[fltsim.0]
Title=IL-62M CU-T1208
Sim=il62m
Model=
Panel=
Sound=
Texture=cubana
Kb_checklists=il62m_check
Kb_reference=il62m_ref
Atc_id=CUT1208
Atc_airline=Cubana de aviaciуn
Atc_flight_number=1234
Atc_heavy=1
Ui_manufacturer=Aeroproyecto
Ui_type=ilyushin il-62M
Ui_variation=Cubana Clasic Colors 4x3 Screen
Description="ILYUSHIN IL62M R2.10 FreeWare \nAEROPROYECTO 1999-2015 \nBy Edgar Guinart Lуpez\n>> [email protected] \n>> aeroproyecto.freetzi.com \n\nFor more details check documents within the model"
Visual_damage=1

[fltsim.1]
Title=IL-62M CU-T1208 WS
Sim=il62m
Model=
Panel=WS
Sound=
Texture=cubana
Kb_checklists=il62m_check
Kb_reference=il62m_ref
Atc_id=CUT1208
Atc_airline=Cubana de aviaciуn
Atc_flight_number=1234
Atc_heavy=1
Ui_manufacturer=Aeroproyecto
Ui_type=ilyushin il-62M
Ui_variation=Cubana Clasic Colors Wide Screen
Description="ILYUSHIN IL62M R2.10 FreeWare \nAEROPROYECTO 1999-2015 \nBy Edgar Guinart Lуpez\n>> [email protected] \n>> aeroproyecto.freetzi.com \n\nFor more details check documents within the model"
Visual_damage=1

[fltsim.2]
Title=IL-62M
Sim=il62m
Model=
Panel=
Sound=
Texture=white
Kb_checklists=il62m_check
Kb_reference=il62m_ref
Atc_id=CUT1282
Atc_airline=Cubana de aviaciуn
Atc_flight_number=
Atc_heavy=1
Ui_manufacturer=Aeroproyecto
Ui_type=ilyushin il-62M
Ui_variation=White Colors
Description="ILYUSHIN IL62M R2.10 FreeWare \nAEROPROYECTO 1999-2015 \nBy Edgar Guinart Lуpez\n>> [email protected] \n>> aeroproyecto.freetzi.com \n\nFor more details check documents within the model"
Visual_damage=1

[general]
Atc_type=ILYUSHIN
Atc_model=IL62
Editable=0
Performance=Cuise Speed: 0.80 mach ~ 850 kph \nEngines: 4 x 107.9KN (24,250) Soloviev D30KU \nRange: 10,500KM \nOperative Altitude: 13000m \nMax Fuel: 1053000 l (x 0.825 kg/l) ~ 86870 kg \nEmpty Weight: 71527kg\nCabin: 186 pax \nPayload: 23,000 kg

Visual_damage=1

[pitot_static]
Vertical_speed_time_constant=1                //increasing this value will cause a more instantaneous reaction in the vsi

[weight_and_balance]
Max_gross_weight=372960                  // (pounds) ~ 168000 kg
Empty_weight=163900                         // (pounds) ~ 74500 kg Operative Empty Weight (OEW)

Reference_datum_position=0, 0, 0      // (feet) distance from flightsim reference position: (1/4 chord, centerline, waterline)
Empty_weight_cg_position=0, 0, 0     // (feet) longitudinal, lateral, vertical distance from specified datum

Max_number_of_stations=20		// max. Payload 23T ()
// Pax *** passenger unit x 148,5lbs (67,5kg America) or 165lbs (75,0kg Europe)  Config: 186 PAX
Station_load.0="4900.0,   60.1,   0.0,   2.0, oa-30 ~ 4950 lbs"	          //weight (lbs), longitudinal, lateral, vertical
Station_load.1="5900.0,   43.6,   0.0,   2.0, ob-36 ~ 5940 lbs"
Station_load.2="5900.0,   12.4,   0.0,   2.0, oc-36 ~ 5940 lbs"
Station_load.3="6900.0,   -2.5,   0.0,   2.0, od-42 ~ 6930 lbs"
Station_load.4="6900.0,  -19.0,   0.0,   2.0, oe-42 ~ 6930 lbs"
Station_load.5="0.0,  -36.0,   0.0,   2.0, wr-4  ~ 1760 lbs"
// Water ballast
Station_load.6 ="0.0,   72.0,   0.0,   -2.0, wb (max 7000)"
// Cargo
Station_load.7 ="1700.0,   57.4,   0.0,   -2.0, c1 (max 6820)"
Station_load.8 ="6800.0,   42.6,   0.0,   -2.0, c2 (max 6820)"
Station_load.9 ="7200.0,  -24.6,   0.0,   -2.0, c3 (max 7260)"
Station_load.10="4400.0,  -36.0,   0.0,   -2.0, c4 (max 4400)"
Station_load.11="0.0,  -55.0,   0.0,    2.0, c6 (max 2948)"

;moments of inertia
Empty_weight_pitch_moi= 6036656		//Calculations: 6036656
Empty_weight_roll_moi = 3500000		//Calculations: 1727840
Empty_weight_yaw_moi  = 5215978		//Calculations: 5215978
Empty_weight_coupled_moi=0.0

[contact_points]

Max_number_of_points=12
//0  class                        <0=none,1=wheel, 2=scrape, 3=float, 4=?, 5=water_rudder>
//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)

Point.0=1,  71.9,    0.0, -12.10, 1200.0, 0, 1.5, 65.0,   0.50, 3.00, 0.60,  10.0,  11.0, 0, 0, 297
Point.1=1, -4.5,   -12.6, -12.00, 1800.0, 1, 2.6, 0.00,   0.60, 1.70, 0.60,  14.0,  15.0, 2, 0, 297
Point.2=1, -4.5,    12.6, -12.00, 1800.0, 2, 2.6, 0.00,   0.60, 1.70, 0.60,  14.0,  15.0, 3, 0, 297
//scrapes
Point.3=2, -29.0, -71.0,   0.37, 500.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 5,   0,   0
Point.4=2, -29.0,  71.0,   0.37, 500.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 6,   0,   0
Point.5=2,  80.2,  0.00,   -4.3, 500.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 9,   0,   0
Point.6=2, -31.0,  0.00,   -4.3, 500.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
//tailwheel
Point.7=5, -42.4, 0.0, -12.6, 120, 0, 0.00, 0.0, 0.0,  0.0, 1.0, 12, 12, 0, 0.0, 13.4
//hard
Point.8=4,   -5.0,  -7.0,  -5.0, 1600, 0, 0.00,  0.0, 0.6, 2.5, 0.6, 0.0, 0.0, 7, 0.0, 0.0
Point.9=4,   -5.0,   7.0,  -5.0, 1600, 0, 0.00,  0.0, 0.6, 2.5, 0.6, 0.0, 0.0, 7, 0.0, 0.0
Point.10=4,  30.0,   0.0,  -5.0, 1600, 0, 0.00,  0.0, 0.6, 2.5, 0.6, 0.0, 0.0, 7, 0.0, 0.0


Static_pitch=0.0
Static_cg_height=12.0
Gear_system_type=1

[views]
Eyepoint=80.0, -1.6, 3.7              ; longitude, latitude and vertical position from reference point, (feet)

[fuel]
//longitudinal (feet), lateral (feet), vertical (feet), usable(gallons), unusable (gallons)
External1= -22.0,  -55.7,  -0.3,  1056.4,   1.0		// 5 Left
Lefttip=    -6.5,  -32.0,  -1.0,  4876.8,   3.0		// 1
Leftaux=     3.3,  -13.0,  -1.9,  4876.8,   3.0		// 2
Rightaux=    3.3,   13.0,  -1.9,  4876.8,   3.0		// 3
Righttip=   -6.5,   32.0,  -1.0,  4876.8,   3.0		// 4
External2= -22.0,   55.7,  -0.3,  1056.4,   1.0		// 5 Right
Center1=    10.0,    0.0,  -2.5,  5554.2,   4.0		// 6 Center wings
Center2=   -54.0,    0.0,  13.3,  1354.7,   1.0		// 7 Tail plane
Fuel_type=2
Number_of_tank_selectors=4                   
Electric_pump=1

[reference speeds]
Flaps_up_stall_speed=145                 //knots true (ktas)
Full_flaps_stall_speed=123                 //knots true (ktas)
Cruise_speed=456                            //knots true (ktas)
Max_indicated_speed=338                //knots true (kias)
Max_mach=0.83

[flaps.0]
Type=1                                    // 1 - tail, 2 - lead
Span-outboard=0.6                                  // 0.0 .. 1.0
Extending-time=20                                   // seconds
Flaps-position.0=0                                    // degrees
Flaps-position.1=15                                   // degrees
Flaps-position.2=30                                   // degrees
Damaging-speed=220                                  // kias
Blowout-speed=241                                  // kias
Lift_scalar=1.0
Drag_scalar=1.0
Pitch_scalar=1.0
System_type=1                                         //hydraulic

