[fltsim.0]
title=Ilyushin Il-18T CU-C1515
sim=il18
model=
panel=
sound=
texture=1515
kb_checklists=
kb_reference=
atc_id=CU-C1515
atc_id_color=
atc_airline=AeroCaribbean
atc_flight_number=
ui_manufacturer=AEROPROYECTO
ui_type="Ilyushin IL-18T"
ui_variation="AeroCaribbean CARGO Variant"
atc_heavy=0
editable=0
description="El Il-18T es una aeronave Il-18D modificada para el transporte de carga. \nAerocaribbean, una aerolнnea regional cubana, introdujo uno de estos equipos en su flota con el objetivo de incrementar el transporte de carga en la isla, con una demanda aъn insatisfecha. \nEsta aronave ha resultado muy exitosa hasta el punto de que es la ъnica de su tipo que aъn, en Julio 2011, presta servicios en Cuba. Todos los demбs IL18 han sido retirados."
visual_damage=1


[General]  
atc_type=Ilyushin
atc_model=Il-18
editable=0
performance=Velocidad mбxima: \n675 km/h (True) \nVelocidad Crucero: \n650 km/h (True) \nMotores: \n4x Ivchenko AI-20M 3,169 kW (4,250 hp) \nAlcance con mбxima carga de pago: \n4,300 km (2,322 nm, 2,650 mi) \nAlcance mбximo: \n6,500 km (3,510 nm, 4,010 mi) \nTecho de vuelo: \n10,000 m (32,800 ft) \nCapacidad de combustible: \n23,700 L \nPeso vacio: \n35,000 kg (77,000 lb) \nMбximo peso de despegue: \n64,000 kg (140,800 lb) \nLargo: \n37.40 m (122 ft 8 in)\nEnvergadura: \n37.90 m (124 ft 4 in) \nAltura: \n10.17 m (33 ft 4 in) \nAsientos: \n100-120 \nSuperficie alar: \n140 mІ (1,506.4 ftІ)


[WEIGHT_AND_BALANCE]  
max_gross_weight=141900                         // (pounds)
empty_weight=77000                              // (pounds)
MTW=140800 					// (pounds)
MLW=115720 					// (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=0.5, 0.0, 0.0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50
//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
// Main Cargo load zone. Cargo Deck.
station_load.0 = "0.0, 1.0, 0.0, 1.0, CDeck Max 30800"
//Extra Crew load zone. Unit x 148,5 (67,5Kg America) у 165 (75,0Kg Europa)
station_load.1 = "0.0, -36.8, 0.0, 1.0, XCrew Max 2475"
// Baggage load zone. Very reduced, almost unuseful, in this cargo version
station_load.2 = "0.0, 0.0, 0.0,-5.0, 1Bagg Max 500"
station_load.3 = "0.0, 0.0, 0.0,-5.0, 2Bagg Max 500"
station_load.4 = "0.0, 0.0, 0.0,-5.0, 3Bagg Max 500"
station_load.5 = "0.0, 0.0, 0.0,-5.0, 4Bagg Max 500"

;Moments of Inertia
empty_weight_pitch_MOI=1287026
empty_weight_roll_MOI=1310000
empty_weight_yaw_MOI=1525867
empty_weight_coupled_MOI=0

[GeneralEngineData] 
engine_type=5
Engine.0=13.1, -29.9, -1.1
Engine.1=16.1, -14.3, -1.7
Engine.2=16.1,  14.3, -1.7
Engine.3=13.1,  29.9, -1.1
max_contrail_temperature = -45
min_throttle_limit=-0.25
fuel_flow_scalar=0.8

[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=150                       //Propeller moment of inertia
beta_max=49.0                           //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=25520                       //Miminum governed RPM
prop_tc=0.004                           //Prop time-constant
gear_reduction_ratio=19.0               //Propeller gear reduction ratio
fixed_pitch_beta=0                      //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80               //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0                   //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=0        //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=600                   //Minimum RPM for prop feathering
beta_feather=93.0                       //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=0.0              //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-12.0              //Minimum pitch angle in reverse, (degrees)
feathering_switches=0                         //Switches which invoke feathering

