[fltsim.0]
title=Li-2
sim=Douglas_DC3
model=
panel=
sound=
texture=
atc_id=63888
atc_airline=Aeroflot
atc_flight_number=63888
ui_manufacturer=Lisunov
ui_type="LI2"
ui_variation="AEROFLOT"
description=" Lisunov LI2 AEROFLOT "

[General]
atc_type=Lisunov 
atc_model=LI2
editable=1
performance="Cruise speed\n240 km/hr\n\nEngines\nASh-62IR 2x1000 hp\n\nMaximum range\n2,500 km\n\nService ceiling\n5600 m\n\nFuel capacity\n1640 kg\n\nEmpty weight\n7,820 kg\n\nMaximum gross weight\n10,700 kg\n\nLength\n19.647 m\n\nWingspan\n28.813 m\n\nHeight\n7.093 m\n\nMaximum seating\n21\n\nUseful load\n1995 kg"
Category=airplane

[WEIGHT_AND_BALANCE]
max_gross_weight = 23600                         // (pounds) =10700 kg
empty_weight     = 16000                         // (pounds) = 7260 kg

reference_datum_position     =   19.25, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -20.90, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations =21

station_load.0  = "485.0,   -5.4,   0.0,   0.0, Flight Crew (3)"    //Weight, Lat, Lon, Vert Position
station_load.1  = "485.0,  -17.4,   0.0,   0.0, Passenger Row 1"    //Weight, Lat, Lon, Vert Position
station_load.2  = "485.0,  -20.7,   0.0,   0.0, Passenger Row 2"    //Weight, Lat, Lon, Vert Position
station_load.3  = "485.0,  -23.9,   0.0,   0.0, Passenger Row 3"    //Weight, Lat, Lon, Vert Position
station_load.4  = "485.0,  -27.2,   0.0,   0.0, Passenger Row 4"    //Weight, Lat, Lon, Vert Position
station_load.5  = "485.0,  -30.4,   0.0,   0.0, Passenger Row 5"    //Weight, Lat, Lon, Vert Position
station_load.6  = "485.0,  -33.7,   0.0,   0.0, Passenger Row 6"    //Weight, Lat, Lon, Vert Position
station_load.7  = "485.0,  -36.9,   0.0,   0.0, Passenger Row 7"    //Weight, Lat, Lon, Vert Position
station_load.8  = "330.0,  -12.0,   0.0,   0.0, Forward Baggage"    //Weight, Lat, Lon, Vert Position
station_load.9  = "220.0,  -45.5,   0.0,   0.0, Rear Cargo"         //Weight, Lat, Lon, Vert Position

;Moments of Inertia
empty_weight_pitch_MOI   =  69699.03  
empty_weight_roll_MOI    =  61179.10  
empty_weight_yaw_MOI     = 131797.97 
empty_weight_coupled_MOI = 0.0         

[flight_tuning]
cruise_lift_scalar     = 1.1
parasite_drag_scalar   = 1.2
induced_drag_scalar    = 1.2
elevator_effectiveness = 0.8
aileron_effectiveness  = 0.8
rudder_effectiveness   = 0.8
pitch_stability        = 1.1
roll_stability         = 1.8
yaw_stability          = 1.2
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0
p_factor_on_yaw          = 0.4
torque_on_roll           = 0.8
gyro_precession_on_yaw   = 0.8
gyro_precession_on_pitch = 0.8

[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 20                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 15                                  // degrees
flaps-position.2 = 25                                   // degrees
flaps-position.3 = 35                                   // degrees
flaps-position.4 = 45                                // degrees
damaging-speed   = 140                                  // KIAS
blowout-speed    = 175                                  // KIAS
lift_scalar = 1.8                                       
drag_scalar = 1.8
pitch_scalar= 1.2
system_type = 1                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -9.75, -9.1, -1.8                     //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -9.75,  9.1, -1.8                     //(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
master_ignition_switch = 1                      //Master Ignition Switch

[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 204.4                   //Cubic inches per cylinder
compression_ratio= 6.4                          //Compression ratio
number_of_cylinders=9                          //Number of cylinders
max_rated_rpm= 2200                             //Max rated RPM
max_rated_hp= 1150                            //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= 1                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 41.2                               //Max design manifold pressure, (inHg)
min_design_mp= 5                               //Min design manifold pressure, (inHg)
critical_altitude= 6500                        //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                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 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= 11.80                       //Propeller Diameter, (feet)
propeller_blades= 3                             //Number of propeller blades
propeller_moi= 40.2                             //Propeller moment of inertia
beta_max= 38.0                                  //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 18.0                                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1550                               //Miminum governed RPM
prop_tc= 0.1                                    //Prop time-constant
gear_reduction_ratio= 1.75                     //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= 1                          //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= 800.0                      //Minimum RPM for prop feathering
beta_feather= 88.8                              //Feathering pitch angle (degrees)
power_absorbed_cf= 0.9                          //Coefficient of friction for power absorbed by propeller in feather
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)
feathering_switches = 1                         //Switches which invoke feathering

