[fltsim.0]
title=Ilyushin Il-18d
sim=Il18d
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=75725
atc_id_color=0xffffffff
atc_airline=Aeroflot
atc_flight_number=75725
ui_manufacturer=Ilyushin
ui_type=Il-18d
ui_variation=Aeroflot '60-'70s
editable=0
description=Long range passenger aircraft, first flight July 4, 1957 \n\nFS2002 only \n\nApr.8.2002
atc_heavy=0

[General]  
atc_type=Ilyushin
atc_model=Il-18
editable=0
performance=Cruise Speed\n625km/h \n\nEngines\n4 Ivchenko AI-20M \n\nMaximum Range\n7'100km \n\nService Ceiling\n9,000 m \n\nFuel Capacity\n23,700 L \n\nEmpty Weight-Standard\n33,760 kg \n\nMaximum Takeoff Weight\n64,000kg \n\nLength\n35.9m \n\nWingspan\n37.42 m \n\nHeight\n10.17m \n\nSeating\nSeats 100 to 120

[pitot_static]
vertical_speed_time_constant=10                //Increasing this value will cause a more instantaneous reaction in the VSI

[WEIGHT_AND_BALANCE]  
max_gross_weight=142200                        // (pounds)
empty_weight=88900                             // (pounds)

reference_datum_position=0.0, 0.0, 0.0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_cg_position=0.0, 0.0, 0.0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=0.000000,0.000000,0.000000,0.000000

;Moments of Inertia
empty_weight_pitch_MOI=1636600
empty_weight_roll_MOI=1659435
empty_weight_yaw_MOI=231380
empty_weight_coupled_MOI=0

[flight_tuning]
cruise_lift_scalar=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[GeneralEngineData] 
engine_type=5
Engine.0=13.5, -30.5, 2.8
Engine.1=16.2, -14.1, 2.1
Engine.2=16.2,  14.1, 2.1
Engine.3=13.5,  30.5, 2.8
fuel_flow_scalar=0.700

[propeller]
thrust_scalar=1.0                       //Propeller thrust scalar
propeller_type=0                        //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=14.76                //Propeller Diameter, (feet)
propeller_blades=4                      //Number of propeller blades
propeller_moi=75                        //Propeller moment of inertia
beta_max=50.0                           //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=8.0                            //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=700.0                       //Miminum governed RPM
prop_tc=0.004                           //Prop time-constant
gear_reduction_ratio=12.100             //Propeller gear reduction ratio
fixed_pitch_beta=0                      //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=180.000          //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=1        //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=500                 //Minimum RPM for prop feathering
beta_feather=93.320                     //Feathering pitch angle (degrees)
power_absorbed_cf=0.9                   //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0   //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=1                //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0              //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0              //Minimum pitch angle in reverse, (degrees)

[TurbineEngineData] 
fuel_flow_gain=0.015
inlet_area=3.5
rated_N2_rpm=22400.0
static_thrust=900.0

[turboprop_engine]
power_scalar=1.0
maximum_torque=13600.0

[electrical]
;BusType, MaxAmpLoad, MinVoltage
;BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage=24.0
generator_alternator_voltate=28.0
max_generator_alternator_amps=200.0
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 15, 17.0
additional_system=0, 2 , 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
starter2=0, 20, 17.0
light_nav=0, 0 , 10.0
light_beacon=0, 5 , 10.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 10.0
light_panel=0, 5 , 10.0

[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 Airspeed limit for retraction     (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
point.0=1,  47.5,  0.000,  -8.60, 1200, 0, 1.0, 55.0, 0.21, 1.0, 1.5,  9.0,  7.0, 0, 189.0, 194.0
point.1=1,  -1.3, -15.445, -9.44, 1900, 1, 1.6,  0.0, 1.00, 1.0, 0.1, 15.0, 14.0, 2, 189.0, 194.0
point.2=1,  -1.3,  15.445, -9.44, 1900, 2, 1.6,  0.0, 1.00, 1.0, 0.1, 14.0, 12.0, 3, 189.0, 194.0
point.3=2,  -1.35, -61.80,   2.8,  415, 0, 0.0,  0.0, 0.00, 0.0, 0.0,  0.0,  0.0, 5,   0.0,   0.0
point.4=2,  -1.35,  61.80,   2.8,  415, 0, 0.0,  0.0, 0.00, 0.0, 0.0,  0.0,  0.0, 6,   0.0,   0.0
point.5=2, -53.20,   0.00,  -0.5,  820, 0, 0.0,  0.0, 0.00, 0.0, 0.0,  0.0,  0.0, 9,   0.0,   0.0
point.6=2,  40.15,   0.00,  -2.6,  680, 0, 0.0,  0.0, 0.00, 0.0, 0.0,  0.0,  0.0, 4,   0.0,   0.0

