0 281.4 0 64.1 0.2 0.2 0.2 20000 1000 0.0 NONE 0 106.5 -180 5.2 0.2 0.2 0.2 10000 2000 0.0 NONE 0 106.5 180 5.2 0.2 0.2 0.2 10000 2000 0.0 NONE 0 0 0 0 0.2 0.2 0.2 10000 2000 0.0 NONE 0 35 0 0 0.0 0 0 0 4 0 0 0.0 0.0 0.0 1 10 90 0 0 150 150 fcs/elevator-cmd-norm fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum 0.01745 -28 23

fcs/elevator-pos-rad

fcs/aileron-cmd-norm fcs/roll-trim-cmd-norm -1 1 fcs/roll-trim-sum 0.01745 -30 15

fcs/left-aileron-pos-rad

-fcs/roll-trim-sum 0.01745 -30 15

fcs/right-aileron-pos-rad

fcs/rudder-cmd-norm fcs/yaw-trim-cmd-norm -1 1 fcs/yaw-trim-sum 0.01745 -27 27

fcs/rudder-pos-rad

fcs/flap-cmd-norm 0 0 15 2 25 1 40 1

fcs/flap-pos-deg

fcs/flap-pos-deg 0 40 0 1

fcs/flap-pos-norm

Change_in_lift_due_to_ground_effect aero/h_b-mac-ft 0.0000 1.2030 0.1000 1.1270 0.1500 1.0900 0.2000 1.0730 0.3000 1.0460 0.4000 1.0550 0.5000 1.0190 0.6000 1.0130 0.7000 1.0080 0.8000 1.0060 0.9000 1.0030 1.0000 1.0020 1.1000 1.0000 Drag_at_zero_lift aero/qbar-psf metrics/Sw-sqft 0.019 Delta_drag_due_to_flap_deflection aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.0000 0.0000 15.0000 0.0100 25.0000 0.0300 40.0000 0.0500 Drag_induced aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -0.1750 0.0130 -0.1400 0.0050 -0.1050 0.0010 -0.0700 0.0000 -0.0350 0.0050 0.0000 0.0150 0.0350 0.0290 0.0700 0.0500 0.1050 0.0760 0.1400 0.1060 0.1750 0.1340 0.2090 0.1590 0.2440 0.1810 0.2790 0.1960 0.3140 0.2050 0.3490 0.2010 Drag_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/mag-elevator-pos-rad 0.0600 Drag_due_to_sideslip aero/qbar-psf metrics/Sw-sqft aero/mag-beta-rad 0.1400 Drag_due_to_landing_gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.0300 Side_force_due_to_beta aero/qbar-psf metrics/Sw-sqft aero/beta-rad -0.2904 Side_force_due_to_aileron aero/qbar-psf metrics/Sw-sqft fcs/left-aileron-pos-rad 0.0000 Side_force_due_to_rudder aero/qbar-psf metrics/Sw-sqft fcs/rudder-pos-rad 0.2300 Side_force_due_to_roll_rate aero/qbar-psf metrics/Sw-sqft aero/bi2vel velocities/p-rad_sec -0.0342 Side_force_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft aero/bi2vel velocities/r-rad_sec 0.2166 Lift_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/function/kCLge aero/alpha-rad -0.1750 -0.4390 -0.1400 -0.2480 -0.1050 -0.0630 -0.0700 0.1260 -0.0350 0.3210 0.0000 0.5220 0.0350 0.7290 0.0700 0.9410 0.1050 1.1550 0.1400 1.3660 0.1750 1.5440 0.2090 1.6880 0.2440 1.7990 0.2790 1.8740 0.3140 1.9110 0.3490 1.8840 Delta_lift_due_to_flap_deflection aero/qbar-psf metrics/Sw-sqft aero/function/kCLge fcs/flap-pos-deg 0.0000 0.0000 15.0000 0.0650 25.0000 0.0160 40.0000 0.2540 Lift_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad 0.8100 Lift_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft aero/alphadot-rad_sec aero/ci2vel aero/alpha-rad -0.1750 2.3500 -0.1400 -0.4460 -0.1050 -0.4450 -0.0700 -0.4640 -0.0350 -0.4820 0.0000 -0.4980 0.0350 -0.5100 0.0700 -0.5180 0.1050 -0.5150 0.1400 -0.4570 0.1750 -0.3610 0.2090 -0.2750 0.2440 -0.1820 0.2790 -0.0750 0.3140 0.0710 0.3490 0.2530 Lift_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft velocities/q-rad_sec aero/ci2vel aero/alpha-rad -0.1750 10.6900 -0.1400 2.3540 -0.1050 2.4200 -0.0700 2.5400 -0.0350 2.6670 0.0000 2.6940 0.0350 2.6110 0.0700 2.5380 0.1050 2.4310 0.1400 2.1760 0.1750 1.7560 0.2090 1.3520 0.2440 0.9840 0.2790 0.4320 0.3140 -0.0930 0.3490 -0.2710 Roll_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad -0.0107 Roll_moment_due_to_roll_rate_(roll_damping) aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-rad_sec -0.4704 Roll_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-rad_sec -0.1665 Roll_moment_due_to_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad 0.0900 Roll_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.0192 Pitch_moment_due_to_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-rad -1.0230 Delta_pitching_moment_due_to_flap_deflection aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/flap-pos-deg 0.0000 0.0000 15.0000 -0.0654 25.0000 -0.0981 35.0000 -0.1140 Pitch_moment_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-rad_sec -6.3480 Pitch_moment_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -0.0840 Pitching_moment_at_zero_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft 0.0700 Pitch_moment_due_to_elevator_deflection aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad -0.6030 Yaw_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad 0.0921 Yaw_moment_due_to_roll_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-rad_sec -0.0691 Yaw_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-rad_sec -0.0930 Yaw_moment_due_to_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad 0.0068 Yaw_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.0430