[fltsim.0]
title=L200D Morava OK-RHJ
sim=morava
model=
panel=
sound=
texture= 
kb_checklists=checklist
ui_manufacturer=Let
ui_type=L200D
ui_variation=OK-RHJ
atc_id=OK-RHJ
prop_anim_ratio=-1.90
description=Let L-200D\n CREW=1\n Passengers=4\n Engine=2 x Walter M337 piston engines, 157kW

[fltsim.1]
title=L200D Morava OK-PRO
sim=morava
model=
panel=
sound=
texture=pro 
kb_checklists=checklist
ui_manufacturer=Let
ui_type=L200D
ui_variation=OK-PRO
atc_id=OK-PRO
prop_anim_ratio=-1.90
description=Let L-200D\n CREW=1\n Passengers=4\n Engine=2 x Walter M337 piston engines, 157kW


[General]
atc_type=let
atc_model=200D
editable=1
performance=WEIGHTS\n    MTOW \t1950 kg\n    \n DIMENSIONS\n    Wingspan \t12.3 m\n    Length \t8.6 m\n    Height \t2.25 m\n    Wing area \t17.3 m2\n PERFORMANCE\n    Cruise speed \t200-230 km\/h\n    Ceiling \t6200 m\n    Range \t1800 km\n \n \n \n \n


[WEIGHT_AND_BALANCE]
max_gross_weight = 4300
empty_weight = 2810

reference_datum_position = 0, 0, 0
empty_weight_CG_position  = -0.70, 0, 1.46

CG_forward_limit = 1
CG_aft_limit = -1

max_number_of_stations = 6
station_load.0 = "170, 0, -1.20, 3, pilot"
station_load.1 = "170, 0, 1.20, 3, passeger front" 
station_load.2 = "170, -4, -1.20, 3, passeger rear L" 
station_load.3 = "147, -4, 0.00, 3, passeger rear C" 
station_load.4 = "170, -4, 1.20, 3, passeger rear R"
station_load.5 = "0, -6, 0, 1, baggage" 

empty_weight_pitch_MOI = 5000
empty_weight_roll_MOI = 2718
empty_weight_yaw_MOI =  5000
empty_weight_coupled_MOI = 0


[flight_tuning]
cruise_lift_scalar     = 1.1
parasite_drag_scalar   = 1.2
induced_drag_scalar    = 1.3
elevator_effectiveness = 0.6
aileron_effectiveness  = 0.9
rudder_effectiveness   = 1.0
pitch_stability        = 2.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.5
aileron_trim_effectiveness  = 0.7
rudder_trim_effectiveness   = 0.7

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 6.25, -5.64, 0.91                      //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 6.25,  5.64, 0.91                      //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.40                           //Fuel flow scalar
min_throttle_limit=0.000000

[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 87                     //Cubic inches per cylinder
compression_ratio= 6.3                          //Compression ratio
number_of_cylinders= 6                          //Number of cylinders
max_rated_rpm= 2750.0                           //Max rated RPM
max_rated_hp= 210.0                             //Max rated HP
fuel_metering_type= 0                           //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3                  //Starter torque factor
turbocharged= 1                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 16.0                              //Max design manifold pressure, (inHg)
min_design_mp= 1.0                              //Min design manifold pressure, (inHg)
critical_altitude= 15000.0                          //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0.0                  //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0.0                //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0                   //Scalar on idle RPM friction

[propeller]
thrust_scalar = 1.0                             //Propeller thrust scalar
propeller_type= 0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 5.70                         //Propeller Diameter, (feet)
propeller_blades= 3                             //Number of propeller blades
propeller_moi= 3.0                              //Propeller moment of inertia 6.9
beta_max= 45.0                                  //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 15.2                                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1100.0                             //Miminum governed RPM
prop_tc= 0.08                                    //Prop time-constant
gear_reduction_ratio= 1.0                       //Propeller gear reduction ratio
fixed_pitch_beta= 0.0                           //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80.0                    //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 0                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 1                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0                      //Minimum RPM for prop feathering
beta_feather= 82.5                              //Feathering pitch angle (degrees)
power_absorbed_cf= 0.9                          //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available= 0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta= 0.0                     //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0                       //Minimum pitch angle in reverse, (degrees)

[contact_points]
        //0  Class
        //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)

point.0 = 1,  8.7,  0.00, -3.55, 1600, 0, 0.633, 40, 0.42, 2.5, 0.80, 3.0, 5.0, 0, 152, 180
point.1 = 1, -1.86, -5.83, -3.2, 1600, 1, 0.886,  0, 0.50, 2.5, 0.85, 4.1, 4.3, 2, 152, 200
point.2 = 1, -1.86,  5.83, -3.2, 1600, 2, 0.886,  0, 0.50, 2.5, 0.85, 4.3, 4.1, 3, 152, 200