static_pitch=0.0
static_cg_height=8.54

[Views]  
eyepoint=42.8, -1.7, 5.4

[Flaps.0] 
type=1
span-outboard=0.57
extending-time=17
system_type=1
damaging-speed=173
blowout-speed=179
lift_scalar=1.9
drag_scalar=1.2
pitch_scalar=1.0
flaps-position.0=0
flaps-position.1=15
flaps-position.2=30

[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

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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1900
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=93
autothrottle_takeoff_ga=1
pitch_takeoff_ga=9
use_no_default_bank=1
use_no_default_pitch=1

[exits]
number_of_exits=3
exit_rate.0=0.3
exit_rate.0=0.4
exit_rate.1=0.7

[fuel] 
LeftMain=0.0, -20.6, 0.0, 1981.5, 0.0		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=0.0, -30.0, 0.0, 1981.5, 0.0		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=0.0,  20.6, 0.0, 1981.5, 0.0		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=0.0,  30.0, 0.0, 1981.5, 0.0		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2.0					//Fuel type: 1=Avgas, 2=JetA
number_of_tank_selectors=2

[airplane_geometry] 
wing_area=1502.2                   //Square feet
wing_span=122.73                   //Feet
wing_root_chord=17.166             //Feet
wing_dihedral=4.500                //Degrees
wing_incidence=0.999756            //Degrees
wing_twist=-1.499634               //Degrees
oswald_efficiency_factor=0.99      //Measure of lift effeciency of wing
wing_winglets_flag=0               //Are winglets available?
wing_sweep=0.0                     //Degrees, wing leading edge
wing_pos_apex_lon=0.0              //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0             //Feet, vertical distance from reference point, positive going up
htail_area=67.0                    //Square feet
htail_span=17.17                   //Feet
htail_pos_lon=-24.6                //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0                 /Feet, vertical distance from reference point, positive going up
htail_incidence=0.5                //Degrees
htail_sweep=0.0                    //Degrees, vertical tail leading edge
vtail_area=42.0                    //Square feet
vtail_span=7.4                     //Feet, tip to body
vtail_sweep=0.0                    //Degrees, vertical tail leading edge
vtail_pos_lon=-52.3                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=22.3                //Feet, vertical distance from reference point, positive going up
elevator_area=75.0                 //Square feet
aileron_area=58.0                  //Square feet
rudder_area=370.0                  //Square feet
elevator_up_limit=20.0             //Degrees
elevator_down_limit=17.5           //Degrees
aileron_up_limit=18.0              //Degrees
aileron_down_limit=18.0            //Degrees
rudder_limit=30.0                  //Degrees
elevator_trim_limit=25.0           //Degrees
spoiler_limit=50.0                 //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

[Reference Speeds]
flaps_up_stall_speed=100.0         //Knots True (KTAS)
full_flaps_stall_speed=83.8        //Knots True (KTAS)
cruise_speed=351.0                 //Knots True (KTAS)

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 0

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3,  0.50, -61.90,  2.90, fx_navredh ,
light.1=3,  0.50,  61.90,  2.90, fx_navgreh ,
light.2=3, -3.00, -61.90,  2.70, fx_navredm ,
light.3=3, -3.00,  61.90,  2.70, fx_navgrem ,
light.4=1, -59.7,   0.00, 26.55, fx_beaconh ,
light.5=1, -45.4,   0.00, -2.10, fx_beaconb ,
light.6=4,  43.0,   0.00,  5.20, fx_vclighth ,
light.7=4,  21.0,  -1.10,  7.00, fx_vclighth ,
light.8=4, -27.0,  -1.10,  7.00, fx_vclighth ,

[SMOKESYSTEM]
smoke.0=0.000, -15.00, -30.50, fx_smoke_rx
smoke.1=-1.000, -17.00, -14.10, fx_smoke_rx
smoke.2=-1.000, -17.00,  14.10, fx_smoke_rx
smoke.3=0.000, -15.00,  30.50, fx_smoke_rx

[forcefeedback]
stick_shaker_magnitude=5000		; 0 - 10000
stick_shaker_direction=0		; 0 - 35999 degrees
stick_shaker_period=111111		; in microseconds
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=9000		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=2700		; 0 - 10000
gear_bump_right_direction=27000		; 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