diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/flight_model.cfg b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/flight_model.cfg
index 9fc4644..12ca2a0 100644
--- a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/flight_model.cfg
+++ b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/flight_model.cfg
@@ -1,4 +1,4 @@
-//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.6.5_GE_F 04APR25
+//TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.0_GE_F 15MAY25
 
 [VERSION]
 //KH Bump major
@@ -22,16 +22,16 @@ max_number_of_stations = 15
 station_load.0=170.0, 82.0, -2.0, 4.0, Pilot, 1
 station_load.1=170.0, 82.0, 2.0, 4.0, First Officer, 2
 station_load.2=170.0, 80.0, 3.3, 4.0, Engineer, 0
-station_load.3=8675.0, 60.0, -5.0, 4.0, Upper zone 1 L, 0
-station_load.4=8675.0, 60.0, 5.0, 4.0, Upper zone 1 R, 0
-station_load.5=11675.0, 10.0, -5.0, 4.0, Upper zone 2 L, 0
-station_load.6=11675.0, 10.0, 5.0, 4.0, Upper zone 2 R, 0
-station_load.7=11675.0, -40.0, -5.0, 4.0, Upper zone 3 L, 0
-station_load.8=11675.0, -40.0, 5.0, 4.0, Upper zone 3 R, 0
-station_load.9=14675.0, -90.0, -5.0, 4.0, Upper zone 4 L, 0
-station_load.10=14675.0, -90.0, 5.0, 4.0, Upper zone 4 R, 0
-station_load.11=44648.0, 30.0, 0.0, -4.5, Lower forward cargo, 0
-station_load.12=64685.0, -50.0, 0.0, -4.5, Lower rear cargo, 0
+station_load.3=8675.0, 55.0, -5.0, 4.0, Upper zone 1 L, 0
+station_load.4=8675.0, 55.0, 5.0, 4.0, Upper zone 1 R, 0
+station_load.5=11675.0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
+station_load.6=11675.0, 20.0, 5.0, 4.0, Upper zone 2 R, 0
+station_load.7=11675.0, -20.0, -5.0, 4.0, Upper zone 3 L, 0
+station_load.8=11675.0, -20.0, 5.0, 4.0, Upper zone 3 R, 0
+station_load.9=14675.0, -50.0, -5.0, 4.0, Upper zone 4 L, 0
+station_load.10=14675.0, -50.0, 5.0, 4.0, Upper zone 4 R, 0
+station_load.11=64648.0, 30.0, 0.0, -4.5, Lower forward cargo, 0
+station_load.12=44685.0, -30.0, 0.0, -4.5, Lower rear cargo, 0
 station_load.13=0.0, 5.0, -2.0, -4.5, Left aux tank, 0
 station_load.14=0.0, 5.0, 2.0, -4.5, Right aux tank, 0
 
@@ -111,7 +111,7 @@ htail_area = 920
 htail_span = 59.5
 htail_pos_lon = -88
 htail_pos_vert = 5.0
-htail_incidence = 1.0
+htail_incidence = 0.8
 htail_sweep = 36.5
 htail_thickness_ratio = 0.02
 vtail_area = 760
@@ -155,7 +155,7 @@ fly_by_wire = 0
 elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
 aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
 rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
-elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.44, 290:0.44, 315:0.40
+elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
 
 [AERODYNAMICS]
 lift_coef_pitch_rate = -8.09375
@@ -403,4 +403,4 @@ drag_scalar = 0.475
 pitch_scalar = 1
 max_on_ground_position = 1
 flaps-position.0 = 0, -1, 0
-flaps-position.1 = 20, 215, 0.5, 0.5
\ No newline at end of file
+flaps-position.1 = 20, 215, 0.5, 0.5
diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/engines.cfg b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/engines.cfg
deleted file mode 100644
index 06d684a..0000000
--- a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/engines.cfg
+++ /dev/null
@@ -1,115 +0,0 @@
-//TFDi Designs MD-11F (P&W PW4662) vRC1.6.5_PW_F 04APR25
-
-[VERSION]
-//KH Bump major
-major = 4
-minor = 1
-
-[GENERALENGINEDATA]
-engine_type =1
-fuel_flow_scalar =0.031
-min_throttle_limit =-0.25
-master_ignition_switch =0
-starter_type =0
-max_contrail_temperature =-25
-Engine.0 = -3.00, -27.75, -8.50
-ThrustAnglesPitchHeading.0 = 0, 0
-Engine.1 = -103.50, 0.00, 15.00
-ThrustAnglesPitchHeading.1 = 0, 0
-Engine.2 = -3.00, 27.75, -8.50
-ThrustAnglesPitchHeading.2 = 0, 0
-accumulated_time_hobbs_min_pct_rpm=0
-accumulated_time_hobbs_min_knots=0
-
-[DISABLED_CONTROLS]
-DisableFuelValveControls =0
-DisableMixtureControls =1
-DisableParkingBrakeControls =0
-DisablePropellerControls =1
-DisableAutopilotControls=1
-
-[TURBINEENGINEDATA]
-fuel_flow_gain=1
-low_idle_n1=24.2
-low_idle_n2=62.9
-inlet_area=10.53
-rated_N2_rpm=11055
-static_thrust=62000
-reverser_available=1
-reverser_mach_controlled=0
-afterburner_available=0
-afterburner_throttle_threshold=0
-ThrustSpecificFuelConsumption=0.362
-use_commanded_Ne_Table=1
-use_corrected_N2_from_FF_table=1
-use_n2_to_n1_table=1
-use_old_fuelflow_simvar=1
-n2_to_n1_table=0:0:0.85,0:0:0,10:1.1:1,20:2.7:2.4,30:5.7:4.7,40:11.1:9.78,50:16.35:14.9,64.54:31.14:30.59,70.28:36.78:35.84,80.12:58.56:57.84,90.37:88.27:87.84,102.67:107.24:106.84,112:120:120
-mach_0_corrected_commanded_ne_table=0:1:5.42,0:63.0:63.5,0.17:69.3:70.2,0.34:76.2:76.8,0.51:83:83.5,0.67:89.8:90.2,0.83:96.7:96.9,0.99:103.5:103.5,1:116.6:117
-mach_hi_corrected_commanded_ne_table=0.88:1:5.42,0:66:66.5,0.25:77.1:79.2,0.33:81.4:83.8,0.5:88.4:90.7,0.66:94.3:97.0,0.85:96.2:99.7,0.9:101.2:105.4,1:116.2:121.2
-corrected_n2_from_ff_table=0:17,0.0099:63.7,0.02:70.5,0.03:73.1,0.04:79.4,0.05:83.6,0.06:89.5,0.07:94.8,0.08:100.1,0.09:106.5
