Found C:\Program Files\Microsoft Games\FS2002\aircraft\Alitalia Express ATR72-500\aired.ini

Record: 0341 Elevators Effectivity
Points: 5
-0.349000 1.000000
-0.175000 0.700000
0.000000 0.600000
0.175000 0.700000
0.349000 1.000000

Record: 0342 Ailerons Effectivity
Points: 7
-0.785000 1.000000
-0.524000 1.000000
-0.175000 1.000000
0.000000 1.000000
0.175000 1.000000
0.524000 1.000000
0.785000 1.000000

Record: 0343 Rudder Effectivity
Points: 7
-0.785000 0.500000
-0.524000 0.600000
-0.175000 0.900000
0.000000 1.000000
0.175000 0.900000
0.524000 0.600000
0.785000 0.500000

Record: 0517 *Elevator Moment Factor vs Dynamic Pressure (lb/ft^2)
Points: 5
0.000000 1.000000
135.000000 1.000000
300.000000 1.000000
1000.000000 0.600000
1500.000000 0.500000

Record: 0518 Ailerons Moment Factor vs Dynamic Pressure (lb/ft^2)
Points: 5
0.000000 1.000000
300.000000 0.700000
600.000000 0.200000
1482.000000 0.100000
1500.000000 0.100000

Record: 0519 Rudder Moment Factor vs Dynamic Pressure (lb/ft^2)
Points: 5
0.000000 1.000000
300.000000 1.000000
800.000000 0.500000
1000.000000 0.300000
1500.000000 0.200000

Record: 1525 *!FS2K Roll? Damping Coeff vs Dynamic Pressure (lb/ft^2)
Points: 5
0.000000 1.000000
300.000000 0.800000
800.000000 0.200000
1000.000000 0.200000
1500.000000 0.200000

Record: 0400 *Wing dCl/dAoA vs Relative Height - Ground Effect
Points: 11
0.054000 1.250000
0.100000 1.160000
0.200000 1.096100
0.300000 1.060000
0.400000 1.040000
0.500000 1.030000
0.600000 1.024200
0.700000 1.021300
0.800000 1.016100
0.900000 1.010000
1.000000 1.000000

Record: 0401 *Wing dCl/dAoA Factor vs Mach
Points: 17
0.000000 1.000000
0.200000 1.000000
0.400000 1.036900
0.600000 1.101800
0.800000 1.268700
1.000000 0.600000
1.200000 0.500000
1.400000 0.400000
1.600000 0.400000
1.800000 0.400000
2.000000 0.400000
2.200000 0.396800
2.400000 0.357100
2.600000 0.337300
2.800000 0.327400
3.000000 0.327400
3.200000 0.327400

Record: 0404 *Wing Cl vs AoA (rad)
Points: 21
-3.141600 0.000000
-2.748900 0.359900
-2.356200 0.500000
-1.570800 0.000000
-0.785400 -0.666500
-0.197200 -0.879900
-0.209400 -0.838200
-0.034900 0.000000
0.226900 1.261000
0.244300 1.344000
0.261800 1.400000
0.279300 1.443000
0.302300 1.344000
0.321300 1.213000
0.401400 1.048500
0.450500 1.030500
0.523600 1.016000
1.570800 0.000000
2.356200 -0.500000
2.748900 -0.359900
3.141600 0.000000

Record: 0410 *Mach Related?
Points: 17
0
0
-21
-82
-246
-246
-205
-164
-123
-82
-41
-41
-41
-41
-41
-41
-41

Record: 0411 *Mach Related * 65536?
Points: 17
0
0
410
1024
2253
3482
2253
1024
410
410
410
410
410
410
410
410
410

Record: 0412 Mach Related
Points: 17
0
0
-410
-1024
-2458
-2458
-1024
-410
0
0
0
0
0
0
0
0
0

Record: 0413 Mach Related
Points: 17
0
0
20
82
328
328
328
328
328
328
328
328
328
328
328
328
328

Record: 0420 Elevator Effect vs Mach * 2048?
Points: 17
0
0
0
-33
-99
-207
-205
-102
0
51
102
102
102
102
102
102
102

