[fltsim.0]
title=Douglas DC10 THY
sim=dc10
model=
panel=
sound=
texture=
checklists=
atc_id=TCJAV
atc_id_color=0xffffffff
atc_airline=TACA
atc_flight_number=4191
ui_manufacturer=McDonnell-Douglas/Boeing
ui_type=DC-10
ui_variation=Turkish Airlines TC-JAV
description=McDonnell Douglas DC-10 Turkish Airlines THY\nRepainted by Salim Unuver\n

[General]
atc_type=MCDONNELDOUGLAS
atc_model=DC10
editable=1
performance=Enter your performance information here.

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI

[WEIGHT_AND_BALANCE]
max_gross_weight = 138500.000
empty_weight = 100792.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations =50

station_load.0 =0.000000,0.000000,0.000000,0.000000

;Moments of Inertia
empty_weight_pitch_MOI  = 3172439.000
empty_weight_roll_MOI   = 2262183.000
empty_weight_yaw_MOI    = 3337024.000
empty_weight_coupled_MOI        = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar     =1.000
parasite_drag_scalar   =1.000
induced_drag_scalar    =1.000
elevator_effectiveness =1.000
aileron_effectiveness  =1.000
rudder_effectiveness   =1.000
pitch_stability        =1.000
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[GeneralEngineData]
engine_type=1
Engine.0=10.66,-26.83,-5.50
Engine.1=-69.50,0.00,17.33
Engine.2=10.66,26.83,-5.50
fuel_flow_scalar=1.0

[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 19.600
rated_N2_rpm = 29920.000
static_thrust = 10134.000
afterburner_available = 0
reverser_available = 1

[jet_engine]
thrust_scalar =1.000

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 10, 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 20, 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 17.0
light_nav          = 0, 5 , 17.0
light_beacon       = 0, 5 , 17.0
light_landing      = 0, 5 , 17.0
light_taxi         = 0, 5 , 17.0
light_strobe       = 0, 5 , 17.0
light_panel        = 0, 5 , 17.0

        //0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
        //1  Longitudinal Position        (feet)
        //2  Lateral Position             (feet)
        //3  Vertical Position            (feet)
        //4  Impact Damage Threshold      (Feet Per Minute)
        //5  Brake Map                    (0=None, 1=Left, 2=Right)
        //6  Wheel Radius                 (feet)
        //7  Steer Angle                  (degrees)
        //8  Static Compression           (feet)  (0 if rigid)
        //9  Max/Static Compression Ratio
        //10 Damping Ratio                (0=Undamped, 1=Critically Damped)
        //11 Extension Time               (seconds)
        //12 Retraction Time              (seconds)
        //13 Sound Type
        //14 Airspeed limit for retraction     (KIAS)
        //15 Airspeed that gear gets damage at (KIAS)
        
[contact_points]
point.0= 1.000, 57.786, 0.000, -15.380, 1181.100, 0.000, 2.042, 70.920, 0.800, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000
point.1= 1.000, -16.700, -19.000, -16.650, 1574.800, 1.000, 2.442, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000
point.2= 1.000, -16.700, 19.000, -16.650, 1574.800, 2.000, 2.442, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000
point.3= 2.000, -42.600, -82.750, 3.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -42.600, 82.750, 3.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -98.360, 0.000, 5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 90.400, 0.000, -0.700, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

max_number_of_points = 21

static_pitch= -1.200
static_cg_height= 16.50

[Views]
eyepoint=76.8, -1.41, 6.00   //(feet) longitudinal, lateral, vertical distance from reference datum

[Radios]
// Radio Type = availiable, standby frequency, has glide slope.
Audio.1       = 1
Com.1         = 1, 1
Com.2         = 1, 1
Nav.1         = 1, 1, 1
Nav.2         = 1, 1, 0
Adf.1         = 1
Transponder.1 = 1
Marker.1      = 1

[LIGHTS] 
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -42.60, -82.75, 2.50, fx_navredm ,
light.1=3, -42.60, 82.75, 2.50, fx_navgrem ,
light.2=3, -50.35, 82.70, 1.65, fx_navwhih ,
light.3=2, -42.60, -82.75, 2.50, fx_strobeh ,
light.4=2, -42.60, 82.75, 2.50, fx_strobeh ,
light.5=1, -25.65, 0.00, -7.35, fx_beaconb ,
light.6=1, 1.20, 0.00, 12.80, fx_beaconh , 
light.7=4, 80.41, 0.00, 3.50, fx_vclight ,
light.8=3, -50.35, -82.70, 1.65, fx_navwhih ,
light.9=2, -50.35, -82.70, 1.65, fx_strobeh ,
light.10=2, -50.35, 82.70, 1.65, fx_strobeh ,

[keyboard_response]      
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator = 150, 250   
aileron  = 150, 250
rudder   = 150, 250

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8;

[fuel]
Center1 = 0.000, 0.000, 0.000, 2313.000, 0.000
LeftMain  = -3.000, -19.000, 0.000, 1500.000, 0.000
RightMain = -3.000, 19.000, 0.000, 1500.000, 0.000
fuel_type = 2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    

[airplane_geometry]
wing_area               = 1137.000
wing_span               = 125.000
wing_root_chord         = 18.000
wing_dihedral           = 6.200
wing_incidence          = 1.000
wing_twist              = -0.500
oswald_efficiency_factor= 0.750
wing_winglets_flag      = 0
wing_sweep              = 25.000
wing_pos_apex_lon       = 8.000
wing_pos_apex_vert      = 0.000
htail_area              = 338.000
htail_span              = 41.700
htail_pos_lon           = -35.000
htail_pos_vert          = 0.000
htail_incidence         = 0.000
htail_sweep             = 30.000
vtail_area              = 224.000
vtail_span              = 20.000
vtail_sweep             = 35.000
vtail_pos_lon           = -35.800
vtail_pos_vert          = 5.800
elevator_area           = 70.500
aileron_area            = 26.900
rudder_area             = 56.200
elevator_up_limit       = 22.500
elevator_down_limit     = 19.500
aileron_up_limit        = 20.000
aileron_down_limit      = 20.000
rudder_limit            = 26.000
elevator_trim_limit     = 20.000
spoiler_limit           = 60.000
spoilerons_available    = 1
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000

[Reference Speeds]
flaps_up_stall_speed    = 142.000
full_flaps_stall_speed  = 113.000
cruise_speed            = 477.000

[forcefeedback]
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 25.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.700
drag_scalar= 0.700
pitch_scalar= 0.700
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 5.000, 0.000
flaps-position.4= 10.000, 0.000
flaps-position.5= 15.000, 0.000
flaps-position.6= 25.000, 0.000
flaps-position.7= 30.000, 0.000
flaps-position.8= 40.000, 0.000

[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 10.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000

[Flaps.2]
type= 2
span-outboard= 0.800
extending-time= 15.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.500, 0.000
flaps-position.2= 1.000, 0.000