-n1_and_mach_on_thrust_table=0.000000:0.000000:0.206803:0.280661:0.354519:0.428377:0.502235:0.576093:0.649951:0.723810:0.797668,0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000,20.000000:0.020334:0.018926:0.018365:0.017768:0.017149:0.016515:0.015863:0.015208:0.014534:0.013860,25.000000:0.029434:0.027422:0.026632:0.025797:0.024940:0.024059:0.023152:0.022235:0.021306:0.020375,30.000000:0.033986:0.030672:0.028919:0.026653:0.025928:0.025184:0.025802:0.021374:0.018702:0.023291,35.000000:0.070581:0.064962:0.062424:0.059648:0.056670:0.053536:0.050308:0.046924:0.043444:0.039910,40.000000:0.115706:0.107129:0.103436:0.099453:0.095210:0.090734:0.086072:0.081361:0.076653:0.071841,45.000000:0.164968:0.152931:0.147828:0.142341:0.136513:0.130440:0.124498:0.118283:0.111870:0.105388,50.000000:0.218546:0.202746:0.196107:0.188982:0.181423:0.174048:0.166338:0.158287:0.149967:0.142050,55.000000:0.276676:0.256828:0.248552:0.239686:0.230419:0.221263:0.211681:0.201686:0.191443:0.181712,60.000000:0.339274:0.315126:0.305110:0.294428:0.283152:0.272084:0.260539:0.248522:0.236179:0.224430,65.000000:0.406072:0.377362:0.365531:0.352959:0.339697:0.326347:0.312745:0.298645:0.284078:0.270104,70.000000:0.476658:0.443151:0.429436:0.414899:0.399618:0.383785:0.368032:0.351772:0.335030:0.318542,75.000000:0.550568:0.512033:0.496350:0.479778:0.462414:0.444307:0.426075:0.407561:0.388596:0.369500,80.000000:0.627228:0.583453:0.565725:0.547049:0.527537:0.507273:0.486477:0.465611:0.444349:0.422704,85.000000:0.705886:0.656705:0.636874:0.616041:0.594344:0.571897:0.548783:0.525433:0.501810:0.477902,90.000000:0.785094:0.730712:0.708789:0.685821:0.661969:0.637381:0.612132:0.586376:0.560384:0.534209,95.000000:0.863065:0.803680:0.779839:0.754920:0.729110:0.702557:0.675366:0.647478:0.619241:0.590907,100.000000:0.936071:0.872277:0.847042:0.820755:0.793551:0.765559:0.736891:0.707114:0.677066:0.646923,105.000000:0.994083:0.928996:0.903986:0.877967:0.850934:0.822172:0.792494:0.762245:0.731543:0.700495,110.000000:0.974676:0.921881:0.905331:0.888737:0.871094:0.851457:0.828909:0.802711:0.772336:0.737555
-corrected_airflow_table=0:0:0.9,0:0:0,20:4.29:14.08,85:4.62:24,90:5.75:25,95:7.23:27,100:8.36:28,105:9.29:29,120:10.94:30
-n2_and_mach_to_epr_table=0:0:0.242:0.413:0.452:0.613:0.673:0.763:0.82:0.84,0:0:0:0:0:0:0:0:0:0,66:0.568:0.570:0.600:0.800:1.100:1.250:1.850:2.000:2.300,89:0.610:0.612:0.820:1.038:1.210:1.350:2.150:2.177:2.700,93:0.625:0.638:0.850:1.048:1.073:1.301:2.040:2.532:2.600,97:0.940:0.959:0.950:1.055:0.913:1.526:2.785:2.991:4.050,100:1.600:1.500:1.900:2.500:3.000:3.500:3.900:4.300:5.230
-JET_density_on_FF_table=0.000462:28.74,0.000587:32.93,0.000738:35.02,0.000891:29.46,0.001066:31.02,0.001267:32.56,0.001496:34.54,0.0017565:35.11,0.002048:30.8,0.002377:22.55
-epr_max=1.8
-epr_tc=14
-epr_tuning_constant=1
-oil_temp_cooling_constant=0.21
-oil_temp_heating_constant=700
-oil_temp_tc=0.07
-oil_temp_tuning_constant=1
-oil_temp_factor_from_rpm=0.00:0.80, 250.00:0.80, 500.00:0.80, 2500.00:1.00, 4000.00:1.00
-oil_press_max=38000
-oil_press_tc=0.8
-oil_press_tuning_constant=1
-itt_peak_temperature=2141
-itt_tc=2
-itt_tuning_constant=1
-egt_peak_temperature=1600
-egt_tc=0.1
-egt_tuning_constant=0.1
-fuel_press_max=2376
-fuel_press_tc=2
-fuel_press_tuning_constant=1
-variable_inlet=0
-primary_nozzle_available=0
-starter_N1_max_pct=40
-starter_N1_rate=200
-starter_time=45
-ignition_auto_type=""
-min_condition_lever_for_combustion=0.01
-min_n1_for_combustion=2
-min_n2_for_combustion=17
-min_n1_for_starter_cutoff=7
-min_n2_for_starter_cutoff=45
-min_n2_for_apu_bleed_air_cutoff=50
-n1_normal_tc=0.5
-n1_start_max_rate=1
-n1_start_combustion_max_rate=2
-idle_fuel_flow=600
-idle_high_fuel_flow=40
-min_n2_for_fuel_flow=17
-high_n1=110
-high_n2=114
-high_fuel_flow=9800
-mach_influence_on_n1=10
-fuel_flow_max=10000
-fuel_flow_controller_p=0.5
-fuel_flow_controller_i=0.01
-fuel_flow_controller_d=0.1
-fuel_flow_controller_iboundary=10
-fuel_flow_controller_dboundary=100
-max_torque_protection=0
-max_n1_protection=110
-max_n2_protection=114
-max_egt_protection=2000
-fuel_flow_max_itt_factor=2
-fuel_flow_min_itt_factor=0.9
-n1_cooling_factor=0.01
-n2_from_bleed_air_psi_table=0.0:0.0, 4.0:8.0, 10.0:18.0, 18.0:25.0
-bleed_air_on_n2_tc=1
-N1_to_oil_pressure_table=0.00:0.00, 0.21:0.71, 0.90:0.99, 1.00:1.00
-
-[JET_ENGINE]
-thrust_scalar=1.0
diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/flight_model.cfg b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/flight_model.cfg
index 9613f2d..e8c0da2 100644
--- a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/flight_model.cfg
+++ b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/flight_model.cfg
@@ -1,4 +1,4 @@
-//TFDi Designs MD-11F (P&W PW4662) vRC1.6.5_PW_F 04APR25
+//TFDi Designs MD-11F (P&W PW4660) vRC1.7.0_PW_F 15MAY25
 
 [VERSION]
 //KH Bump major
@@ -10,7 +10,7 @@ max_gross_weight = 630500
 empty_weight = 248567
 reference_datum_position = 0, 0, 0
 empty_weight_CG_position = -13.3, 0, 0
-CG_forward_limit = 0.13
+CG_forward_limit = 0.12
 CG_aft_limit = 0.34
 empty_weight_pitch_MOI = 20897456
 empty_weight_roll_MOI = 6368555
@@ -22,16 +22,16 @@ max_number_of_stations = 15
 station_load.0=170.0, 82.0, -2.0, 4.0, Pilot, 1
 station_load.1=170.0, 82.0, 2.0, 4.0, First Officer, 2
 station_load.2=170.0, 80.0, 3.3, 4.0, Engineer, 0
-station_load.3=8675.0, 60.0, -5.0, 4.0, Upper zone 1 L, 0
-station_load.4=8675.0, 60.0, 5.0, 4.0, Upper zone 1 R, 0
-station_load.5=11675.0, 10.0, -5.0, 4.0, Upper zone 2 L, 0
-station_load.6=11675.0, 10.0, 5.0, 4.0, Upper zone 2 R, 0