Record: 0421 Aileron Effect vs Mach * 2048?
Points: 17
0
51
205
563
1536
2048
0
-6144
-8192
-9216
-10240
-10240
-10240
-10240
-10240
-10240
-10240

Record: 0422 Rudder Effect vs Mach * 2048?
Points: 17
0
-1229
-2458
-3686
-5222
-6758
-5068
-3379
-1690
0
1024
2048
2048
2048
2048
2048
2048

Record: 0423 Mach Related * 2048?
Points: 17
0
102
205
410
1024
717
717
717
717
717
717
717
717
717
717
717
717

Record: 0536 CFS/FS2K Elevator Moment Factor vs Body AoA
Points: 5
-25.000000 0.100000
-12.000000 1.000000
12.000000 1.000000
16.000000 0.300000
25.000000 0.100000

Record: 0537 CFS/FS2K Ailerons Moment Factor vs Body AoA
Points: 5
-15.000000 0.000000
0.000000 1.000000
13.000000 0.700000
14.000000 0.700000
25.000000 0.400000

Record: 0538 CFS/FS2K Rudder Moment Factor vs Body AoA
Points: 5
-15.000000 1.000000
0.000000 1.000000
5.000000 1.000000
16.000000 0.700000
25.000000 0.300000

Record: 0539 *!CFS/FS2K Pitch Damping? Coeff vs Body AoA
Points: 5
-15.000000 1.000000
0.000000 1.000000
11.000000 1.000000
16.000000 0.700000
25.000000 0.700000

Record: 0430 *Mach Drag vs Mach * 2048
Points: 17
0
0
7
14
20
80
70
60
50
40
40
40
40
40
40
40
40

Record: 0433 *Pitching Moment vs Mach * 2048?
Points: 17
0
0
0
2
6
6
6
6
6
6
6
6
6
6
6
6
6

Record: 0440 ?Zeros
Points: 17
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0

Record: 0441 Mach Related
Points: 17
0
0
0
0
-10
-10
-10
-10
-10
-10
-10
-10
-10
-10
-10
-10
-10

Record: 0442 ?Zeros
Points: 17
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0

Record: 0443 ?Zeros
Points: 17
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0

Record: 0450 ?Zeros
Points: 17
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0

Record: 0451 *Dihedral Effect Coeff vs Body AoA
Points: 9
-180.000000 1.000000
-90.000000 0.200000
-16.000000 0.200000
-10.000000 0.800000
0.000000 1.000000
10.000000 0.800000
16.000000 0.200000
90.000000 0.200000
180.000000 1.000000

Record: 0452 ?Zeros
Points: 17
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0

Record: 0453 Mach Related
Points: 17
0
0
-10
-21
-41
-51
-51
-51
-51
-51
-51
-51
-51
-51
-51
-51
-51

Record: 0454 ?Zeros
Points: 17
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0

Record: 0455 Mach Related
Points: 17
0
-10
-41
-102
-205
-225
-225
-225
-225
-225
-225
-225
-225
-225
-225
-225
-225

Record: 0456 *Roll Damping Coeff vs Body AoA
Points: 9
-180.000000 1.000000
-90.000000 0.300000
-16.000000 0.200000
-10.000000 0.600000
0.000000 1.000000
10.000000 0.600000
16.000000 0.200000
90.000000 0.300000
180.000000 1.000000

Record: 0459 ?Zeros
Points: 17
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0

Record: 0460 *Weathervane Stability Coeff vs Body AoA
Points: 9
-180.000000 1.000000
-90.000000 0.000000
-16.000000 0.200000
-10.000000 0.300000
0.000000 1.000000
10.000000 0.300000
16.000000 0.200000
90.000000 0.000000
180.000000 1.000000

Record: 0461 ?Zeros
Points: 17
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0

Record: 0462 Mach Related?
Points: 17
0
0
-2
-4
-6
-6
-6
-6
-6
-6
-6
-6
-6
-6
-6
-6
-6

Record: 0463 ?Zeros or Mach Related
Points: 17
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0

Record: 0464 Yaw Damping Coeff vs Body AoA
Points: 9
-180.000000 1.000000
-90.000000 0.100000
-16.000000 0.200000
-10.000000 0.400000
0.000000 1.000000
10.000000 0.400000
16.000000 0.200000
90.000000 0.100000
180.000000 1.000000