        //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


[contact_points]
point.0=1,  -56.00,  0.0,   -2.3, 1200.0, 0, 0.60, 180.0, 0.200, 2.5, 0.695,  0.0,  0.0, 0.0,   0.0,   0.0
point.1=1,  -18.55, -9.25, -11.0, 1600.0, 1, 1.35,   0.0, 0.704, 2.5, 0.686,  7.0,  9.0, 7.0, 166.0, 166.0
point.2=1,  -18.55,  9.25, -11.0, 1600.0, 2, 1.35,   0.0, 0.704, 2.5, 0.682,  3.0,  5.0, 7.0, 166.0, 166.0
point.3=2,  -27.00, -46.3,  -0.1,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 5.0, 0.0, 0.0
point.4=2,  -27.00,  46.3,  -0.1,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 6.0, 0.0, 0.0
point.5=2,  -61.00,   0.0,  14.0,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 9.0, 0.0, 0.0
point.6=2,    0.40,   0.0,  -1.2,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 4.0, 0.0, 0.0

static_pitch = 12.76
static_cg_height = 9.9
gear_system_type=1      //Hydraulic
tailwheel_lock = 1 

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  0.0     //Flap angle that activates warning at idle
flap_limit_power   = 16.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.5  //Brake scalar
differential_braking_scale = 1.4        //Delta on the amount of brake when the rudder pedals deflected

[hydraulic_system]
normal_pressure = 732.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[Views]
eyepoint = -6.495, -1.512, 3.217

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3,  -27.20, -46.3,  0.65, fx_navredm ,
light.1 = 3,  -27.20,  46.3,  0.65, fx_navgrem ,
light.2 = 3, -64.00,   0.00,  2.72, fx_navwhi ,
light.3 = 4,  -6.00,   0.00,  1.80, fx_vclight,
light.4 = 4,  -33.00,   0.00,  4.20, fx_vclighth,

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

[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 =200, 1000
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 to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=1,0
direction_indicator.1=2,0

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

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

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

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 100

[fuel]
LeftMain =  -22.55,  -6.7, -3.0, 202.0,  0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=  -22.55,   6.7, -3.0, 202.0,  0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1  =  -22.55,   0.0, -2.7, 200.0,  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 = 2                    
electric_pump=1




[airplane_geometry]
wing_area               = 987.0                 //Square feet
wing_span               = 95.0                  //Feet
wing_root_chord         = 12.85                  //Feet
wing_dihedral           = 5.0                   //Degrees
wing_incidence          = 2.0                   //Degrees
wing_twist              = -1.0                  //Degrees
oswald_efficiency_factor= 0.65                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 14.5                   //Degrees, wing leading edge
wing_pos_apex_lon       = -13.00                //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = -2.7                   //Feet, vertical distance from reference point, positive going up

htail_area              = 95.8                  //Square feet
htail_span              = 28.25                 //Feet
htail_pos_lon           = -52.7                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = -52.7                 //Feet, vertical distance from reference point, positive going up
htail_incidence         = -1.0                   //Degrees
htail_sweep             = 27.0                  //Degrees, horizontal tail leading edge

vtail_area              = 37.9                  //Square feet
vtail_span              = 11.49                 //Feet, tip to body
vtail_sweep             = 50.4                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -51.4                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 6.7                   //Feet, vertical distance from reference point, positive going up

elevator_area           = 83.4                  //Square feet
aileron_area            = 102.8                 //Square feet
rudder_area             = 46.7                  //Square feet
elevator_up_limit       = 30.0                  //Degrees
elevator_down_limit     = 20.0                  //Degrees
aileron_up_limit        = 27.0                  //Degrees
aileron_down_limit      = 18.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 12.0                  //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
auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000
               

[Reference Speeds]
flaps_up_stall_speed    = 67.5                  //Knots True (KTAS)
full_flaps_stall_speed  = 61.5                  //Knots True (KTAS)
cruise_speed            = 130.0                  //Knots True (KTAS)
max_indicated_speed     = 242                   //Red line (KIAS)

[autopilot]
autopilot_available= 1
flight_director_available= 0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
attitude_indicator =1
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 = 0.0
default_bank_mode=2     //Default to Heading Hold
default_pitch_mode=1

[forcefeedback]
ground_bumps_magnitude1=2600            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200            ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000                 ; in microseconds

[stall_warning]
type=1
stick_shaker=0

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


[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0