[fltsim.0]
title=Ilyusin Il-96-300 VC Aeroflot
sim=96M
model=V2
panel=
sound=
texture=Aeroflot
kb_checklists=
kb_reference=
atc_id=96010
atc_airline=
atc_flight_number=96010
atc_heavy=1
ui_manufacturer=Ilyushin
ui_type=Il-96-300
ui_variation=Aeroflot
description=Test Dynamics for 96-300

[General]
atc_type=ILYUSHIN
atc_model=IL96
performance=Ильюшин Ил-96-300 
Category=airplane

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction в VSI
pitot_heat=1.000000

[WEIGHT_AND_BALANCE]
max_gross_weight = 551155.730
empty_weight = 262535.000

reference_datum_position     = 100.000, 0.000, -20.000
empty_weight_CG_position     = -105.000, 0.000, 20.000

max_number_of_stations = 50

;Moments of Inertia
empty_weight_roll_MOI= 15200000.000
empty_weight_pitch_MOI= 17000000.000
empty_weight_yaw_MOI= 17000000.000
empty_weight_coupled_MOI= 2048.000


station_load.0=19841.000000, -75.000000, 0.000000, 16.000000, Front Cargo
station_load.1=15000.000000, -76.000000, 0.000000, 25.000000, Front Pass 
station_load.2=33068.000000, -130.000000, 0.000000, 16.000000, Rear Cargo 
station_load.3=20000.000000, -120.000000, 0.000000, 25.000000, Rear Pass 

[fuel]
Center1    = -85.000, 0.000, 14.000, 11753.1000, 0.000, Tank 6(Центральный)

LeftMain  = -95.000, -23.000, 17.500, 4950.000, 0.000, Tank 2(Расходный 2го)

RightMain = -95.000, 23.000, 17.500, 4950.000, 0.000, Tank 3(Расходный 3го)

LeftAux = -110.000, -40.000, 18.000, 5361.000, 0.000, Tank 1(Расходный 1го)

RightAux= -110.000, 40.000, 18.000, 5361.000, 0.000, Tank 4(Расходный 4го)

LeftTip   = -118.000, -50.000, 19.500, 3618.000, 0.000, Tank 5+5A Left(Концевые лев.)

RightTip  = -118.000, 50.000, 19.500, 3618.000, 0.000, Tank 5+5A Right(Концевые прав.)


fuel_type = 2                                     //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 4                    
electric_pump=0


[airplane_geometry]
wing_area               = 4215.000
wing_span               = 197.200
wing_root_chord         = 40.000
wing_dihedral           = 7.000
wing_incidence          = 0.000
wing_twist              = -1.000
oswald_efficiency_factor= 0.700
wing_winglets_flag      = 1
wing_sweep              = 30.000
wing_pos_apex_lon       = -80.000
wing_pos_apex_vert      = 19.000
htail_area              = 800.000
htail_span              = 64.000
htail_pos_lon           = -175.000
htail_pos_vert          = 28.000
htail_incidence         = 0.000
htail_sweep             = 44.500
vtail_area              = 1115.000
vtail_span              = 29.000
vtail_sweep             = 41.500
vtail_pos_lon           = -163.000
vtail_pos_vert          = 32.000
elevator_area           = 350.000
aileron_area            = 770.000
rudder_area             = 171.000
elevator_up_limit       = 30.000
elevator_down_limit     = 30.000
aileron_up_limit        = 25.000
aileron_down_limit      = 20.000
rudder_limit            = 30.000
elevator_trim_limit     = 10.000
spoiler_limit           = 70.000
spoilerons_available    = 1
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000

[Reference Speeds]
flaps_up_stall_speed    = 190.000
full_flaps_stall_speed  = 140.000
cruise_speed            = 505.000
max_mach                = 0.90
max_indicated_speed= 365.0



[flight_tuning]
cruise_lift_scalar     =1.000  //1.2 было
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
fuel_flow_scalar        = 1.100
min_throttle_limit = -0.20                      //Minimum percent throttle.  Generally negative for turbine reverser

Engine.0= -105.000, -53.600, 14.000
Engine.1= -90.000, -34.000, 12.800
Engine.2= -90.000, 34.000, 12.800
Engine.3= -105.000, 53.600, 14.000

[TurbineEngineData]
fuel_flow_gain          = 0.002
inlet_area              = 32.000
rated_N2_rpm            = 20000.000
static_thrust           = 35520.000
afterburner_available   = 0
reverser_available      = 1.000