Record: 0465 ?Zeros
Points: 17
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0

Record: 0473 *Pitch Moment Coeff vs Body AoA (rad)
Points: 7
-3.141600 -1.274400
-0.392700 -0.814000
-0.279300 -0.296000
0.000000 0.000000
0.279300 0.296000
0.392700 0.814000
3.141600 1.274400

Record: 1503 *FS2K Turbine LoMach CN2 vs Throttle IAP Ratio
columns: 3 rows: 9
0.000000 1.000000 4.237000
0.000000 62.000000 67.020000
0.420000 80.800000 94.480000
0.510000 86.200000 101.520000
0.610000 89.700000 108.060000
0.750000 95.700000 108.060000
0.800000 97.000000 108.060000
0.900000 99.600000 108.060000
1.000000 101.500000 108.060000

Record: 1504 *FS2K Turbine HiMach CN2 vs Throttle and IAP Ratio
columns: 3 rows: 9
0.900000 1.000000 4.237000
0.000000 44.290000 60.460000
0.420000 63.390000 75.100000
0.510000 68.280000 79.400000
0.610000 73.180000 83.800000
0.700000 76.610000 88.000000
0.790000 80.120000 90.000000
0.930000 82.380000 94.000000
1.000000 83.830000 95.000000

Record: 1506 *FS2K Turbine Thrust Factor vs CN1 and Mach No.
columns: 11 rows: 21
0.000000 0.000000 0.100000 0.200000 0.300000 0.400000 0.500000 0.600000 0.700000 0.800000 0.900000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
20.000000 0.025400 0.055400 0.061890 0.105230 0.118770 0.094630 0.076800 0.202860 0.073260 0.074090
25.000000 0.050800 0.066460 0.083710 0.123340 0.147570 0.141940 0.138970 0.231830 0.153860 0.159290
30.000000 0.079830 0.088630 0.109200 0.145110 0.179970 0.196540 0.204800 0.275290 0.238090 0.255630
35.000000 0.112490 0.114460 0.138310 0.181400 0.215970 0.247490 0.270630 0.329710 0.322290 0.348290
40.000000 0.152370 0.151400 0.181970 0.217690 0.262770 0.309430 0.340000 0.387710 0.410290 0.444570
45.000000 0.199540 0.192030 0.225660 0.268490 0.316860 0.367710 0.413140 0.460000 0.498290 0.540860
50.000000 0.253970 0.243710 0.283890 0.326570 0.374290 0.436860 0.490000 0.536000 0.589710 0.540860
55.000000 0.315710 0.306570 0.345710 0.395430 0.453430 0.506000 0.570570 0.623140 0.681430 0.740860
60.000000 0.388290 0.380290 0.422290 0.471710 0.532860 0.582290 0.654570 0.720860 0.780290 0.844570
65.000000 0.471710 0.468860 0.506000 0.555140 0.615430 0.669710 0.746000 0.826000 0.886570 0.959430
70.000000 0.569710 0.564860 0.596860 0.649430 0.709140 0.768000 0.844860 0.934570 1.000000 1.078000
75.000000 0.678570 0.672000 0.706000 0.754570 0.817140 0.873430 0.954570 1.050570 1.120860 1.200290
80.000000 0.805430 0.808570 0.844290 0.881710 0.946570 1.000860 1.082570 1.170000 1.249140 1.337430
85.000000 0.946860 0.948860 0.986290 1.030290 1.087140 1.146570 1.236000 1.318570 1.399140 1.489140
90.000000 1.121140 1.118860 1.142860 1.193710 1.249140 1.310290 1.400570 1.488860 1.564000 1.648570
95.000000 1.306000 1.303430 1.328570 1.375140 1.443430 1.506860 1.590860 1.659140 1.747140 1.826290
100.000000 1.458570 1.462290 1.488570 1.538290 1.601710 1.666860 1.733430 1.796570 1.904860 1.985710
105.000000 1.589140 1.580570 1.626860 1.668860 1.720570 1.790860 1.839430 1.919710 2.025710 2.119140
110.000000 1.690570 1.680000 1.743430 1.781430 1.817710 1.892570 1.920000 2.032290 2.120860 2.233710