-station_load.7=11675.0, -40.0, -5.0, 4.0, Upper zone 3 L, 0
-station_load.8=11675.0, -40.0, 5.0, 4.0, Upper zone 3 R, 0
-station_load.9=14675.0, -90.0, -5.0, 4.0, Upper zone 4 L, 0
-station_load.10=14675.0, -90.0, 5.0, 4.0, Upper zone 4 R, 0
-station_load.11=44648.0, 30.0, 0.0, -4.5, Lower forward cargo, 0
-station_load.12=64685.0, -50.0, 0.0, -4.5, Lower rear cargo, 0
+station_load.3=8675.0, 55.0, -5.0, 4.0, Upper zone 1 L, 0
+station_load.4=8675.0, 55.0, 5.0, 4.0, Upper zone 1 R, 0
+station_load.5=11675.0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
+station_load.6=11675.0, 20.0, 5.0, 4.0, Upper zone 2 R, 0
+station_load.7=11675.0, -20.0, -5.0, 4.0, Upper zone 3 L, 0
+station_load.8=11675.0, -20.0, 5.0, 4.0, Upper zone 3 R, 0
+station_load.9=14675.0, -50.0, -5.0, 4.0, Upper zone 4 L, 0
+station_load.10=14675.0, -50.0, 5.0, 4.0, Upper zone 4 R, 0
+station_load.11=64648.0, 30.0, 0.0, -4.5, Lower forward cargo, 0
+station_load.12=44685.0, -30.0, 0.0, -4.5, Lower rear cargo, 0
 station_load.13=0.0, 5.0, -2.0, -4.5, Left aux tank, 0
 station_load.14=0.0, 5.0, 2.0, -4.5, Right aux tank, 0
 
@@ -111,7 +111,7 @@ htail_area = 920
 htail_span = 59.5
 htail_pos_lon = -88
 htail_pos_vert = 5.0
-htail_incidence = 1.0
+htail_incidence = 0.8
 htail_sweep = 36.5
 htail_thickness_ratio = 0.02
 vtail_area = 760
@@ -155,7 +155,7 @@ fly_by_wire = 0
 elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
 aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
 rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
-elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.44, 290:0.44, 315:0.40
+elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
 
 [AERODYNAMICS]
 lift_coef_pitch_rate = -8.09375
@@ -383,7 +383,7 @@ blowout-speed = 300
 maneuvering_flaps = 0
 lift_scalar = 0.5
 // KH From 0.75
-drag_scalar = 0.75
+drag_scalar = 0.475
 pitch_scalar = 1
 max_on_ground_position = 1
 flaps-position.0 = 0, -1, 0
@@ -399,8 +399,8 @@ blowout-speed = 300
 maneuvering_flaps = 0
 lift_scalar = 0.5
 // KH From 0.75
-drag_scalar = 0.75
+drag_scalar = 0.475
 pitch_scalar = 1
 max_on_ground_position = 1
 flaps-position.0 = 0, -1, 0
-flaps-position.1 = 20, 215, 0.5, 0.5
\ No newline at end of file
+flaps-position.1 = 20, 215, 0.5, 0.5
diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/flight_model.cfg b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/flight_model.cfg
new file mode 100644
index 0000000..c37a076
--- /dev/null
+++ b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/flight_model.cfg
@@ -0,0 +1,415 @@
+//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.0_GE 15MAY25
+
+[VERSION]
+//KH Bump major
+major = 4
+minor = 1
+
+[WEIGHT_AND_BALANCE]
+max_gross_weight = 630500
+empty_weight = 283975
+reference_datum_position = 0, 0, 0
+empty_weight_CG_position = -13.3, 0, 0
+CG_forward_limit = 0.12
+CG_aft_limit = 0.34
+empty_weight_pitch_MOI = 20897456
+empty_weight_roll_MOI = 6368555
+empty_weight_yaw_MOI = 40761191
+empty_weight_coupled_MOI = 0
+activate_mach_limit_based_on_cg = 0
+activate_cg_limit_based_on_mach = 0
+max_number_of_stations = 21
+station_load.0=170.0, 82.0, -2.0, 4.0, Pilot, 1
+station_load.1=170.0, 82.0, 2.0, 4.0, First Officer, 2
+station_load.2=170.0, 80.0, 3.3, 4.0, Engineer, 0
+station_load.3=850.0, 66.0, 0.0, 4.0, Cabin crew 1, 0
+station_load.4=680.0, 45.0, -5.0, 4.0, Business 1 L, 0
+station_load.5=680.0, 45.0, 0.0, 4.0, Business 1 C, 0
+station_load.6=680.0, 45.0, 5.0, 4.0, Business 1 R, 0
+station_load.7=680.0, 25.0, -5.0, 4.0, Business 2 L, 0
+station_load.8=960.0, 25.0, 0.0, 4.0, Business 2, 0
+station_load.9=680.0, 25.0, 5.0, 4.0, Business 2 R, 0
+station_load.10=5723.0, -20.0, -5.0, 4.0, Economy 3 L, 0
+station_load.11=5724.0, -20.0, 0.0, 4.0, Economy 3 C, 0
+station_load.12=5723.0, -20.0, 5.0, 4.0, Economy 3 R, 0
+station_load.13=9066.0, -50.0, -5.0, 4.0, Economy 4 L, 0
+station_load.14=9067.0, -50.0, 0.0, 4.0, Economy 4 C, 0
+station_load.15=9066.0, -50.0, 5.0, 4.0, Economy 4 R, 0
+station_load.16=850.0, -55.0, 0.0, 4.0, Cabin crew 2, 0
+station_load.17=40648.0, 30.0, 0.0, -4.5, Forward cargo, 0
+station_load.18=26648.0, -30.0, 0.0, -4.5, Rear cargo, 0
+station_load.19=0.0, 5.0, -2.0, -4.5, Left aux tank, 0
+station_load.20=0.0, 5.0, 2.0, -4.5, Right aux tank, 0
+
+[CONTACT_POINTS]
+static_pitch = 0
+static_cg_height = 16.4
+gear_system_type = 1
+tailwheel_lock = 0
+max_number_of_points = 16
+gear_locked_on_ground = 0
+gear_locked_above_speed = -1
+max_speed_full_steering = 25
+min_available_steering_angle_pct = 0.2
+max_speed_decreasing_steering = 45
+max_speed_full_steering_castering = 20
+max_speed_decreasing_steering_castering = 35
+emergency_extension_type = 2
+hyd_need_power_to_function= 0
+min_castering_angle = 0.05236
+max_castering_angle = 1.32645
+allow_stopped_steering = 1
+point.0 = 1, 64.22,  0.00,  -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50,  0, 200, 250, 8
+point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0,  1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
+point.2 = 1, -19.00,  17.15, -18.02, 2000, 2, 2.25, 0,  1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8
+point.3 = 1, -19.00,  0.00, -18.02, 2000, 2, 2.25, 0,  1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8
