[fltsim.XX]
title=Tu-204-100E Cubana CU-T1701
sim=Tu-204
model=204
panel=
sound=
texture=cubana
atc_id=CU-T1701
atc_airline=Cubana
atc_flight_number=
ui_manufacturer=Tupolev_Kirill Konovalov
ui_type=Tu-204-100
ui_variation=Cubana CU-T1701
description=Tu-204 by Tu-2X4 Development team
atc_parking_types=GATE,RAMP
atc_parking_codes=


[General]
atc_type=Tupolev 
atc_model=Tu-204 
editable=1 
performance=Cruise Speed\tMach .84\nMaximum Range\t5,600 nm\nService Ceiling\t36,400 ft\nMax Takeoff Weight\t580,000 lb\nSeating\t\t368 to 550\nCargo Capacity\t7,552 CU ft\n 


[Reference Speeds]
flaps_up_stall_speed=166
full_flaps_stall_speed=115
cruise_speed=290.0 
max_indicated_speed=340
max_mach=0.83


[pitot_static]
vertical_speed_time_constant = 999
pitot_heat=1.0


[weight_and_balance]
max_gross_weight = 255000.000
empty_weight = 132940.000
max_zero_fuel_weight = 188000.000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 6, 0, 7
empty_weight_roll_MOI = 3425645.000000
empty_weight_pitch_MOI = 3494000.000000
empty_weight_yaw_MOI = 3371429.000000
empty_weight_coupled_MOI = 1020.000000

max_number_of_stations = 7
station_load.0 = 3000,   44, 0,  7, First Class
station_load.1 = 5000,   14, 0,  7, Mid Economy
station_load.2 = 21000, -20, 0,  7, Rear Economy
station_load.3 = 5000,   40, 0,  2, Front Cargo
station_load.4 = 5000,  -24, 0,  2, Aft Cargo
station_load.5 = 0.0, 0.0, 0.0, 0.0, FsStation
station_load.6 = 0.0, 0.0, 0.0, 0.0, FsStation
max_station_load.0 = 3000
max_station_load.1 = 15000
max_station_load.2 = 19000
max_station_load.3 = 10300
max_station_load.4 = 16300


[flight_tuning]
cruise_lift_scalar=1.3
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0
elevator_effectiveness=1.0 
aileron_effectiveness=1.5 
rudder_effectiveness=1.0
pitch_stability=2.0
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=0.8 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 1, -24.9, 0, 6.5, 	fx_beaconh,
light.1 = 1, -9.8, -1.65, -7.35,   fx_beaconb,


[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
contrail = fx_contrail_l
startup = fx_engstrt, 1
windshield_rain_effect_available = 1
contrail=fx_A_I_Contrail


[fuel]
fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1
Center1 = 0, 0, 2, 6964, 3
LeftMain = -3, -12, 4, 2156, 3
RightMain = -3, 12, 4, 2156, 3


[contact_points]
static_pitch = 0.5
static_cg_height = 15.3
max_number_of_points = 10

point.0 = 1, 50.51,         0, -15.65, 2800, 0, 1.42, 65, 0.75, 1.67, 0.72, 9, 9, 0, 0, 220
point.1 = 1,  -5.17, -12.83, -15.60, 3574, 1, 1.7, 0, 0.68, 1.4, 0.74, 12.9, 12.9, 2, 0, 220
point.2 = 1,  -5.17,  12.83, -15.60, 3574, 2, 1.7, 0, 0.68, 1.4, 0.74, 12.1, 12.1, 3, 0, 220

point.3 = 2, -9.1631, -64.7555, 2.5334, 3787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -9.17, 64.939, 2.5267, 3787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -36.7602, 0, -4.1834, 3787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 22.8768, 21.6011, -9.1049, 5000, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.7 = 2, 22.8768, -21.2509, -9.0899, 5000, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.8 = 2, -73.2509, 0, 6.1198, 5000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.9 = 2, 61.4236, 0, -4.617, 3787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
gear_system_type=0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[airplane_geometry]
wing_area = 1815.12
wing_span = 134.12 //effective wing span
wing_root_chord = 15.12 //MAC
wing_dihedral = 0
wing_incidence = 3.0
wing_twist = 0
oswald_efficiency_factor = 0.75 // 
wing_winglets_flag = 1 // ?
wing_sweep = 0
wing_pos_apex_lon = 3.78
wing_pos_apex_vert = 0
htail_area = 472.27
htail_span = 48.82
htail_pos_lon = -65.5
htail_pos_vert = 2.3
htail_incidence = 0.000
htail_sweep = 0 // 35
vtail_area = 354.4
vtail_span = 24.6
vtail_sweep = 0 // 39
vtail_pos_lon = -59
vtail_pos_vert = 5.9
elevator_area = 101.2
aileron_area = 48.2
rudder_area = 123.8
elevator_up_limit = 25.00
elevator_down_limit = 20.00
aileron_up_limit = 25.000
aileron_down_limit = 20.000
rudder_limit = 35.000
elevator_trim_limit = 8.708958  
spoiler_limit = 50.000
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 1
stab_step=0.008
stab_max=0.000
stab_min=0.000