Record: 1507 *FS2K Turbine Mass Flow Factor vs CN1 and Mach No.
columns: 11 rows: 21
0.000000 0.000000 0.100000 0.200000 0.300000 0.400000 0.500000 0.600000 0.700000 0.800000 0.900000
0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000
20.000000 4.289540 5.128800 7.063760 9.464970 9.651470 9.628160 10.327540 11.423240 12.472320 14.080900
25.000000 6.061310 6.714070 8.299340 10.210980 10.700550 11.073550 11.772930 12.775380 13.707890 15.153280
30.000000 7.809770 8.345960 9.651470 11.213430 11.936120 12.612190 13.334890 14.174150 15.060030 16.318920
35.000000 9.581540 9.977850 11.050240 12.332440 13.148390 14.034270 14.826900 15.596220 16.365540 17.507870
40.000000 11.329990 11.609740 12.425690 13.637950 14.547150 15.526290 16.342230 16.948360 17.647740 18.626880
45.000000 13.148390 13.241640 14.010960 14.990090 15.945910 17.018300 17.834250 18.347130 18.999880 19.792520
50.000000 14.873530 14.920150 15.596220 16.458790 17.391300 18.510320 19.349570 19.699270 20.305400 20.911530
55.000000 16.621980 16.621980 17.228120 17.927500 18.906630 19.979020 20.841590 21.121340 21.587600 21.983910
60.000000 18.393750 18.417060 19.069820 19.559390 20.491900 21.424410 22.520110 22.473480 22.939740 23.149550
65.000000 20.025640 20.165520 20.771650 21.261220 22.007230 22.916420 23.475930 23.825620 24.245250 24.221940
70.000000 21.844040 21.983910 22.543420 22.963050 23.569180 24.338500 24.804760 25.177760 25.527450 25.340950
75.000000 23.662430 23.848930 24.245250 24.734820 25.201070 25.807200 26.320080 26.599840 26.529900 26.390020
80.000000 25.620700 25.760580 26.133580 26.483270 26.879590 27.485720 27.858720 27.998600 27.835410 27.765470
85.000000 27.835410 27.858720 28.185100 28.441540 28.697980 29.024360 29.420680 29.350740 29.234180 29.164240
90.000000 30.259940 30.026810 30.306560 30.423130 30.609630 30.749500 30.982630 30.702880 30.702880 30.586320
95.000000 32.124960 32.124960 32.171580 32.241520 32.474650 32.311460 32.428020 31.938450 32.055020 32.008390
100.000000 33.593660 33.756850 33.663600 33.663600 33.686910 33.383840 33.523720 33.010840 33.174030 33.174030
105.000000 34.712670 34.805920 34.829230 34.829230 34.502860 34.083230 34.246420 33.826790 34.129850 34.129850
110.000000 35.295490 35.155610 35.481990 35.715120 35.085670 34.572790 34.479540 34.642730 34.945800 35.225550

Record: 1508 *!FS2K Turbine Turboprop Torque Related vs CN2
Points: 3
0.000000 0.000000
40.000000 0.031000
101.500000 1.900000

Record: 0509 *Engine[Per Cyl]/TurboProp Friction Torque vs RPM
Points: 4
-10.000000 -0.200000
10.000000 0.200000
70.000000 0.800000
100.000000 0.800000