+point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 9, 0, 0, 1
+point.5 = 2, -48, -82.5, 0.0,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 5, 0, 0, 1
+point.6 = 2, -48, 82.5, 0.0,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 6, 0, 0, 1
+point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 9, 0, 0, 1
+point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 9, 0, 0, 1
+point.9 = 2, 16.0,  -28.00,  -13.00,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 4, 0, 0, 1
+point.10 = 2, 16.0,  28.00,  -13.00,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 4, 0, 0, 1
+point.11 = 2, -110.0,  0.00,  14.20,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 4, 0, 0, 1
+point.12 = 2, -96.5, 0.0, 42.0,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 4, 0, 0, 1
+point.13 = 2, -94.5, -30.0, 8.0,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 4, 0, 0, 1
+point.14 = 2, -94.5, 30.0, 8.05,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 4, 0, 0, 1
+point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 9, 0, 0, 1
+
+[FUEL]
+LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
+RightMain = -20.00, 38.00, -1.0, 8938, 10.00
+Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
+Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
+Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
+LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
+RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
+External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
+LeftAux = 5.00, -2.00, -3.00, 0.00, 10.00
+RightAux = 5.00, 2.00, -3.00, 0.00, 10.00
+fuel_type = 2
+number_of_tank_selectors = 3
+electric_pump = 0
+engine_driven_pump = 1
+manual_transfer_pump = 0
+manual_pump = 0
+anemometer_pump = 0
+fuel_dump_rate = 0.02
+default_fuel_tank_selector.1 = 1
+default_fuel_tank_selector.2 = 1
+default_fuel_tank_selector.3 = 1
+
+[AIRPLANE_GEOMETRY]
+wing_area = 3648
+wing_span = 170.5
+wing_root_chord = 34.68
+wing_camber = 1
+wing_thickness_ratio = 0.04
+wing_dihedral = 2.2
+wing_incidence = 1.5
+wing_twist = -0.5
+oswald_efficiency_factor = 0.72
+wing_winglets_flag = 1
+wing_sweep = 38
+wing_pos_apex_lon = 1
+wing_pos_apex_vert = -2.75
+htail_area = 920
+htail_span = 59.5
+htail_pos_lon = -88
+htail_pos_vert = 5.0
+htail_incidence = 0.8
+htail_sweep = 36.5
+htail_thickness_ratio = 0.02
+vtail_area = 760
+vtail_span = 28.1
+vtail_sweep = 43
+vtail_pos_lon = -79.5
+vtail_pos_vert = 28
+vtail_thickness_ratio = 0.03
+fuselage_length = 202.16
+fuselage_diameter = 19.75
+fuselage_center_pos = 10, 0, 1.0
+elevator_area = 327.0
+aileron_area = 225.0
+rudder_area = 190.0
+elevator_up_limit = 25
+elevator_down_limit = 15
+aileron_up_limit = 25
+aileron_down_limit = 15
+rudder_limit = 23
+rudder_trim_limit = 20
+elevator_trim_limit = 30
+spoiler_limit = 60
+spoilerons_available = 1
+aileron_to_spoileron_gain = 3
+min_ailerons_for_spoilerons = 10
+min_flaps_for_spoilerons = 0
+spoiler_extension_time = 2.0
+spoiler_handle_available = 1
+auto_spoiler_available = 1
+auto_spoiler_auto_retracts = 0
+auto_spoiler_min_speed = 72
+positive_g_limit_flaps_up = 5.0
+positive_g_limit_flaps_down = 4.0
+negative_g_limit_flaps_up = -4.0
+negative_g_limit_flaps_down = -3.0
+load_safety_factor = 1.5
+elevator_trim_neutral = -1
+aileron_to_rudder_scale = 0
+flap_to_aileron_scale = 0
+fly_by_wire = 0
+elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
+aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
+rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
+elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
+
+[AERODYNAMICS]
+lift_coef_pitch_rate = -8.09375
+lift_coef_daoa = 2.68359
+lift_coef_delta_elevator = -0.28906
+lift_coef_horizontal_incidence = 0.91357
+lift_coef_flaps = 1
+lift_coef_spoilers = 0
+drag_coef_zero_lift = 0.02539
+drag_coef_flaps = 0.1889
+drag_coef_gear = 0.0549
+drag_coef_spoilers = 0.05207
+side_force_slip_angle = -0.77392
+side_force_roll_rate = 0.15478
+side_force_yaw_rate = 0
+side_force_delta_rudder = -0.14746
+pitch_moment_horizontal_incidence = 4.24755
+pitch_moment_delta_elevator = -2.37011
+pitch_moment_delta_trim = 0
+pitch_moment_pitch_damping = -214.1455
+pitch_moment_aoa_0 = 0.11621
+pitch_moment_daoa = 8.87255
+pitch_moment_flaps = 0.0105
+pitch_moment_gear = 0.0171
+pitch_moment_spoilers = 0
+pitch_moment_delta_elevator_propwash = -2.37011
+pitch_moment_pitch_propwash = -214.1455
+roll_moment_slip_angle = 0.26855
+roll_moment_roll_damping = -3.40869
+roll_moment_yaw_rate = -0.27197
+roll_moment_spoilers = 0.07
+roll_moment_delta_aileron = -0.34521
+roll_moment_delta_rudder = 0.01660
+roll_moment_delta_aileron_trim_scalar = -0.2
+yaw_moment_slip_angle = 0.18066
+yaw_moment_roll = 0.07470
+yaw_moment_yaw_damping = -2.49023
+yaw_moment_yaw_propwash = 0
+yaw_moment_delta_aileron = -0.00683
+yaw_moment_delta_rudder = 0.07128
+yaw_moment_delta_rudder_propwash = 0.075
+yaw_moment_delta_rudder_trim_scalar = -0.2
+compute_aero_center = 0
+aero_center_lift = -13.75
+lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0
+lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0
+lift_coef_mach_table = 0:1
+lift_coef_delta_elevator_mach_table = 0:0
