[fltsim.0]
title=Ilyusin Il-96M
sim=96M
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=96100
atc_airline=
atc_flight_number=96100
atc_heavy=1
ui_manufacturer=Ilyushin
ui_type=Il-96M
ui_variation=Aeroflot
description=Visual model and flight dynamics by Konovalov Kirill
96M Dynamic v.0.75
[General]
atc_type=ILYUSHIN
atc_model=IL96
performance="Ilyushin 96M \nWing Span (m) 60,105\nLenght (m) 63,939\nHight (m) 15,717\nEngine type\nPW-2337\n \nWeghts\nMTOW (t) 265\nMaximum Commerce Load (t) 58\nMaximum Fuel Capacity (l) 152620\n \nCruice Speed (km/h) 870\nMaximum Range with full load (km) 10000\nCervice ceiling (m) 9000-12000\nTakeOff Distance (m) 2700\nLanding Distance (m) 1650
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 = 595248.000
empty_weight = 291892.000
reference_datum_position = 100.000, 0.000, -20.000
empty_weight_CG_position = -105.000, 0.000, 20.000
max_number_of_stations = 50
station_load.0 =10000.000000, -42.000000, 0.000000, 16.000000, longitudinal
;Moments of Inertia
empty_weight_roll_MOI = 15352310.000
empty_weight_pitch_MOI = 24223159.000
empty_weight_yaw_MOI = 39531785.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.1=10000.000000, -76.000000, 0.000000, 16.000000, Station 2
station_load.2=10000.000000, -135.000000, 0.000000, 16.000000, Station 3
station_load.3=10000.000000, -150.000000, 0.000000, 18.000000, Station 4
station_load.4=10000.000000, -66.000000, 0.000000, 25.000000, Station 6
station_load.5=10000.000000, -143.000000, 0.000000, 25.000000, Station 7
[fuel]
Center1 = -100.000, 0.000, 17.000, 10000.000, 0.000
Center2 = 0.000, 0.000, 0.000, 0.000, 0.000
LeftMain = -115.000, -40.000, 20.000, 3000.000, 0.000
LeftAux = -110.000, -23.000, 19.500, 7500.000, 0.000
RightMain = -115.000, 40.000, 20.000, 3000.000, 0.000
RightAux = -110.000, 23.000, 19.500, 7500.000, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
Center3= 0.000, 0.000, 0.000, 0.000, 0.000
LeftTip= -136.000, -75.000, 23.600, 2100.000, 0.000
RightTip= -136.000, 75.000, 23.600, 2100.000, 0.000
External1= -126.000, -53.000, 21.500, 3000.000, 0.000
External2= -26.000, 52.000, 1.500, 3000.000, 0.000
[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= 0.600
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 = -185.000
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 = -173.000
vtail_pos_vert = 32.000
elevator_area = 350.000
aileron_area = 770.000
rudder_area = 171.000
elevator_up_limit = 19.000
elevator_down_limit = 19.000
aileron_up_limit = 25.000
aileron_down_limit = 20.000
rudder_limit = 30.000
elevator_trim_limit = 20.000
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 = 170.000
full_flaps_stall_speed = 130.000
cruise_speed = 505.000
max_mach = 0.90
max_indicated_speed= 365.0
[flight_tuning]
cruise_lift_scalar =1.000
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 = -0.25 //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 = 55.000
rated_N2_rpm = 20000.000
static_thrust = 38220.000
afterburner_available = 0
reverser_available = 1.000
[jet_engine]
thrust_scalar =1.000
[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 1800.0
autothrottle_available = 1
autothrottle_arming_required = 1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga = 1
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[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, -20.000, 0.000, 5.500, 1500.000, 0.000, 2.100, 70.000, 1.200, 1.200, 1.500, 10.000, 10.000, 0.000, 250.000, 280.000
static_pitch = 0.000
static_cg_height = 12.000
gear_system_type=1 //Hydraulic
point.1= 1.000, -111.500, -17.000, 5.000, 2000.000, 1.000, 2.106, 0.000, 1.000, 0.800, 1.600, 15.000, 15.000, 0.000, 0.000, 0.000
point.2= 1.000, -111.500, 17.000, 5.000, 2000.000, 2.000, 2.106, 0.000, 1.000, 0.800, 1.600, 15.000, 15.000, 0.000, 250.000, 280.000
//point.3= 1.000, -113.000, 0.000, 6.500, 17498.000, 0.000, 2.200, 0.000, 1.000, 2.000, //0.800, 15.000, 15.000, 0.000, 250.000, 280.000
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
[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 = 1.0 //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 = -19.4, -1.25, 25 ; Longitude, Latitude и Vertical position from Reference Point, (FEET)
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Генератор/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 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
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//light.0 = 3, -131.00, -92.56, 25.00, fx_navredh ,
//light.1 = 3, -131.00, 92.56, 25.00, fx_navgreh ,
light.1 = 3, -195.00, 0.00, 30.00, fx_navwhih ,
light.2 = 2, -141.00, -92.56, 24.00, fx_strobeh ,
light.3 = 2, -141.30, 92.56, 24.00, fx_strobeh ,
//light.4 = 2, -201.0, 0.00, 61.00, fx_strobeh ,
//light.6 = 1, -100.05, 0.00, 31.00, fx_beaconh ,
//light.7 = 1, -150.22, 0.00, 12.05, fx_beaconb ,
//light.8 = 4, -7.24, 0.00, 30.19, fx_vclighth,
//light.8 = 5, -2.00, -2.00, 16.50, fx_navwhih ,
//light.9 = 5, -2.00, 2.00, 16.50, fx_navwhih,
//light.10 = 5, -20.40, 0.50, 12.00, fx_navwhih ,
//light.11 = 5, -20.40, -0.50, 12.00, fx_navwhih,
[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]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 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= 230.000
blowout-speed= 280.000
lift_scalar= 0.800
drag_scalar= 0.800
pitch_scalar= 0.600
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 5.000, 0.000
flaps-position.3= 10.000, 0.000
flaps-position.4= 15.000, 0.000
flaps-position.5= 20.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 40.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 10.000
system_type= 1
damaging-speed= 300.000
blowout-speed= 350.000
lift_scalar= 0.300
drag_scalar= 0.100
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 3.000, 0.000
flaps-position.4= 5.000, 0.000
flaps-position.5= 5.000, 0.000
flaps-position.6= 5.000, 0.000
flaps-position.7= 5.000, 0.000
flaps-position.8= 5.000, 0.000
[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