Record: 0511 *Propeller Efficiency vs Blade Angle and Adv Ratio
columns: 13 rows: 12
0.000000 0.000000 0.200000 0.400000 0.600000 0.800000 1.000000 1.200000 1.400000 1.600000 1.800000 2.000000 2.200000
10.000000 0.000000 0.021000 0.046000 0.155000 0.619000 0.700000 0.598000 0.456000 0.400000 0.343000 0.271000 0.215000
15.000000 0.380000 0.542000 0.670000 0.790000 0.500000 0.403000 0.360000 0.320000 0.290000 0.253000 0.210000 0.164000
20.000000 0.081000 0.280000 0.560000 0.760000 0.860000 0.625000 0.552000 0.498000 0.425000 0.361000 0.307000 0.255000
25.000000 0.050000 0.200000 0.425000 0.650000 0.800000 0.883000 0.750000 0.674000 0.595000 0.509000 0.425000 0.332000
30.000000 0.040000 0.160000 0.325000 0.505000 0.680000 0.820000 0.890000 0.870000 0.748000 0.636000 0.542000 0.449000
35.000000 0.030000 0.130000 0.270000 0.400000 0.550000 0.690000 0.810000 0.885000 0.909000 0.700000 0.606000 0.523000
40.000000 0.020000 0.100000 0.210000 0.330000 0.440000 0.560000 0.690000 0.790000 0.865000 0.904000 0.900000 0.712000
45.000000 0.010000 0.109000 0.179000 0.269000 0.371000 0.478000 0.573000 0.660000 0.760000 0.831000 0.881000 0.906000
50.000000 0.000000 0.081000 0.155000 0.240000 0.313000 0.397000 0.471000 0.552000 0.629000 0.720000 0.785000 0.840000
55.000000 0.000000 0.067000 0.135000 0.206000 0.283000 0.353000 0.427000 0.506000 0.571000 0.640000 0.710000 0.743000
70.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000

Record: 0512 *Propeller Thrust Coefficient vs Blade Angle and Adv Ratio
columns: 14 rows: 12
0.000000 0.000000 0.200000 0.400000 0.600000 0.800000 1.000000 1.200000 1.400000 1.600000 1.800000 2.000000 2.200000 2.400000
10.000000 0.060000 0.045000 0.025000 -0.060000 -0.236000 -0.750000 -1.580000 -2.600000 -3.570000 -4.820000 -6.050000 -7.170000 -8.390000
15.000000 0.120000 0.095000 0.070000 0.035000 -0.050000 -0.378000 -1.080000 -1.780000 -2.610000 -3.450000 -4.390000 -5.450000 -6.600000
20.000000 0.248000 0.225000 0.180000 0.142000 0.089000 -0.032000 -0.250000 -0.806000 -1.630000 -2.390000 -3.200000 -4.060000 -5.000000
25.000000 0.354000 0.343000 0.309000 0.263000 0.222000 0.146000 0.000000 -0.167000 -0.567000 -1.260000 -2.020000 -2.940000 -3.780000
30.000000 0.472000 0.468000 0.461000 0.430000 0.392000 0.347000 0.290000 0.165000 0.000000 -0.356000 -0.760000 -1.350000 -2.280000
35.000000 0.605000 0.608000 0.586000 0.559000 0.555000 0.536000 0.506000 0.461000 0.404000 0.305000 0.127000 -0.234000 -1.630000
40.000000 0.768000 0.753000 0.737000 0.722000 0.722000 0.700000 0.677000 0.654000 0.612000 0.559000 0.483000 0.385000 0.077000
45.000000 0.912000 0.908000 0.889000 0.889000 0.889000 0.889000 0.893000 0.878000 0.851000 0.810000 0.734000 0.650000 0.529000
50.000000 1.030000 1.030000 1.030000 1.030000 1.030000 1.030000 1.030000 1.030000 1.007000 0.961000 0.900000 0.817000 0.684000
55.000000 1.117000 1.117000 1.117000 1.117000 1.117000 1.117000 1.117000 1.117000 1.117000 1.117000 1.117000 1.117000 1.117000
60.000000 1.261000 1.261000 1.261000 1.261000 1.261000 1.261000 1.261000 1.261000 1.261000 1.261000 1.261000 1.261000 1.261000

Record: 0514 *CFS/FS2K Hydraulic (Elec/Pneu?) Output vs RPM
Points: 5
0.000000 0.000000
5500.000000 160000.000000
14000.000000 350000.000000
22000.000000 420000.000000
29920.000000 422000.000000

Record: 1524 *FS2K Turbine Reheat Thrust Factor vs Mach No.
Points: 10
0.000000 1.000000
0.200000 1.000000
0.400000 1.000000
0.600000 1.000000
0.800000 1.000000
1.000000 1.000000
1.200000 1.000000
1.400000 1.000000
1.600000 1.000000
1.800000 1.000000


Record count: 127