+lift_coef_daoa_mach_table = 0:0
+lift_coef_pitch_rate_mach_table = 0:0
+lift_coef_horizontal_incidence_mach_table = 0:0
+drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337
+side_force_slip_angle_mach_table = 0:0
+side_force_delta_rudder_mach_table = 0:0
+side_force_yaw_rate_mach_table = 0:0
+side_force_roll_rate_mach_table = 0:0
+pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2
+pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1
+pitch_moment_horizontal_incidence_aoa_table = 0:1
+pitch_moment_daoa_aoa_table = 0:1
+pitch_moment_pitch_alpha_table = 0:1
+pitch_moment_delta_elevator_mach_table = 0:0
+pitch_moment_daoa_mach_table = 0:0
+pitch_moment_pitch_rate_mach_table = 0:0
+pitch_moment_horizontal_incidence_mach_table = 0:0
+pitch_moment_aoa_0_mach_table = 0:0
+roll_moment_aoa_table = 0:0
+roll_moment_slip_angle_aoa_table = 0:1
+roll_moment_roll_rate_aoa_table = 0:1
+roll_moment_delta_aileron_aoa_table = 0:1
+roll_moment_slip_angle_mach_table = 0:0
+roll_moment_delta_rudder_mach_table = 0:0
+roll_moment_delta_aileron_mach_table = 0:0
+roll_moment_yaw_rate_mach_table = 0:0
+roll_moment_roll_rate_mach_table = 0:0
+yaw_moment_aoa_table = 0:0
+yaw_moment_slip_angle_aoa_table = 0:1
+yaw_moment_yaw_rate_aoa_table = 0:1
+yaw_moment_delta_rudder_aoa_table = 0:1
+yaw_moment_slip_angle_mach_table = 0:0
+yaw_moment_delta_rudder_mach_table = 0:0
+yaw_moment_delta_aileron_mach_table = 0:0
+yaw_moment_yaw_rate_mach_table = 0:0
+yaw_moment_roll_rate_mach_table = 0:0
+elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
+aileron_scaling_table = -0.785:1 ;0:1
+rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
+elevator_lift_coef=3
+rudder_lift_coef=2
+aileron_load_factor_effectiveness_table = 0:1
+lift_coef_at_drag_zero = 0.1
+lift_coef_at_drag_zero_flaps = 0.1
+
+[FLIGHT_TUNING]
+modern_fm_only = 1
+cruise_lift_scalar = 1
+parasite_drag_scalar = 1
+induced_drag_scalar = 1
+flap_induced_drag_scalar = 1
+elevator_effectiveness = 1
+elevator_maxangle_scalar = 1
+aileron_effectiveness = 1
+rudder_effectiveness = 1
+rudder_maxangle_scalar = 1
+pitch_stability = 5
+roll_stability = 1
+yaw_stability = 1
+pitch_gyro_stability = 1
+roll_gyro_stability = 1
+yaw_gyro_stability = 1
+empty_CG_deviation_limit=0
+elevator_trim_effectiveness = 1.5
+aileron_trim_effectiveness = 1
+rudder_trim_effectiveness = 1
+hi_alpha_on_roll = 0
+hi_alpha_on_yaw = 0
+p_factor_on_yaw = 0
+torque_on_roll = 0
+gyro_precession_on_roll = 0
+gyro_precession_on_yaw = 0
+engine_wash_on_roll = 0
+wingflex_scalar = 2
+wingflex_offset = 0
+stall_coef_at_min_weight = 0.71
+ground_crosswind_effect_zero_speed=10
+ground_crosswind_effect_max_speed=150
+ground_high_speed_steeringwheel_static_friction_scalar=1.5
+ground_high_speed_otherwheel_static_friction_scalar=1.2
+//KH START New ground physics
+ground_new_contact_model_gear_flex=0.0044
+ground_new_contact_model_gear_flex_damping=7
+ground_new_contact_model_rolling_stickyness=0.15
+ground_new_contact_model_up_to_speed_lateral=10000
+ground_new_contact_model_up_to_speed_lateral_steering=10000
+ground_new_contact_model_up_to_speed_longitudinal=10000
+enable_high_accuracy_integration=1
+//KH END New ground physics
+
+[REFERENCE SPEEDS]
+full_flaps_stall_speed = 115
+flaps_up_stall_speed = 149
+cruise_speed = 345
+cruise_mach = 0.85
+crossover_speed = 330
+max_mach = 0.9
+max_indicated_speed = 395
+max_flaps_extended = 170
+normal_operating_speed = 325
+airspeed_indicator_max = 562.5
+rotation_speed_min = 145
+climb_speed = 250
+cruise_alt = 41000
+takeoff_speed = 165
+spawn_cruise_altitude = 5000
+spawn_descent_altitude = 500
+best_angle_climb_speed = 0
+approach_speed = 0
+best_glide = 0
+max_gear_extended = 200
+
+[INTERACTIVE POINTS]
+number_of_interactive_points = 3
+interactive_point.0 = 0.4, 44.15, -10.05, -0.567, 0, 0, 0, -88, 35, 0, 35, 0, 2, 33
+interactive_point.1 = 0.4, 75.65, 7.92, -0.567, 0, 0, 0, 75, 33, 2, 33, 2, 2, 33
+interactive_point.2 = 0.4, 33.3, 6.28, -7.18, 1, 0, 0, 90, 0, 0, 0, 0, 0, 0
+
+[STALL PROTECTION]
+stall_protection = 1		; Alpha Protection
+off_limit = 11.5				; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit)
+off_yoke_limit = 1			; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit)
+on_limit = 14				; Alpha above which the Alpha Protection timer starts
+on_goal = 10				; The alpha that the Alpha Protection will attempt to reach when triggered
+timer_trigger = 1.0			; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered
+
+;===================== FLAPS =====================
+
+[FLAPS.0]
+type = 1
+system_type = 1
+span-outboard = 0.25
+extending-time = 22
+damaging-speed = 250
+blowout-speed = 300
+maneuvering_flaps = 0
+lift_scalar = 0.1
+drag_scalar = 1.1
+pitch_scalar = 1
+max_on_ground_position = 7
+flaps-position.0 = 0, -1, 0
+flaps-position.1 = 0, -1, 0
+flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
+flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
+flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1
+flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
+flaps-position.6 = 35, 160, 0.32, 1
+flaps-position.7 = 50, 150, 0.33, 1
+
+
+[FLAPS.1]
+type = 1
+system_type = 1
+span-outboard = 0.7
+extending-time = 23
+damaging-speed = 250
+blowout-speed = 300