[electrical]
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 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
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


[TurbineEngineData]
fuel_flow_gain = 0.0020
inlet_area = 29.930000
static_thrust = 43000.000000
afterburner_available = 0
reverser_available = 1
rated_N2_rpm = 29920.000000

/////////////////////////////////////////////////////////  TU-204  ///////////////////////////////
//[TurbineEngineData]
//fuel_flow_gain=0.002 
//bypass_ratio=4.35
//inlet_area=16.5
//rated_N2_rpm=12200.000 
//static_thrust=35274 //16000 kgs
//afterburner_available=0 
//reverser_available=1 
/////////////////////////////////////////////////////////////////////////////////////////

[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop 
engine_type = 1
fuel_flow_scalar = 1.0
engine.0 = 10, -21, -8,
engine.1 = 10, 21, -8,
min_throttle_limit=-0.5
max_contrail_temperature=-27.0


[jet_engine]
thrust_scalar = 1.065


[brakes]
parking_brake = 1
toe_brakes_scale =0.6


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


[Views]
eyepoint=67.00, -1.65, 2.463   //(feet) longitudinal, lateral, vertical distance from reference datum


[Radios]
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 0
Adf.1 = 1
Adf.2 = 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


[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


[exits]
number_of_exits = 4
exit.0 = 0.4, 30.50, -4.0, 12,0
exit.1 = 0.4, -28.5, 5, 0.4, 2 =
exit_rate.0 = 0.12
exit_rate.1 = 0.13
exit_rate.2 = 0.14
exit_rate.3 = 0.12


[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1000
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=113
pitch_takeoff_ga=10
max_pitch=10
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=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=20
max_bank_acceleration=1.8
max_bank_velocity=3.0
max_throttle_rate=0.1
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                       = 1.00
use_no_default_pitch =1
use_no_default_bank =1
default_pitch_mode=0
default_bank_mode=0


[stall_warning]
type=1


[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
type = 1


[Flaps.0]//Dummi for Animation
type= 2
span-outboard= 1.000
extending-time= 15.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 290.000
lift_scalar= 0.0
drag_scalar= 0.0
pitch_scalar= 0.0
flaps-position.0= 0.000, 
flaps-position.1= 8.000,
flaps-position.2= 18.000,
flaps-position.3= 26.000,
flaps-position.4= 37.000,


[Flaps.1]//Slat
type= 2
span-outboard= 0.100
extending-time= 22.000
system_type= 1
damaging-speed= 227.000
blowout-speed= 250.000
lift_scalar= 0.0
drag_scalar= 0.0
pitch_scalar= 0.0
flaps-position.0= 0.000, 0.000
flaps-position.1= 19.000, 225.000
flaps-position.2= 19.000, 225.000
flaps-position.3= 23.000, 202.000
flaps-position.4= 23.000, 202.000


[Flaps.2]//Inboard Flap
type= 1
span-outboard= 1.0 //0.200
extending-time= 23.000
system_type= 1
damaging-speed= 245.000
blowout-speed= 270.000
lift_scalar= 1
drag_scalar= 1
pitch_scalar= 1
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.000, 222.000
flaps-position.2= 18.000, 202.000
flaps-position.3= 26.000, 192.000
flaps-position.4= 37.000, 162.000


[Flaps.3]//Outboard Flap
type= 1
span-outboard= 1.0 //0.600
extending-time= 23.000
system_type= 1
damaging-speed= 245.000
blowout-speed= 270.000
lift_scalar= 0.27
drag_scalar= -1.0
pitch_scalar= -0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.000, 222.000
flaps-position.2= 18.000, 202.000


[forcefeedback]
gear_bump_nose_magnitude = 3001
gear_bump_nose_direction = 18001
gear_bump_nose_duration = 250001
gear_bump_left_magnitude = 2701
gear_bump_left_direction = 35501
gear_bump_left_duration = 250001
gear_bump_right_magnitude = 2701
gear_bump_right_direction = 00501
gear_bump_right_duration = 250001
ground_bumps_magnitude1 = 1301
ground_bumps_angle1 = 08901
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09101
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10001
crash_direction1 = 01001
crash_magnitude2 = 10001
crash_direction2 = 9001
crash_period2 = 75001
crash_duration2 = 2500001