[jet_engine]
thrust_scalar =1.000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_pitch=1
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
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

[contact_points]

        //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 Скорость полета limit for retraction     (УЗЛ)
        //15 Скорость полета that gear gets damage at (УЗЛ)

point.0= 1.000, -40.000, 0.000, 6.300, 900.000, 0.000, 2.100, 80.000, 0.200, 0.6, 0.780, 10.000, 10.000, 0.000, 280.000, 320.000
point.1= 1.000, -111.500, -17.000, 6.000, 1000.000, 1.000, 2.106, 0.000, 1.000, 0.800, 0.800, 15.000, 15.000, 0.000, 290.000, 320.000
point.2= 1.000, -111.500, 17.000, 6.000, 1000.000, 2.000, 2.106, 0.000, 1.000, 0.800, 0.800, 15.000, 15.000, 0.000, 290.000, 320.000
point.3= 2.000, -39.000, 0.000, 12.000, 20000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.4= 2.000, -120.000, 0.000, 12.000, 20000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

//point.3= 1.000, -111.500, 0.000, 5.600, 2000.000, 0.000, 2.106, 0.000, 1.000, 0.900, 1.600, 15.000, 15.000, 0.000, 250.000, 280.000

static_pitch = 0.000
static_cg_height = 12.000
gear_system_type=1      //Hydraulic

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.099976     //Percent throttle that activates warning
flap_limit_power=20.000009
flap_limit_idle=20.000009

//pct_throttle_limit =  0.1
//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 = 0.60  //Brake scalar
auto_brakes=4

[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,1,1   //pumps on Eng1,2,3,4

[Views]
eyepoint = -24.0, -1.30, 25.1            ; Longitude, Latitude и Vertical position from Reference Point, (FEET)

[electrical]
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 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
pitot_heat=0, 15, 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2,  17.0
starter1=0, 20, 17.0
starter2=0, 20, 17.0
starter3=0, 20, 17.0
starter4=0, 20, 17.0
auto_brakes=0, 15, 17.0
hydraulic_pump=0, 2,  17.0
fuel_transfer_pump=0, 5,  17.0
max_battery_voltage=28.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0
//electric_always_available=1

[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, 1
Adf.1         = 1
Transponder.1 = 1
Marker.1      = 1

[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -186.00, 0.00, 30.00, fx_navwhih ,
light.1 = 2, -141.00, -92.56, 24.00, fx_strobeh ,
light.2 = 2, -141.30, 92.56, 24.00, fx_strobeh ,
light.3 = 7, -105.000, -53.600, 14.000, fx_737NG ,
light.4 = 7, -90.000, -34.000, 12.800, fx_737NG ,
light.5 = 7, -90.000, 34.000, 12.800, fx_737NG ,
light.6 = 7, -105.000, 53.600, 14.000, fx_737NG ,
light.7 = 4, -23, 0, 25.5, fx_vclighth

[direction_indicators]
//1 Type: 0=None, 1=Вакуумное 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=Вакуумное Gyro, 2=Electric Gyro
attitude_indicator.0 = 1

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

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

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

[EFFECTS]
wake      = fx_wake
water     = fx_wop_spray,
dirt      = fx_wop_tchdrt.fx,
concrete  = CLS_sparks, 1
touchdown = cs707_tchdwn, 1 
windshield_rain_effect_available = 1

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

[forcefeedback]
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; в microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; в microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; в 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                     ; в microseconds
crash_duration2=2500000                 ; в microseconds

[stall_warning]
type=1
stick_shaker=1

[Flaps.0]
type= 1
span-outboard= 0.750
extending-time= 20.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 230.000
lift_scalar= 0.000
drag_scalar= 0.00
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 35.000, 0.000
flaps-position.2= 70.000, 0.000
flaps-position.3= 100.000, 0.000

[Flaps.1]
type= 1
span-outboard= 0.750
extending-time= 20.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 230.000
lift_scalar= 0.900
drag_scalar= 1.500
pitch_scalar= 1.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 28.000, 0.000
flaps-position.3= 45.000, 0.000

[Flaps.2]
type= 2
span-outboard= 0.800
extending-time= 2.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.200
drag_scalar= 0.1
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000

[GROUND_REACTION]
MAX_STEERING_ANGLE=70
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=1