[fltsim.0]
title=Aeroflot Ilyushin Ilyushin Il-62
sim=IL62
model=
texture=IL62
ui_manufacturer=AI
ui_type=Ил-62
ui_variation=IL-62
atc_parking_types=GATE
atc_parking_codes=
description=IL- 62       \n\n    

[fltsim.1]
title=Aeroflot Ilyushin IL-62M circa 1974
sim=IL62
model=
texture=IL62M
ui_manufacturer=AI
ui_type=IL62M
ui_variation=IL62M
atc_parking_types=GATE
atc_parking_codes=
description=IL- 62       \n\n  

[fltsim.2]
title=Aeroflot Ilyushin IL-62M Olympic
sim=IL62
model=
texture=olympic
ui_manufacturer=AI
ui_type=IL62M
ui_variation=Olympic
atc_parking_types=GATE
atc_parking_codes=
description=IL- 62       \n\n  

[fltsim.3]
title=76-Aeroflot Ilyushin IL-62M 1973 c/s
sim=IL62
model=
texture=IL-62M 1973
ui_manufacturer=AI
ui_type=Ил-62M
ui_variation=IL-62M'73
atc_parking_types=GATE
atc_parking_codes=
description=IL- 62       \n\n    
                                                                                                              
[General]
atc_type=ILYUSHIN
atc_model=Il-62
editable=0
performance=length: 42,5m,\n wingspan: 53,11m\n height 12,35m\n Cruise speed 850km/h,\n Landing speed: 300km/h,\n Range 11050km\n Seats: 138-198  

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 8.000, 0.000, 0.000            
max_number_of_stations= 50
station_load.0= 0.000, -20.000, 0.000, 0.000
empty_weight= 251770.000                          
max_gross_weight= 454147.600                       
;Moments of Inertia
empty_weight_roll_MOI    =  4369576.3              
empty_weight_pitch_MOI   =  18640473.0 
empty_weight_yaw_MOI     = 10068586.0             
empty_weight_coupled_MOI = 0
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[fuel]
Center1= 0.000, 0.000, 0.000, 8.000, 0.000
LeftMain= 0.000, 0.000, 3.000, 5.000, 0.000
LeftAux= 0.000, -63.000, 4.000, 8.000, 0.000         
RightMain= 0.000, 0.000, 3.000, 5.000, 0.000
RightAux= 0.000, 63.000, 4.000, 8.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0

[flaps.0]    
type             = 1       
span-outboard    = 0.2     
extending-time   = 25      
flaps-position.0 = 0       
flaps-position.1 = 5       
flaps-position.2 = 15      
flaps-position.3 = 20      
flaps-position.4 = 25      
flaps-position.5 = 30      
flaps-position.6 = 40      
damaging-speed   = 220     
blowout-speed    = 300     
lift_scalar = 0.25
drag_scalar = 0.85
pitch_scalar= 0.01
system_type = 1                                         //Hydraulic

[flaps.1]   
type             = 2  
span-outboard    = 0.5
extending-time   = 4  
flaps-position.0 = 0  
flaps-position.1 = 0.5
flaps-position.2 = 0.5 
flaps-position.3 = 0.5 
flaps-position.4 = 0.5 
flaps-position.5 = 1.0
flaps-position.6 = 1.0
damaging-speed   = 260
blowout-speed    = 300 
lift_scalar = 0.05
drag_scalar = 0.15
pitch_scalar= 0.01
system_type = 1   

[flight_tuning]
cruise_lift_scalar=1.200
parasite_drag_scalar=1.4
induced_drag_scalar=1.400
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=1.200
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[contact_points]
static_pitch = 0
static_cg_height = 11.3
max_number_of_points = 5
//          0       1       2        3        4          5       6       7       8     9      10    11      12      13     14       15
point.0 = 1.000, 72.200,  0.000,  -12.100,  900.000,  0.000,  1.500, 55.000, 0.656, 2.000, 0.550, 10.000, 10.000, 0.000, 300.000, 300.000
point.1 = 1.000, -6.6,  -12.500, -11.900,  1100.000,  1.000,  2.380,  0.000, 0.820, 2.000, 0.950, 12.800, 12.800, 2.000, 300.000, 300.000
point.2 = 1.000, -6.6,   12.500, -11.900,  1100.000,  2.000,  2.380,  0.000, 0.820, 2.000, 0.950, 12.800, 12.800, 3.000, 0.000, 0.000
point.3 = 5.000, -50.5,    0, -3.5, 0, 0, 0, 0, 0, 0, 0, 30, 30, 0, 0, 0
point.4 = 2.000, -50.500, 0.000, -3.500, 2000.000, 0.000, 1.000, 80.000, 0.600, 1.200, 0.98, 0.000, 0.000, 0.000, 300.000, 300.000
gear_system_type=0


