//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.0_GE 15MAY25

[VERSION]
//KH Bump major
major = 4
minor = 2

[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, 4
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 4
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 4
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 4
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 4
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 4
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 3
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 3
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 3
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 5
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 5
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 5
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, 6
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 6
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 = 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 = 13
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,-1
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33,-1
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,-1
interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,-1
interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,-1
interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,-1
interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,-1

[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 = 280
blowout-speed = 310
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 = 280
blowout-speed = 310
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 = 300
blowout-speed = 330
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 = 300
blowout-speed = 330
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