[generalenginedata]
Engine_type=1                                 //0=piston, 1=jet, 2=none, 3=helo-turbine, 4=rocket, 5=turboprop
Engine.0=-47.0, -17.07,  2.86                 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-47.0, -10.54,  2.86                  //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2=-47.0,  10.54,  2.86                  //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3=-47.0,  17.07,  2.86                 //(feet) longitudinal, lateral, vertical distance from reference datum
Min_throttle_limit=-0.35                      //minimum percent throttle.  Generally negative for turbine reverser
Max_contrail_temperature=-30                  //temperature (deg c) below which contrails may appear
Fuel_flow_scalar=1.0                          //scalar for fuel flow efficiency 

[turbineenginedata]
Fuel_flow_gain=0.002                 //gain on fuel flow
Inlet_area=20.5                         //square feet, engine nacelle inlet area (1.91 m2)
Rated_n2_rpm=15800                 //rpm, second stage compressor rated value   (Real: 15800 real)
Static_thrust=24200                 //lbs, max rated static thrust at sea level   (Max rated: ~ 24200 at sea level / ~ 6600 at 0.8M FL360)
Afterburner_available=0                     //afterburner available?
Reverser_available=1                     //thrust reverser available?

[jet_engine]
Thrust_scalar = 1.0

[TailHook]				//used in reverser system... DO NOT REMOVE!!!
tailhook_length       =1                                       ;(feet)
tailhook_position    =  44.0,  0.0,  2.25           ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 0.0

[electrical]
;BusType, MaxAmpLoad, MinVoltage
;BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
electric_always_available = 0   // Never set to 1 !!!
max_battery_voltage		= 24.0
generator_alternator_voltate	= 28.0
max_generator_alternator_amps	= 200.0
flap_motor 			= 0, 0 , 17.0
gear_motor 			= 0, 0 , 17.0
autopilot 			= 0, 0 , 17.0
avionics_bus 			= 0, 0 , 17.0
avionics 			= 1, 0 , 17.0
pitot_heat 			= 0, 0 , 17.0
additional_system 		= 0, 0 , 17.0
marker_beacon 			= 1, 0 , 17.0
gear_warning 			= 0, 0 , 17.0
fuel_pump 			= 0, 0 , 17.0
starter1 			= 0, 0 , 17.0
starter2 			= 0, 0 , 17.0
starter3 			= 0, 0 , 17.0
starter4 			= 0, 0 , 17.0
light_nav 			= 0, 0 , 17.0
light_beacon 			= 0, 0 , 17.0
light_strobe 			= 0, 0 , 17.0
light_landing 			= 0, 0 , 17.0
light_taxi 			= 0, 0 , 17.0
light_panel 			= 0, 0 , 17.0
prop_sync 			= 0, 0 , 17.0
auto_feather 			= 0, 0 , 17.0
auto_brakes 			= 0, 0 , 17.0
standby_vacuum 			= 0, 0 , 17.0
hydraulic_pump 			= 0, 0 , 17.0
fuel_transfer_pump 		= 0, 0 , 17.0
propeller_deice 		= 0, 0 , 17.0
directional_gyro 		= 0, 0 , 17.0
directional_gyro_slaving 	= 0, 0 , 17.0
//Engines smokes
light_cabin 			= 0, 0 , 17.0
light_recognition 		= 0, 0 , 17.0
light_wing 			= 0, 0 , 17.0
light_logo 			= 0, 0 , 17.0


[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=1
Marker.1=1

[lights]
//types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing                   
Light.0=3, -25.90,      -70.90,   0.00, fx_navwhih 
Light.1=3, -25.90,       70.90,   0.00, fx_navwhih 
Light.2=1, -68.93,        0.00,  29.13, fx_beaconb 
Light.3=1,  28.10,        0.00,  -5.4, fx_beaconb 
Light.4=3, -26.70,      -71.30,   0.00, fx_navredh 
Light.5=3, -26.70,       71.30,   0.00, fx_navgreh
Light.6=3, -29.74,      -70.23,   -0.36, fx_navwhih 
Light.7=3, -29.74,       70.23,   -0.36, fx_navwhih
//Cabin lights
Light.8=4,  84.50,        0.00,   4.0, IL62_cabin
Light.9=4,  70.80,        0.00,   3.0, IL62_cabin
Light.10=4, 28.20,        0.00,   3.0, IL62_cabin
//Engines smoke
light.11 =7, -44.0, -17.07,  2.25, IL62_smoke 
light.12=8, -44.0, -10.54,  2.25, IL62_smoke
light.13=9, -44.0,  10.54,  2.25, IL62_smoke
light.14=10,-44.0,  17.07,  2.25, IL62_smoke
//APU smoke
light.15=2, -67.0,  0.0,  3.5, IL62_smoke_APU

[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 = 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

[smokesystem]
smoke.0= 0.00,  -35.5, -70.00, IL62_dump                 // vertical, longitudinal, lateral, effect
smoke.1= 0.00,  -35.5,  70.00, IL62_dump 


[exits]
Number_of_exits=2
Exit_rate.0=0.4                               ;percent per second
Exit_rate.1=0.4                               ;percent per second

[brakes]
Parking_brake=1             //parking brake available
Toe_brakes_scale=0.6       //brake scalar

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  1.0     //Percent throttle that activates warning
flap_limit_idle    = 15.0     //Flap angle that activates warning at idle
flap_limit_power   = 30.0     //Flap angle that activates warning at above idle

[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

[stall_warning]
Type=1

[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=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=1,0


[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


[airplane_geometry]
Wing_area=3009.0                   //square feet MS Total=3009.0
Wing_span=143.0                    // feet
Wing_root_chord=35.0                  //feet
Wing_dihedral=3.0                   //degrees
Wing_incidence=3.0                   //degrees
Wing_twist=-2.5                          //degrees
Oswald_efficiency_factor=0.7             //measure of lift effeciency of wing
Wing_winglets_flag=0                     //are winglets available?
Wing_sweep=35.0                  //degrees, wing leading edge
Wing_pos_apex_lon=27.0                 //feet, longitudinal distance from reference point, negative going aft
Wing_pos_apex_vert=-1.6                     //feet, vertical distance from reference point, positive going up

Htail_area=480                     //square feet
Htail_span=40.8                  //feet
Htail_pos_lon=-59.5                //feet, longitudinal distance from reference point, negative going aft
Htail_pos_vert=27.3                   //feet, vertical distance from reference point, positive going up
Htail_incidence=0.0                  //degrees
Htail_sweep=35.0                  //degrees, horizontal tail leading edge

Vtail_area=361                  //square feet
Vtail_span=18.3                  //feet, tip to body
Vtail_sweep=42.0                  //degrees, vertical tail leading edge
Vtail_pos_lon=-43.7                //feet, longitudinal distance from reference point, negative going aft
Vtail_pos_vert=6.5                  //feet, vertical distance from reference point, positive going up

Elevator_area=190                   //square feet
Aileron_area=156                   //square feet
Rudder_area=144                   //square feet
Elevator_up_limit=26                    //degrees
Elevator_down_limit=14                    //degrees
Aileron_up_limit=27                    //degrees
Aileron_down_limit=15                    //degrees
Rudder_limit=30.0                  //degrees
Elevator_trim_limit=15                    //degrees
Spoiler_limit=60                    //degrees
Spoilerons_available=1                     //spoilerons available?
Aileron_to_spoileron_gain=1                   //aileron to spoileron gain
Min_ailerons_for_spoilerons=5                //degrees
Min_flaps_for_spoilerons=0                    //minimum flap handle position when spoilerons activate
positive_g_limit_flaps_up=3.0
negative_g_limit_flaps_up=-1.0
positive_g_limit_flaps_down=2.0
negative_g_limit_flaps_down=-0.5

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 99
autothrottle_takeoff_ga=0
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=20.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0


[forcefeedback]
Gear_bump_nose_magnitude=3000           ; 0 - 10000
Gear_bump_nose_direction=18000          ; 0 - 35999 degrees
Gear_bump_nose_duration=250000          ; in microseconds
Gear_bump_left_magnitude=2700           ; 0 - 10000
Gear_bump_left_direction=35500          ; 0 - 35999 degrees
Gear_bump_left_duration=250000          ; in microseconds
Gear_bump_right_magnitude=2700          ; 0 - 10000
Gear_bump_right_direction=00500         ; 0 - 35999 degrees
Gear_bump_right_duration=250000         ; in 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                     ; in microseconds
Crash_duration2=2500000                 ; in microseconds