[brakes]
parking_brake = 1    
toe_brakes_scale = 0.18

[lights]

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

light.0 = 3, -31.9, -70.0,  -0.6, fx_navredm ,
light.1 = 3, -31.9, 70.0,  -0.6, fx_navgrem ,
light.2 = 3, -71.10,   0.60,  4.00, fx_navwhih ,
light.3 = 2,   24.0,   0.40, -5.72, fx_beaconb ,
light.4 = 1,   -75.70,   0.60,  27.80, fx_beaconh ,
light.5 = 4,  79.9,   0.90,  5.10, fx_vclight ,
light.6 = 5,  80.5, -4.33, -2.0, fx_landing.fx ,
light.7 = 5,  80.5, 3.7, -3.7, fx_landing.fx ,
light.8 = 5,  -10.4, -39.1, -2.47, fx_landing.fx ,
light.9 = 5, -10.4, 39.1, -2.47, fx_landing.fx
light.10 = 5, -56.1 , -10.20 , -1.3 , fx_nicksmokeAI_747,      // Engine 1 
light.11 = 5, -56.1 , -16.8 , -1.3 , fx_nicksmokeAI_747,      // Engine 2 
light.12 = 5, -56.1 , 16.8 , -1.3 , fx_nicksmokeAI_747,      // Engine 3 
light.13 = 5, -56.1 , 10.20 , -1.3 , fx_nicksmokeAI_747,      // Engine 4

[GeneralEngineData]
engine_type = 1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -80.0, -10.5,  0.0                //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -80.0,-18.9, 0.0                  //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = -80.0, 18.9, 0.0                  //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3 = -80.0,  10.5,  0.0                 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar        = 1.0                   //Scalar for fuel flow efficiency
min_throttle_limit = -0.0500

[TurbineEngineData]
fuel_flow_scalar=1.123000
fuel_flow_gain= 0.002
inlet_area= 25.500
rated_N2_rpm= 29920.000
static_thrust= 29715.200                  
afterburner_available= 0
reverser_available= 1

[jet_engine]
thrust_scalar=1.000

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 900.0
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_max_rpm = 100
autothrottle_takeoff_ga= 1
pitch_takeoff_ga = 0.4;                     
max_pitch=1.500000                         
max_pitch_acceleration=10.000000             
max_pitch_velocity_lo_alt=0.700000
max_pitch_velocity_hi_alt=1.700000
max_pitch_velocity_lo_alt_breakpoint=5000.000000
max_pitch_velocity_hi_alt_breakpoint=20000.000000
max_bank=25.000000
max_bank_acceleration=5.800000
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

[hydraulic_system]
normal_pressure = 3000.0   
electric_pumps  = 0        
engine_map      = 1,1,1,1  

[Views]
eyepoint=81.133018,-1.435367,9.355520

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  5.0     //Flap angle that activates warning at idle
flap_limit_power   = 25.5     //Flap angle that activates warning at above idle

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/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

[airplane_geometry]
wing_area= 3551.000
wing_span= 158.200                     
wing_root_chord= 22.500
wing_dihedral= 6.476
wing_incidence= 0.000
wing_twist= -0.478
oswald_efficiency_factor= 0.720
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 924.000
htail_span= 66.250
htail_pos_lon= -87.750
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 600.000
vtail_span= 27.928
vtail_sweep= 0.000
vtail_pos_lon= -89.167
vtail_pos_vert= 5.833
elevator_area= 231.000
aileron_area= 152.960
rudder_area= 102.000
elevator_up_limit= 25.502
elevator_down_limit= 18.626
aileron_up_limit= 19.481
aileron_down_limit= 14.897
rudder_limit= 23.491
elevator_trim_limit= 14.481
spoiler_limit= 45.000
spoilerons_available= 1
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons=15.000

[Reference Speeds]
flaps_up_stall_speed=142.000000        
full_flaps_stall_speed=110.600000      
cruise_speed            =470
max_indicated_speed    = 330	
max_mach=0.879980

[direction_indicators]
direction_indicator.0=3,0

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

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

[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_ljet, 1
contrail=fx_A_I_Contrail

[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

[stall_warning]
type=2