; Localized	06/01/2009 DZIES design projekt  FF demo
[fltsim.0]
title=Lisunov Li-2
sim=Lisunov_Li_2
model=""
panel=""
sound=""
texture=""
kb_checklists=Lisunov_Li_2_check
kb_reference=Lisunov_Li_2_ref
atc_id=N 01
ui_manufacturer=Lisunov
ui_type=Li-2 (DZIES_demo)
ui_variation=Lizunov_Li_2 FF
ui_typerole=Двухмоторный винтовой
ui_createdby=Projekt Fresh Flight
description="Lizunov_Li_2" Демо-версия от DZIES design (подробности на сайте www.dzies.ru)


[General]
atc_type=Lizunov
atc_model=Li_2
editable=0
performance= "Крейсерская скорость: 240 км/ч\n\nДвигатели: два АШ-62 2x1000 л.с\n\nМаксимальная дальность: 2500 км\n\nМаксимальная высота полета: 5600 мn\nCruise speed\n240 km/hr\n\nEngines\nASh-62IR 2x1000 hp\n\nMaximum range\n2,500 km\n\nService ceiling\n5600 mn\nинформация на www.dzies.ru"
Category=airplane

[CameraDefinition.0]
Title=Хвост
Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description=Вид с хвостовой части самолета
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.75
ShowWeather=Yes
InitialXyz=0, -0.7, -10.0
InitialPbh=10, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title=Правое сиденье
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Origin=Virtual Cockpit
MomentumEffect=Yes
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=YES
AllowZoom=TRUE
InitialZoom=0.75
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.82, 0.05, 0.0
InitialPbh=7, 0, 0

[CameraDefinition.2]
Title=Левое крыло
Guid={f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description=Вид на кабину с кончика левого крыла
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=-15.8, 1.3, 0.0
InitialPbh=8, 0, 90
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=No
ClipMo

[CameraDefinition.001]
Title=Блок радиосвязи
Guid={195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin=Virtual Cockpit
MomentumEffect=No
SnapPbhAdjust=None
SnapPbhReturn=False
PanPbhAdjust=None
PanPbhReturn=False
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.45, -0.1, 0.2
InitialPbh=-65, 0, 0

[CameraDefinition.002]
Title=Панель управления двигателем
Guid={195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
Origin=Virtual Cockpit
MomentumEffect=No
SnapPbhAdjust=None
SnapPbhReturn=False
PanPbhAdjust=None
PanPbhReturn=False
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.4
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.45, 0.15, -0.4
InitialPbh=44, 0, 0de=Minimum


[WEIGHT_AND_BALANCE]
max_gross_weight=26200                         // (pounds)
empty_weight=16145                         // (pounds)

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=50

station_load.0=170.0,   -5.4,  -2.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.1=170.0,   -5.4,   2.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.2=0.0,  -14.2,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.3=0.0,  -17.4,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.4=0.0,  -20.7,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.5=0.0,  -23.9,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.6=0.0,  -27.2,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.7=0.0,  -30.4,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.8=0.0,  -33.7,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.9=340.0,  -36.9,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.10=500.0,  -23.8,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.11=100.0,  -45.5,   0.0,   0.0   //Weight, Lat, Lon, Vert Position

station_name.0=Пилот
station_name.1=2-й пилот
station_name.2=1 ряд сидений
station_name.3=2 ряд сидений
station_name.4=3 ряд сидений
station_name.5=4 ряд сидений
station_name.6=5 ряд сидений
station_name.7=6 ряд сидений
station_name.8=7 ряд сидений
station_name.9=8 ряд сидений
station_name.10=Баг. отсек (П)
station_name.11=Груз. отсек (З)

;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=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
p_factor_on_yaw=0.5
torque_on_roll=1.0
gyro_precession_on_yaw=1.0
gyro_precession_on_pitch=1.0

[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.5                                  // 0.0 .. 1.0
extending-time=7                                    // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=15                                   // degrees
flaps-position.2=30                                   // degrees
flaps-position.3=45                                   // degrees                                // degrees
damaging-speed=140                                  // KIAS
blowout-speed=175                                  // KIAS
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
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=202.5                   //Cubic inches per cylinder
compression_ratio=6.4                          //Compression ratio
number_of_cylinders=9                          //Number of cylinders
max_rated_rpm=2350                             //Max rated RPM
max_rated_hp=1000                              //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=6.500                        //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
magneto_order_left_right_both=1		//sets the order of the magneto switch direction

[propeller]
thrust_scalar=1.0                             //Propeller thrust scalar
propeller_type=0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=11.81                       //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=1.6                     //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,  60.0, 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=0.7  //Brake scalar
differential_braking_scale=1.0        //Delta on the amount of brake when the rudder pedals deflected
auto_brakes=0

[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, -1.4, 3.26

[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3,  -27.20, -46.30,  0.65, fx_navredm ,
light.1=3,  -27.20,  46.30,  0.65, fx_navgrem ,
light.2=3,  -64.00,   0.00,  2.72, fx_navwhi ,
light.3=1,  -36.80,   0.00,  6.25, fx_beaconh ,
light.4=4,  -6.50,   0.00,  4.80, fx_vclighth,
light.5=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

[altimeters]
altimeter.0=1
altimeter.1=1

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

[vacuum_system]
max_pressure=5.0    //PSI
vacuum_type=1   //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
engine_map=1,1

[pneumatic_system]
max_pressure=0.000000

[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.0    //Scalar on heat effectiveness, 0 = not available

[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)
LeftAux=-22.55,  -0.4, -3.0, 202.0,  0.0 
RightMain=-22.55,   6.7, -3.0, 202.0,  0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=-22.55,   0.4, -3.0, 202.0,  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=0.60                  //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=4.0               //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=2.0               //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up=-1.5               //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down=-1.5               //Design G load tolerance (negative, flaps down)
load_safety_factor=1.5               //Design G load safety factor


[Reference Speeds]
flaps_up_stall_speed=67.5                  //Knots True (KTAS)
full_flaps_stall_speed=61.5                  //Knots True (KTAS)
cruise_speed=95.0                  //Knots True (KTAS)
max_indicated_speed=224                   //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

[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

[deice_system]
structural_deice_type=0     //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots