diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/flight_model.cfg b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/flight_model.cfg
similarity index 100%
rename from PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/flight_model.cfg
rename to PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/flight_model.cfg
diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/panel/PANEL.CFG b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/panel/PANEL.CFG
similarity index 100%
rename from PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/panel/PANEL.CFG
rename to PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/panel/PANEL.CFG
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
deleted file mode 100644
index 6bc9b62..0000000
--- a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/flight_model.cfg
+++ /dev/null
@@ -1,399 +0,0 @@
-//TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.0_GE_F 15MAY25
-
-[VERSION]
-//KH Bump major
-major = 4
-minor = 1
-
-[WEIGHT_AND_BALANCE]
-max_gross_weight = 630500
-empty_weight = 248567
-reference_datum_position = 0, 0, 0
-empty_weight_CG_position = -13.3, 0, 0
-CG_forward_limit = 0.12
-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 = 15
-//KH START Empty default
-station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
-station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
-station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
-station_load.3=0, 55.0, -5.0, 4.0, Upper zone 1 L, 0
-station_load.4=0, 55.0, 5.0, 4.0, Upper zone 1 R, 0
-station_load.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
-station_load.6=0, 20.0, 5.0, 4.0, Upper zone 2 R, 0
-station_load.7=0, -20.0, -5.0, 4.0, Upper zone 3 L, 0
-station_load.8=0, -20.0, 5.0, 4.0, Upper zone 3 R, 0
-station_load.9=0, -50.0, -5.0, 4.0, Upper zone 4 L, 0
-station_load.10=0, -50.0, 5.0, 4.0, Upper zone 4 R, 0
-station_load.11=0, 30.0, 0.0, -4.5, Lower forward cargo, 0
-station_load.12=0, -30.0, 0.0, -4.5, Lower rear cargo, 0
-station_load.13=0, 5.0, -2.0, -4.5, Left aux tank, 0
-station_load.14=0, 5.0, 2.0, -4.5, Right aux tank, 0
-//KH END
-
-[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
-//KH From 5.00, -2.00, -3.00, 0.00, 10.00
-LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00
-//KH From 5.00, 2.00, -3.00, 0.00, 10.0
-RightAux = 5.00, 2.00, -3.00, 1917.00, 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
-
-[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 = 2
-interactive_point.0 = 0.4, 75.65, -8.12, -0.567, 0, 0, 0, -75, 33, 2, 33, 2, 2, 33
-interactive_point.1 = 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
-drag_scalar = 0.75
-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
-drag_scalar = 0.75
-pitch_scalar = 1
-max_on_ground_position = 1
-flaps-position.0 = 0, -1, 0
-flaps-position.1 = 20, 215, 0.5, 0.5
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
deleted file mode 100644
index a6e752f..0000000
--- a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/flight_model.cfg
+++ /dev/null
@@ -1,399 +0,0 @@
-//TFDi Designs MD-11F (P&W PW4660) vRC1.7.0_PW_F 15MAY25
-
-[VERSION]
-//KH Bump major
-major = 4
-minor = 1
-
-[WEIGHT_AND_BALANCE]
-max_gross_weight = 630500
-empty_weight = 248567
-reference_datum_position = 0, 0, 0
-empty_weight_CG_position = -13.3, 0, 0
-CG_forward_limit = 0.12
-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 = 15
-//KH START Empty default
-station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
-station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
-station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
-station_load.3=0, 55.0, -5.0, 4.0, Upper zone 1 L, 0
-station_load.4=0, 55.0, 5.0, 4.0, Upper zone 1 R, 0
-station_load.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
-station_load.6=0, 20.0, 5.0, 4.0, Upper zone 2 R, 0
-station_load.7=0, -20.0, -5.0, 4.0, Upper zone 3 L, 0
-station_load.8=0, -20.0, 5.0, 4.0, Upper zone 3 R, 0
-station_load.9=0, -50.0, -5.0, 4.0, Upper zone 4 L, 0
-station_load.10=0, -50.0, 5.0, 4.0, Upper zone 4 R, 0
-station_load.11=0, 30.0, 0.0, -4.5, Lower forward cargo, 0
-station_load.12=0, -30.0, 0.0, -4.5, Lower rear cargo, 0
-station_load.13=0, 5.0, -2.0, -4.5, Left aux tank, 0
-station_load.14=0, 5.0, 2.0, -4.5, Right aux tank, 0
-//KH END
-
-[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
-//KH From 5.00, -2.00, -3.00, 0.00, 10.00
-LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00
-//KH From 5.00, 2.00, -3.00, 0.00, 10.0
-RightAux = 5.00, 2.00, -3.00, 1917.00, 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
-
-[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 = 2
-interactive_point.0 = 0.4, 75.65, -8.12, -0.567, 0, 0, 0, -75, 33, 2, 33, 2, 2, 33
-interactive_point.1 = 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
-drag_scalar = 0.75
-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
-drag_scalar = 0.75
-pitch_scalar = 1
-max_on_ground_position = 1
-flaps-position.0 = 0, -1, 0
-flaps-position.1 = 20, 215, 0.5, 0.5
diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/panel/PANEL.CFG b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/panel/PANEL.CFG
deleted file mode 100644
index b5e9e8d..0000000
--- a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/panel/PANEL.CFG
+++ /dev/null
@@ -1,59 +0,0 @@
-// Panel Configuration File
-// TFDi Design MD-11
-
-[VCockpit01]
-size_mm=2048,2048
-visible=1
-pixel_size=2048,2048
-texture=vc1
-background_color=0,0,0
-htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=Core, 0,0,509,510
-htmlgauge01=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU1,0,0,508,508
-htmlgauge02=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU2,514,0,510,510
-htmlgauge03=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU3,1027,0,510,510
-htmlgauge04=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU4,1539,0,510,508
-htmlgauge05=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU5,0,513,511,509
-htmlgauge06=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU6,513,512,510,511
-htmlgauge07=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=LMCDU, 0,1050,666,574
-htmlgauge08=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=RMCDU,678,1050,666,574
-htmlgauge09=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=CMCDU,1353,1050,666,574
-htmlgauge10=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=ISFD,1032,519,544,505
-//KH new gauge
-htmlgauge11=WasmInstrument/WasmInstrument.html?wasm_module=load-manager.wasm&wasm_gauge=Load_Manager,0,0,509,510
-
-[VIEWS]
-VIEW_FORWARD_DIR=2.000, 0.000, 0.000
-
-[Color]
-Day=255,255,255
-Night=255,255,255
-Luminous=201,64,64
-
-[Vcockpit02]
-Background_color=0,0,0 
-size_mm=1024,1024
-visible=1
-pixel_size=1024,1024
-texture=vc2
-
-htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=AFS,3,0,1015,185
-htmlgauge01=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=FUEL,4,200,1016,196
-//above should actually be 3,192,1018,199 - moved due to visual offset
-
-[Vcockpit03]
-Background_color=0,0,0 
-size_mm=1024,1024
-visible=1
-pixel_size=1024,1024
-texture=RADIOS_XPNDR
-
-htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=RADIOS_XPNDR,0,5,1019,295
-
-[VCockpit04]
-Background_color=0,0,0
-size_mm=1536,1024
-visible=1
-pixel_size=1536,1024
-texture=EFB
-
-htmlgauge00=aircraft_efb/KH_TFDi_MD11_efb/efb.html,0,0,1536,1024
\ No newline at end of file
diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/panel/PANEL.CFG b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/panel/PANEL.CFG
deleted file mode 100644
index b5e9e8d..0000000
--- a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/panel/PANEL.CFG
+++ /dev/null
@@ -1,59 +0,0 @@
-// Panel Configuration File
-// TFDi Design MD-11
-
-[VCockpit01]
-size_mm=2048,2048
-visible=1
-pixel_size=2048,2048
-texture=vc1
-background_color=0,0,0
-htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=Core, 0,0,509,510
-htmlgauge01=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU1,0,0,508,508
-htmlgauge02=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU2,514,0,510,510
-htmlgauge03=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU3,1027,0,510,510
-htmlgauge04=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU4,1539,0,510,508
-htmlgauge05=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU5,0,513,511,509
-htmlgauge06=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU6,513,512,510,511
-htmlgauge07=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=LMCDU, 0,1050,666,574
-htmlgauge08=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=RMCDU,678,1050,666,574
-htmlgauge09=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=CMCDU,1353,1050,666,574
-htmlgauge10=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=ISFD,1032,519,544,505
-//KH new gauge
-htmlgauge11=WasmInstrument/WasmInstrument.html?wasm_module=load-manager.wasm&wasm_gauge=Load_Manager,0,0,509,510
-
-[VIEWS]
-VIEW_FORWARD_DIR=2.000, 0.000, 0.000
-
-[Color]
-Day=255,255,255
-Night=255,255,255
-Luminous=201,64,64
-
-[Vcockpit02]
-Background_color=0,0,0 
-size_mm=1024,1024
-visible=1
-pixel_size=1024,1024
-texture=vc2
-
-htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=AFS,3,0,1015,185
-htmlgauge01=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=FUEL,4,200,1016,196
-//above should actually be 3,192,1018,199 - moved due to visual offset
-
-[Vcockpit03]
-Background_color=0,0,0 
-size_mm=1024,1024
-visible=1
-pixel_size=1024,1024