+maneuvering_flaps = 0
+lift_scalar = 0.1
+drag_scalar = 1.1
+pitch_scalar = 1
+max_on_ground_position = 7
+flaps-position.0 = 0, -1, 0
+flaps-position.1 = 0, -1, 0
+flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
+flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
+flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1
+flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
+flaps-position.6 = 35, 160, 0.32, 1
+flaps-position.7 = 50, 150, 0.33, 1
+
+
+[FLAPS.2]
+type = 2
+system_type = 1
+span-outboard = 0.2
+extending-time = 8
+damaging-speed = 250
+blowout-speed = 300
+maneuvering_flaps = 0
+lift_scalar = 0.5
+// KH From 0.75
+drag_scalar = 0.475
+pitch_scalar = 1
+max_on_ground_position = 1
+flaps-position.0 = 0, -1, 0
+flaps-position.1 = 20, 215, 0.5, 0.5
+
+[FLAPS.3]
+type = 2
+system_type = 1
+span-outboard = 0.7
+extending-time = 21
+damaging-speed = 250
+blowout-speed = 300
+maneuvering_flaps = 0
+lift_scalar = 0.5
+// KH From 0.75
+drag_scalar = 0.475
+pitch_scalar = 1
+max_on_ground_position = 1
+flaps-position.0 = 0, -1, 0
+flaps-position.1 = 20, 215, 0.5, 0.5
\ No newline at end of file
diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_PW/flight_model.cfg b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_PW/flight_model.cfg
new file mode 100644
index 0000000..1682b7f
--- /dev/null
+++ b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_PW/flight_model.cfg
@@ -0,0 +1,413 @@
+//TFDi Designs MD-11 (PW4460) vRC1.7.0_PW 15MAY25
+
+[VERSION]
+//KH Bump major
+major = 4
+minor = 1
+
+[WEIGHT_AND_BALANCE]
+max_gross_weight = 630500
+empty_weight = 283975
+reference_datum_position = 0, 0, 0
+empty_weight_CG_position = -13.3, 0, 0
+CG_forward_limit = 0.12
+CG_aft_limit = 0.34
+empty_weight_pitch_MOI = 20897456
+empty_weight_roll_MOI = 6368555
+empty_weight_yaw_MOI = 40761191
+empty_weight_coupled_MOI = 0
+activate_mach_limit_based_on_cg = 0
+activate_cg_limit_based_on_mach = 0
+max_number_of_stations = 21
+station_load.0=170.0, 82.0, -2.0, 4.0, Pilot, 1
+station_load.1=170.0, 82.0, 2.0, 4.0, First Officer, 2
+station_load.2=170.0, 80.0, 3.3, 4.0, Engineer, 0
+station_load.3=850.0, 66.0, 0.0, 4.0, Cabin crew 1, 0
+station_load.4=680.0, 45.0, -5.0, 4.0, Business 1 L, 0
+station_load.5=680.0, 45.0, 0.0, 4.0, Business 1 C, 0
+station_load.6=680.0, 45.0, 5.0, 4.0, Business 1 R, 0
+station_load.7=680.0, 25.0, -5.0, 4.0, Business 2 L, 0
+station_load.8=960.0, 25.0, 0.0, 4.0, Business 2, 0
+station_load.9=680.0, 25.0, 5.0, 4.0, Business 2 R, 0
+station_load.10=5723.0, -20.0, -5.0, 4.0, Economy 3 L, 0
+station_load.11=5724.0, -20.0, 0.0, 4.0, Economy 3 C, 0
+station_load.12=5723.0, -20.0, 5.0, 4.0, Economy 3 R, 0
+station_load.13=9066.0, -50.0, -5.0, 4.0, Economy 4 L, 0
+station_load.14=9067.0, -50.0, 0.0, 4.0, Economy 4 C, 0
+station_load.15=9066.0, -50.0, 5.0, 4.0, Economy 4 R, 0
+station_load.16=850.0, -55.0, 0.0, 4.0, Cabin crew 2, 0
+station_load.17=40648.0, 30.0, 0.0, -4.5, Forward cargo, 0
+station_load.18=26648.0, -30.0, 0.0, -4.5, Rear cargo, 0
+station_load.19=0.0, 5.0, -2.0, -4.5, Left aux tank, 0
+station_load.20=0.0, 5.0, 2.0, -4.5, Right aux tank, 0
+
+[CONTACT_POINTS]
+static_pitch = 0
+static_cg_height = 16.4
+gear_system_type = 1
+tailwheel_lock = 0
+max_number_of_points = 16
+gear_locked_on_ground = 0
+gear_locked_above_speed = -1
+max_speed_full_steering = 25
+min_available_steering_angle_pct = 0.2
+max_speed_decreasing_steering = 45
+max_speed_full_steering_castering = 20
+max_speed_decreasing_steering_castering = 35
+emergency_extension_type = 2
+hyd_need_power_to_function= 0
+min_castering_angle = 0.05236
+max_castering_angle = 1.32645
+allow_stopped_steering = 1
+point.0 = 1, 64.22,  0.00,  -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50,  0, 200, 250, 8
+point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0,  1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
+point.2 = 1, -19.00,  17.15, -18.02, 2000, 2, 2.25, 0,  1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8
+point.3 = 1, -19.00,  0.00, -18.02, 2000, 2, 2.25, 0,  1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8
+point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 9, 0, 0, 1
+point.5 = 2, -48, -82.5, 0.0,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 5, 0, 0, 1
+point.6 = 2, -48, 82.5, 0.0,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 6, 0, 0, 1
+point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 9, 0, 0, 1
+point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 9, 0, 0, 1
+point.9 = 2, 16.0,  -28.00,  -13.00,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 4, 0, 0, 1
+point.10 = 2, 16.0,  28.00,  -13.00,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 4, 0, 0, 1
+point.11 = 2, -110.0,  0.00,  14.20,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 4, 0, 0, 1
+point.12 = 2, -96.5, 0.0, 42.0,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 4, 0, 0, 1
+point.13 = 2, -94.5, -30.0, 8.0,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 4, 0, 0, 1
+point.14 = 2, -94.5, 30.0, 8.05,  787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 4, 0, 0, 1
+point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0,  0, 0.00, 0.0, 0.0,  0.0,  0.0, 9, 0, 0, 1
+
+[FUEL]
+LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
+RightMain = -20.00, 38.00, -1.0, 8938, 10.00
+Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
+Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
+Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
+LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
+RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
+External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
+LeftAux = 5.00, -2.00, -3.00, 0.00, 10.00
+RightAux = 5.00, 2.00, -3.00, 0.00, 10.00
+fuel_type = 2
+number_of_tank_selectors = 3
+electric_pump = 0
+engine_driven_pump = 1
+manual_transfer_pump = 0
+manual_pump = 0
+anemometer_pump = 0
+fuel_dump_rate = 0.02
+default_fuel_tank_selector.1 = 1
+default_fuel_tank_selector.2 = 1
+default_fuel_tank_selector.3 = 1
+
+[AIRPLANE_GEOMETRY]
+wing_area = 3648
+wing_span = 170.5
+wing_root_chord = 34.68
+wing_camber = 1
+wing_thickness_ratio = 0.04
+wing_dihedral = 2.2
+wing_incidence = 1.5
+wing_twist = -0.5
+oswald_efficiency_factor = 0.72
+wing_winglets_flag = 1
+wing_sweep = 38
+wing_pos_apex_lon = 1
+wing_pos_apex_vert = -2.75
+htail_area = 920
+htail_span = 59.5
+htail_pos_lon = -88
+htail_pos_vert = 5.0
+htail_incidence = 0.8
+htail_sweep = 36.5
+htail_thickness_ratio = 0.02
+vtail_area = 760
+vtail_span = 28.1
+vtail_sweep = 43
+vtail_pos_lon = -79.5
+vtail_pos_vert = 28
+vtail_thickness_ratio = 0.03
+fuselage_length = 200.92
+fuselage_diameter = 19.75
+fuselage_center_pos = 10, 0, 1.0
+elevator_area = 327.0
+aileron_area = 225.0
+rudder_area = 190.0
+elevator_up_limit = 25
+elevator_down_limit = 15
+aileron_up_limit = 25
+aileron_down_limit = 15
+rudder_limit = 23
+rudder_trim_limit = 20
+elevator_trim_limit = 30
+spoiler_limit = 60
+spoilerons_available = 1
+aileron_to_spoileron_gain = 3
+min_ailerons_for_spoilerons = 10
+min_flaps_for_spoilerons = 0
+spoiler_extension_time = 2.0
+spoiler_handle_available = 1
+auto_spoiler_available = 1
+auto_spoiler_auto_retracts = 0
+auto_spoiler_min_speed = 72
+positive_g_limit_flaps_up = 5.0
+positive_g_limit_flaps_down = 4.0
+negative_g_limit_flaps_up = -4.0
+negative_g_limit_flaps_down = -3.0
+load_safety_factor = 1.5
+elevator_trim_neutral = -1
+aileron_to_rudder_scale = 0
+flap_to_aileron_scale = 0
+fly_by_wire = 0
+elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
+aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
+rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
+elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
+
+[AERODYNAMICS]
+lift_coef_pitch_rate = -8.09375
+lift_coef_daoa = 2.68359
+lift_coef_delta_elevator = -0.28906
+lift_coef_horizontal_incidence = 0.91357
+lift_coef_flaps = 1
+lift_coef_spoilers = 0
+drag_coef_zero_lift = 0.02539
+drag_coef_flaps = 0.1889
+drag_coef_gear = 0.0549
+drag_coef_spoilers = 0.05207
+side_force_slip_angle = -0.77392
+side_force_roll_rate = 0.15478
+side_force_yaw_rate = 0
+side_force_delta_rudder = -0.14746
+pitch_moment_horizontal_incidence = 4.24755
+pitch_moment_delta_elevator = -2.37011
+pitch_moment_delta_trim = 0
+pitch_moment_pitch_damping = -214.1455
+pitch_moment_aoa_0 = 0.11621
+pitch_moment_daoa = 8.87255
+pitch_moment_flaps = 0.0105
+pitch_moment_gear = 0.0171
+pitch_moment_spoilers = 0
+pitch_moment_delta_elevator_propwash = -2.37011
+pitch_moment_pitch_propwash = -214.1455
+roll_moment_slip_angle = 0.26855
+roll_moment_roll_damping = -3.40869
+roll_moment_yaw_rate = -0.27197
+roll_moment_spoilers = 0.07
+roll_moment_delta_aileron = -0.34521
+roll_moment_delta_rudder = 0.01660
+roll_moment_delta_aileron_trim_scalar = -0.2
+yaw_moment_slip_angle = 0.18066
+yaw_moment_roll = 0.07470
+yaw_moment_yaw_damping = -2.49023
+yaw_moment_yaw_propwash = 0
+yaw_moment_delta_aileron = -0.00683
+yaw_moment_delta_rudder = 0.07128
+yaw_moment_delta_rudder_propwash = 0.075
+yaw_moment_delta_rudder_trim_scalar = -0.2
+compute_aero_center = 0
+aero_center_lift = -13.75
+lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0
+lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0
+lift_coef_mach_table = 0:1
+lift_coef_delta_elevator_mach_table = 0:0
+lift_coef_daoa_mach_table = 0:0
+lift_coef_pitch_rate_mach_table = 0:0
+lift_coef_horizontal_incidence_mach_table = 0:0
+drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337
+side_force_slip_angle_mach_table = 0:0
+side_force_delta_rudder_mach_table = 0:0
+side_force_yaw_rate_mach_table = 0:0
+side_force_roll_rate_mach_table = 0:0
+pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2
+pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1
+pitch_moment_horizontal_incidence_aoa_table = 0:1
+pitch_moment_daoa_aoa_table = 0:1
+pitch_moment_pitch_alpha_table = 0:1
+pitch_moment_delta_elevator_mach_table = 0:0
+pitch_moment_daoa_mach_table = 0:0
+pitch_moment_pitch_rate_mach_table = 0:0
+pitch_moment_horizontal_incidence_mach_table = 0:0
+pitch_moment_aoa_0_mach_table = 0:0
+roll_moment_aoa_table = 0:0
+roll_moment_slip_angle_aoa_table = 0:1
+roll_moment_roll_rate_aoa_table = 0:1
+roll_moment_delta_aileron_aoa_table = 0:1
+roll_moment_slip_angle_mach_table = 0:0
+roll_moment_delta_rudder_mach_table = 0:0
+roll_moment_delta_aileron_mach_table = 0:0
+roll_moment_yaw_rate_mach_table = 0:0
+roll_moment_roll_rate_mach_table = 0:0