point.3=  2, -17.62, -6.37,  0.96,  800, 0, 0, 0, 0, 0, 0, 0, 0, 5,    //derive G
point.4=  2, -17.62,  6.37,  0.96,  800, 0, 0, 0, 0, 0, 0, 0, 0, 6,    //derive D
point.5=  2,  0.35,  -19.76,  0.66,  800, 0, 0, 0, 0, 0, 0, 0, 0, 9,    //bidonG
point.6=  2,  0.35,   19.76,  0.66,  800, 0, 0, 0, 0, 0, 0, 0, 0, 4,    //bidonD
point.7=  2,  6.46,   -5.64,  2.00,  800, 0, 0, 0, 0, 0, 0, 0, 0, 4,    //heliceG
point.8=  2,  6.46,    5.64,  2.00,  800, 0, 0, 0, 0, 0, 0, 0, 0, 4,    //heliceD
point.9=  2,  8.61,   0.00, 0.55,  800, 0, 0, 0, 0, 0, 0, 0, 0, 4,    //av fuselage



static_pitch = 0.0
static_cg_height = 3.0815
gear_system_type=1


[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.41                                 // 0.0 .. 1.0
extending-time   = 10                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 15                                   // degrees
flaps-position.2 = 30                                   // degrees
damaging-speed   = 115                                  // KIAS
blowout-speed    = 135                                  // KIAS
system_type = 1                                         //Hydraulic


[electrical]
//BusType, MaxAmpLoad, MinVoltage
//BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)

max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0

autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 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
starter2           = 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


[hydraulic_system]
normal_pressure = 1000.0
electric_pumps  = 0
engine_map      = 1,1,0,0




[pitot_static]
vertical_speed_time_constant = 0.7              //1.00 Increasing this value will cause a more instantaneous reaction in the VSI

[exits]
number_of_exits = 2
exit_rate.0 = 0.4

[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

[Views]
eyepoint = -0.45, -1.00, 3.60    //Longitudinal, Lateral, Vertical (feet)

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3,  0.410, -20.22,  1.53, fx_navred     //rouge gauche
light.1 = 3,  0.410,  20.22,  1.53, fx_navgre     //vert droit
light.2 = 1, -0.433,  0.00,  4.68, fx_beaconm      //beacon sup
light.3 = 2,  0.30,  -20.22,  1.53, fx_strobe     //strobe gauche
light.4 = 2,  0.30,   20.22,  1.53, fx_strobe     //strobe droit
light.5 = 1,  -6.82,   0.00,  0.141, fx_beaconm    //beacon inf
light.6 = 4,   -0.80,   0.0,  1.00, fx_vclight    //VC light
light.7 = 4,   -0.20,   0.0,  2.00, fx_vclight    //VC light
light.8 = 3,   -18.55,   0.0,  1.50, fx_navwhi

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the increment is reduced to  1/2 and 1/8 respectively.
elevator = 100, 250
aileron  = 100, 250
rudder   = 100, 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

[fuel]
LeftMain  = -1.00, -4.11, 0.21, 30.37, 0.50     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -1.00,  4.11, 0.21, 30.37, 0.50     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Lefttip  = -1.0, -19.50, 1.80, 25.09, 0.0
Righttip = -1.0,  19.50, 1.80, 25.09, 0.0
fuel_type = 1
number_of_tank_selectors = 2                    
electric_pump=1

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

[airplane_geometry]
wing_area               = 186.21                 //Square feet
wing_span               = 40.35                  //Feet
wing_root_chord         = 5.41                   //Feet
wing_dihedral           = 6.1                   //Degrees
wing_incidence          = 1.8                   //Degrees
wing_twist              = -1.0                  //Degrees
oswald_efficiency_factor= 0.7                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 0.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = 1.5                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 10.76                  //Square feet
htail_span              = 11.68                  //Feet
htail_pos_lon           = -16.40                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.5                   //Degrees
htail_sweep             = 0.0                   //Degrees, horizontal tail leading edge
vtail_area              = 10.76                  //Square feet
vtail_span              = 10.7                  //Feet, tip to body
vtail_sweep             = 0.0                   //Degrees, vertical tail leading edge
vtail_pos_lon           =-16.40                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 3.1                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 16.14                  //Square feet
aileron_area            = 4.84                  //Square feet
rudder_area             = 10.76                  //Square feet
elevator_up_limit       = 23.0                  //Degrees
elevator_down_limit     = 15.5                  //Degrees
aileron_up_limit        = 18.0                  //Degrees
aileron_down_limit      = 18.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 25.0                  //Degrees
spoiler_limit           = 0.0                   //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate


[Reference Speeds]
flaps_up_stall_speed    = 68.0                  //Knots True (KTAS)
full_flaps_stall_speed  = 60.0                  //Knots True (KTAS)
cruise_speed            = 145.0                 //Knots True (KTAS)
max_indicated_speed=190.000000

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.000000
use_no_default_pitch=1
use_no_default_bank=1


crash_duration2=2500000                 ; in microseconds
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
default_pitch_mode=0
default_bank_mode=0

[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5#
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1#
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[brakes]
toe_brakes_scale=0.700000
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=31.512679
flap_limit_idle=31.512679

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=1000.000000


[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0