-texture=RADIOS_XPNDR
-
-htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=RADIOS_XPNDR,0,5,1019,295
-
-[VCockpit04]
-Background_color=0,0,0
-size_mm=1536,1024
-visible=1
-pixel_size=1536,1024
-texture=EFB
-
-htmlgauge00=aircraft_efb/KH_TFDi_MD11_efb/efb.html,0,0,1536,1024
\ 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
deleted file mode 100644
index 55c413d..0000000
--- a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_PW/flight_model.cfg
+++ /dev/null
@@ -1,406 +0,0 @@
-//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
-//KH START Empty default
-station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
-station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
-station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
-station_load.3=760, 66.0, 0.0, 4.0, Cabin crew 1, 0
-station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 0
-station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 0
-station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 0
-station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 0
-station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 0
-station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 0
-station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 0
-station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 0
-station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 0
-station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 0
-station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 0
-station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 0
-station_load.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0
-station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 0
-station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 0
-station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0
-station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0
-//KH END
-
-[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
-//KH From 5.00, -2.00, -3.00, 0.00, 10.00
-LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00
-//KH From 5.00, 2.00, -3.00, 0.00, 10.0
-RightAux = 5.00, 2.00, -3.00, 1917.00, 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
-
-[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
-drag_scalar = 0.75
-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
-drag_scalar = 0.75
-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/panel/PANEL.CFG b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_PW/panel/PANEL.CFG
deleted file mode 100644
index b5e9e8d..0000000
--- a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_PW/panel/PANEL.CFG
+++ /dev/null
@@ -1,59 +0,0 @@
-// Panel Configuration File
-// TFDi Design MD-11
-
-[VCockpit01]
-size_mm=2048,2048
-visible=1
-pixel_size=2048,2048
-texture=vc1
-background_color=0,0,0
-htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=Core, 0,0,509,510
-htmlgauge01=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU1,0,0,508,508
-htmlgauge02=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU2,514,0,510,510
-htmlgauge03=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU3,1027,0,510,510
-htmlgauge04=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU4,1539,0,510,508
-htmlgauge05=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU5,0,513,511,509
-htmlgauge06=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU6,513,512,510,511
-htmlgauge07=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=LMCDU, 0,1050,666,574
-htmlgauge08=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=RMCDU,678,1050,666,574
-htmlgauge09=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=CMCDU,1353,1050,666,574
-htmlgauge10=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=ISFD,1032,519,544,505
-//KH new gauge
-htmlgauge11=WasmInstrument/WasmInstrument.html?wasm_module=load-manager.wasm&wasm_gauge=Load_Manager,0,0,509,510
-
-[VIEWS]
-VIEW_FORWARD_DIR=2.000, 0.000, 0.000
-
-[Color]
-Day=255,255,255
-Night=255,255,255
-Luminous=201,64,64
-
-[Vcockpit02]
-Background_color=0,0,0 
-size_mm=1024,1024
-visible=1
-pixel_size=1024,1024
-texture=vc2
-
-htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=AFS,3,0,1015,185
-htmlgauge01=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=FUEL,4,200,1016,196
-//above should actually be 3,192,1018,199 - moved due to visual offset
-
-[Vcockpit03]
-Background_color=0,0,0 
-size_mm=1024,1024
-visible=1
-pixel_size=1024,1024
-texture=RADIOS_XPNDR
-
-htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=RADIOS_XPNDR,0,5,1019,295
-
-[VCockpit04]
-Background_color=0,0,0
-size_mm=1536,1024
-visible=1
-pixel_size=1536,1024
-texture=EFB
-
-htmlgauge00=aircraft_efb/KH_TFDi_MD11_efb/efb.html,0,0,1536,1024
\ No newline at end of file