+yaw_moment_aoa_table = 0:0
+yaw_moment_slip_angle_aoa_table = 0:1
+yaw_moment_yaw_rate_aoa_table = 0:1
+yaw_moment_delta_rudder_aoa_table = 0:1
+yaw_moment_slip_angle_mach_table = 0:0
+yaw_moment_delta_rudder_mach_table = 0:0
+yaw_moment_delta_aileron_mach_table = 0:0
+yaw_moment_yaw_rate_mach_table = 0:0
+yaw_moment_roll_rate_mach_table = 0:0
+elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
+aileron_scaling_table = -0.785:1 ;0:1
+rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
+elevator_lift_coef=3
+rudder_lift_coef=2
+aileron_load_factor_effectiveness_table = 0:1
+lift_coef_at_drag_zero = 0.1
+lift_coef_at_drag_zero_flaps = 0.1
+
+[FLIGHT_TUNING]
+modern_fm_only = 1
+cruise_lift_scalar = 1
+parasite_drag_scalar = 1
+induced_drag_scalar = 1
+flap_induced_drag_scalar = 1
+elevator_effectiveness = 1
+elevator_maxangle_scalar = 1
+aileron_effectiveness = 1
+rudder_effectiveness = 1
+rudder_maxangle_scalar = 1
+pitch_stability = 5
+roll_stability = 1
+yaw_stability = 1
+pitch_gyro_stability = 1
+roll_gyro_stability = 1
+yaw_gyro_stability = 1
+empty_CG_deviation_limit=0
+elevator_trim_effectiveness = 1.5
+aileron_trim_effectiveness = 1
+rudder_trim_effectiveness = 1
+hi_alpha_on_roll = 0
+hi_alpha_on_yaw = 0
+p_factor_on_yaw = 0
+torque_on_roll = 0
+gyro_precession_on_roll = 0
+gyro_precession_on_yaw = 0
+engine_wash_on_roll = 0
+wingflex_scalar = 2
+wingflex_offset = 0
+stall_coef_at_min_weight = 0.71
+ground_crosswind_effect_zero_speed=10
+ground_crosswind_effect_max_speed=150
+ground_high_speed_steeringwheel_static_friction_scalar=1.5
+ground_high_speed_otherwheel_static_friction_scalar=1.2
+//KH START New ground physics
+ground_new_contact_model_gear_flex=0.0044
+ground_new_contact_model_gear_flex_damping=7
+ground_new_contact_model_rolling_stickyness=0.15
+ground_new_contact_model_up_to_speed_lateral=10000
+ground_new_contact_model_up_to_speed_lateral_steering=10000
+ground_new_contact_model_up_to_speed_longitudinal=10000
+enable_high_accuracy_integration=1
+//KH END New ground physics
+
+[REFERENCE SPEEDS]
+full_flaps_stall_speed = 115
+flaps_up_stall_speed = 149
+cruise_speed = 345
+cruise_mach = 0.85
+crossover_speed = 330
+max_mach = 0.9
+max_indicated_speed = 395
+max_flaps_extended = 170
+normal_operating_speed = 325
+airspeed_indicator_max = 562.5
+rotation_speed_min = 145
+climb_speed = 250
+cruise_alt = 41000
+takeoff_speed = 165
+spawn_cruise_altitude = 5000
+spawn_descent_altitude = 500
+best_angle_climb_speed = 0
+approach_speed = 0
+best_glide = 0
+max_gear_extended = 200
+
+[INTERACTIVE POINTS]
+number_of_interactive_points = 3
+interactive_point.0 = 0.4, 44.15, -10.05, -0.567, 0, 0, 0, -88, 35, 0, 35, 0, 2, 33
+interactive_point.1 = 0.4, 75.65, 7.92, -0.567, 0, 0, 0, 75, 33, 2, 33, 2, 2, 33
+interactive_point.2 = 0.4, 33.3, 6.28, -7.18, 1, 0, 0, 90, 0, 0, 0, 0, 0, 0
+
+[STALL PROTECTION]
+stall_protection = 1		; Alpha Protection
+off_limit = 11.5				; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit)
+off_yoke_limit = 1			; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit)
+on_limit = 14				; Alpha above which the Alpha Protection timer starts
+on_goal = 10				; The alpha that the Alpha Protection will attempt to reach when triggered
+timer_trigger = 1.0			; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered
+
+;===================== FLAPS =====================
+
+[FLAPS.0]
+type = 1
+system_type = 1
+span-outboard = 0.25
+extending-time = 22
+damaging-speed = 250
+blowout-speed = 300
+maneuvering_flaps = 0
+lift_scalar = 0.1
+drag_scalar = 1.1
+pitch_scalar = 1
+max_on_ground_position = 7
+flaps-position.0 = 0, -1, 0
+flaps-position.1 = 0, -1, 0
+flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
+flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
+flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1
+flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
+flaps-position.6 = 35, 160, 0.32, 1
+flaps-position.7 = 50, 150, 0.33, 1
+
+[FLAPS.1]
+type = 1
+system_type = 1
+span-outboard = 0.7
+extending-time = 23
+damaging-speed = 250
+blowout-speed = 300
+maneuvering_flaps = 0
+lift_scalar = 0.1
+drag_scalar = 1.1
+pitch_scalar = 1
+max_on_ground_position = 7
+flaps-position.0 = 0, -1, 0
+flaps-position.1 = 0, -1, 0
+flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
+flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
+flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1
+flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
+flaps-position.6 = 35, 160, 0.32, 1
+flaps-position.7 = 50, 150, 0.33, 1
+
+[FLAPS.2]
+type = 2
+system_type = 1
+span-outboard = 0.2
+extending-time = 8
+damaging-speed = 250
+blowout-speed = 300
+maneuvering_flaps = 0
+lift_scalar = 0.5
+// KH From 0.75
+drag_scalar = 0.475
+pitch_scalar = 1
+max_on_ground_position = 1
+flaps-position.0 = 0, -1, 0
+flaps-position.1 = 20, 215, 0.5, 0.5
+
+[FLAPS.3]
+type = 2
+system_type = 1
+span-outboard = 0.7
+extending-time = 21
+damaging-speed = 250
+blowout-speed = 300
+maneuvering_flaps = 0
+lift_scalar = 0.5
+// KH From 0.75
+drag_scalar = 0.475
+pitch_scalar = 1
+max_on_ground_position = 1
+flaps-position.0 = 0, -1, 0
+flaps-position.1 = 20, 215, 0.5, 0.5
\ No newline at end of file