[TurbineEngineData]
fuel_flow_gain=0.01			//Gain on fuel flow
inlet_area=2.0				//Square Feet, engine nacelle inlet area
rated_N2_rpm=33000.0			//RPM, second stage compressor rated value (AI-20M 13260 RPM overspeed)
static_thrust=1000.0			//Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar=1.0			//Scalar on Turboprop power
maximum_torque=13000.0			//Maximum torque available (ft-lbs)

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

[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,  39.3,   0.0, -11.3, 1000, 0, 1.2, 45.0, 0.4, 3.0, 0.9,  9.0,  7.0, 0, 200.0, 300.0
point.1=1,  -1.8, -14.5, -11.5, 1800, 1, 1.6,  0.0, 0.5, 1.5, 0.5, 15.0, 14.0, 1, 200.0, 300.0
point.2=1,  -1.8,  14.5, -11.5, 1800, 2, 1.6,  0.0, 0.5, 1.5, 0.5, 14.0, 12.0, 2, 200.0, 300.0
// Hard countach
point.3 = 4,  -3.00, -14.00, -6.00, 1600, 0, 0.00,  0.0, 0.3, 2.5, 0.6, 0.0, 0.0, 7, 0.0, 0.0
point.4 = 4,  -3.00,  14.00, -6.00, 1600, 0, 0.00,  0.0, 0.3, 2.5, 0.6, 0.0, 0.0, 7, 0.0, 0.0
point.5 = 4,  40.00,   0.00, -5.00, 1600, 0, 0.00,  0.0, 0.5, 2.5, 0.5, 0.0, 0.0, 7, 0.0, 0.0
point.6 = 4, -40.00,   0.00, -5.00, 1600, 0, 0.00,  0.0, 0.5, 2.5, 0.5, 0.0, 0.0, 7, 0.0, 0.0
// crash points
point.7 =2,   0.00, -60.66,  -0.50,  515, 0, 0.0,  0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.8 =2,   0.00,  60.66,  -0.50,  515, 0, 0.0,  0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.9 =2,  50.00,   0.00,  -3.00,  920, 0, 0.0,  0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.10=2, -60.00,   0.00,   0.00,  920, 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=11.0
gear_system_type=0			//0-electric, 1-hidraulic

[Views]  
eyepoint=41.0, -1.6, 1.7

[Flaps.0] 
type=1
system_type=1
span-outboard=0.6
extending-time=17
damaging-speed=188
blowout-speed=198
flaps-position.0=0
flaps-position.1=15
flaps-position.2=30
pitch_scalar=1.0
lift_scalar=1.3
drag_scalar=1.2

[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, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1, 0
Adf.2=1, 0
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=0
autothrottle_available=0
autothrottle_arming_required=1
autothrottle_max_rpm=93
autothrottle_takeoff_ga=0
pitch_takeoff_ga=9
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
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=3.0
max_throttle_rate=0.1
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=0.0

[exits]
number_of_exits=1
exit_rate.0=0.3

[fuel]
LeftTip=   	-1.0, -44.0, -1.6,  851.0, 0.0		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=   	-1.0, -29.9, -2.4,  940.0, 0.0		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=   	-1.0, -14.3, -3.2, 1266.0, 0.0		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1=   	-1.0,   0.0, -3.8, 1628.0, 0.0		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=   	-1.0,  14.3, -3.2, 1266.0, 0.0		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=  	-1.0,  29.9, -2.4,  940.0, 0.0		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightTip=  	-1.0,  44.0, -1.6,  851.0, 0.0		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2.0					        //Fuel type: 1=Avgas, 2=JetA 6.7lbs=3.04kg/galon
number_of_tank_selectors=4
electric_pump=1

