[fltsim.0]
title=Leo
sim=Leo
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
prop_anim_ratio=-1,15
atc_id_color=
atc_id=N8092U
ui_manufacturer=Leo Da
ui_type=LeoHeli
ui_variation=1
description=Вертолет Леонардо Да Винчи
 [General]
atc_type=Leo
atc_model=Leo
performance


[WEIGHT_AND_BALANCE]
max_gross_weight = 1370                          // (pounds)
empty_weight = 862.4                             // (pounds)

reference_datum_position     =  8.33,  0.0, 0.0   // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = -8.73,  0.0, 0.0   // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 = "160, -6.6,  0.89, 0.0, Пилот"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "160, -6.6, -0.78, 0.0, Пассажир"      // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)


;Moments of Inertia
empty_weight_pitch_MOI   =  6000
empty_weight_roll_MOI    =  4000
empty_weight_yaw_MOI     = 10000
empty_weight_coupled_MOI =     0

[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, 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
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=skid>
        //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=3,   -3.74,  -3.13, -4.00, 1600, 0, 0, 0.0, 0.39, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0
point.1=3,   -3.74,   3.13, -4.00, 1600, 0, 0, 0.0, 0.39, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0
point.2=3,  -10.00,  -3.13, -3.70, 1600, 0, 0, 0.0, 0.28, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0
point.3=3,  -10.00,   3.13, -3.70, 1600, 0, 0, 0.0, 0.28, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0
point.4=2,   -8.50, -11.80,  5.30,  100, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5, 0.0, 0.0
point.5=2,   -8.50,  11.80,  5.30,  100, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6, 0.0, 0.0
point.6=2,    3.00,   0.00,  5.30,  100, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4, 0.0, 0.0
point.7=2,  -23.00,   0.00, -0.60,  300, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9, 0.0, 0.0

static_pitch = 0.2
static_cg_height = 3.58

[brakes]
parking_brake = 0       //Parking brake available
toe_brakes_scale = 0.0  //Brake scalar

[hydraulic_system]
normal_pressure = 0.0    //PSI

[Views]
eyepoint = -7.453, .718, 1.358

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -5.60, -1.88, -1.60,  fx_navred ,
light.1 = 3, -5.60,  1.88, -1.60,  fx_navgre ,
light.2 = 3, -23.39,  0.40, 1.95,  fx_navwhi ,
light.3 = 1, -18.90,  0.04, 2.58,  fx_beacon ,
light.4 = 5,  -2.85,  0.20, -1.65,  fx_landing ,
light.5 = 5,  -2.85,  -0.20, -1.65,  fx_landing ,
light.6 = 4,   -7.75,  0.30, 1.50,  fx_vclighth ,

[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

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced --  1/2 and 1/8 respectively.
//NOTE: These map -- cyclic (fore/aft), cyclic (left/right), and anti-torque
elevator = 100,  180
aileron  = 200, 1000
rudder   = 200, 1000

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

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt

[fuel]
LeftMain  = -8.85, -0.5, 0.0, 19.2, 0.0         //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -8.85,  0.5, 0.0, 10.5, 0.0         //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=0

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -8.5, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0                           //Fuel flow scalar
min_throttle_limit =  0.0;                      //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 90.0                     //Cubic inches per cylinder
compression_ratio= 8.5                          //Compression ratio
number_of_cylinders=4                           //Number of cylinders
max_rated_rpm= 2700                             //Max rated RPM
max_rated_hp= 180                               //Max rated HP
fuel_metering_type= 1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3                  //Starter torque factor
turbocharged= 0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0                                //Max design manifold pressure, (inHg)
min_design_mp= 0                                //Min design manifold pressure, (inHg)
critical_altitude= 0                            //Altitude -- 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                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0                  //Multiplier on manifold pressure due -- 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

[Reference Speeds]
cruise_speed            = 90.0                 //Knots True (KTAS)
max_indicated_speed     = 102                  //Red line (KIAS)

[autopilot]
autopilot_available= 0
flight_director_available= 0

[yaw_string]
yaw_string_available=1

[Helicopter]
reference_length       = 21.58   
reference_frontal_area = 17.7
reference_side_area    = 44.5
side_aero_center       = -12.5
right_trim_scalar      = 1.0
correlator_available   = 1
governed_pct_rpm_ref   = 1.04
governor_pid = 0.4, 0, 0.1, 0, 0.2
rotor_brake_scalar     = 1.0
torque_scalar          = 1.0
cyclic_roll_control_scalar  =1.0
cyclic_pitch_control_scalar =1.0
pedal_control_scalar        =1.0
collective_on_rotor_torque_scalar = 1.0

[fuselage_aerodynamics]
drag_force_cf      = 0.55
side_drag_force_cf = 10.0
pitch_damp_cf      = -2.0
roll_damp_cf       = -2.0
yaw_damp_cf        = -0.1
yaw_stability_cf   = 0.27

[MainRotor]
Position = -8.5, 0, 4.91                       //Longitudinal, Lateral, Vertical feet from datum
Radius   = 12.583                               //feet
max_disc_angle = 5.0
RatedRpm = 510
Number_of_blades = 2
Weight_per_blade = 26.0
Weight_to_moi_factor = 0.58
inflow_vel_reference = 34.0

[SecondaryRotor]
Position = -22.8, -0.74, 1.8                    //Longitudinal, Lateral, Vertical feet from datum
TailRotor = 1
Radius   = 1.75                                 //feet