[airplane_geometry] 
wing_area=1721.3                     //Square feet REAL = 140.4 + 19 (central inwing) ~ 160m2 = 1721.344 feet
wing_span=122.0                     //Feet
wing_root_chord=17.2                //Feet
wing_dihedral=3.0                   //Degrees
wing_incidence=3.0                  //Degrees
wing_twist=-1.0                     //Degrees
oswald_efficiency_factor=0.76        //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=4.3               //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=-3.7             //Feet, vertical distance from reference point, positive going up

htail_area=299.4                    //Square feet
htail_span=38.7                    //Feet
htail_incidence=-1.0                //Degrees
htail_sweep=12.0                    //Degrees, vertical tail leading edge
htail_pos_lon=-54.6                //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=1.0                 /Feet, vertical distance from reference point, positive going up

vtail_area=193.6                    //Square feet
vtail_span=64.4                     //Feet, tip to body
vtail_sweep=27.0                    //Degrees, vertical tail leading edge
vtail_pos_lon=-49.4                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=0.0                 //Feet, vertical distance from reference point, positive going up

elevator_area=102                  //Square feet
aileron_area=98                   //Square feet
rudder_area=60                     //Square feet
elevator_up_limit=24.5             //Degrees
elevator_down_limit=15.0           //Degrees
aileron_up_limit=20.0              //Degrees
aileron_down_limit=20.0            //Degrees
rudder_limit=25.0                  //Degrees
elevator_trim_limit=13.0           //Degrees
spoiler_limit=0.0                 //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
auto_spoiler_available=0
spoiler_extension_time=0.0

positive_g_limit_flaps_up=4.4
positive_g_limit_flaps_down=3.1
negative_g_limit_flaps_up=-3.0
negative_g_limit_flaps_down=-2.0

[Reference Speeds]
flaps_up_stall_speed=100.0         //Knots True (KTAS)
full_flaps_stall_speed=84.0        //Knots True (KTAS)
cruise_speed=350.0                 //Knots True (KTAS)
max_indicated_speed=328.0          //Red Line   (KIAS)
max_mach=0.9

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

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3,  0.42, -60.66,  -0.50, fx_navredh ,
light.1=3,  0.42,  60.66,  -0.50, fx_navgreh ,
light.2=3, -2.92, -60.66,  -0.54, fx_navredm ,
light.3=3, -2.92,  60.66,  -0.54, fx_navgrem ,
light.4=1,-59.77,   0.00,  22.12, fx_beaconh ,
light.5=1,-45.04,   0.00,  -4.89, fx_beaconb ,
light.6=4, 40.00,   0.00,   3.00, fx_vclighth ,
light.7=5, -0.33, -59.80,  -1.20, fx_landing ,
light.8=5, -0.33,  59.80,  -1.20, fx_landing ,
light.9=5, 43.30,  -3.93,  -3.36, fx_landing ,
light.10=5, 43.30,  3.93,  -3.36, fx_landing ,
light.11=3,-66.00,  0.00,   1.35, fx_navwhih ,
//Engines smokes
light.12=7, -13.0, -29.9,  -0.1, Ilyushin_smoke ,
light.13=8, -17.0, -14.3,  -0.7, Ilyushin_smoke ,
light.14=9, -17.0,  14.3,  -0.7, Ilyushin_smoke ,
light.15=10,-13.0,  29.9,  -0.1, Ilyushin_smoke ,


[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
p_factor_on_yaw=0.3
torque_on_roll=0.2
gyro_precession_on_yaw=0.3
gyro_precession_on_pitch=0.2
hi_alpha_on_roll=1.0
hi_alpha_on_yaw=1.0
hi_alpha_on_pitch=1.0


[SMOKESYSTEM]
smoke.0=0.0, 0.0, 0.0


[brakes]
toe_brakes_scale=0.6
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.1
flap_limit_power=30.0
flap_limit_idle=15.0

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

[stall_warning]
type=1

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

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

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

[TailHook]
tailhook_length=1                        ;(feet)
tailhook_position=0.0, 0.0, 0.0          ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0

[folding_wings]
wing_fold_system_type=4                  ;0=None
fold_rates=0.10,0.10                     ;Percent per second