[General]
atc_type=TUPOLEV AIRCRAFT
atc_model=T204
editable=1
performance=Do not load more then 9342gall fuel, or aircraft will go overweight. Tupolev TU204 by Robert Versluys.

[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 = 227000.000
empty_weight = 128530.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations =50

station_load.0 =36800.000000,0.000000,0.000000,0.000000 // 184 Passengers @200lbs each

;Moments of Inertia
empty_weight_pitch_MOI  = 3172439.000
empty_weight_roll_MOI   = 2262183.000
empty_weight_yaw_MOI    = 3337024.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[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

[GeneralEngineData]
engine_type = 1
Engine.0 = 4.750, -21.64, -2.500
Engine.1 = 4.750, 21.64, -2.500
fuel_flow_scalar = 1.000
min_throttle_limit=-0.250000

[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 55
rated_N2_rpm = 29920.000
static_thrust = 43100.000
afterburner_available = 0
reverser_available = 1

[jet_engine]
thrust_scalar = 1.0

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
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, 2 , 17.0
additional_system  = 0, 20, 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

        //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)
        
[contact_points]
point.0= 1.000, 54.7, 0.000, -6.163, 1181.102, 0.000, 2.188, 73.320, 0.239, 2.500, 1.933, 4.000, 4.000, 0.000, 0.000, 0.000
point.1= 1.000, -2.06, -14.23, -7.047, 1574.803, 1.000, 2.188, 0.000, 0.972, 2.500, 0.498, 6.900, 6.900, 2.000, 0.000, 0.000
point.2= 1.000, -2.06, 14.23, -7.047, 1574.803, 2.000, 2.188, 0.000, 0.972, 2.500, 0.498, 7.100, 7.100, 3.000, 0.000, 0.000

point.3= 2.000, -18.98, -63.86, 6.883, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //Vleugel r
point.4= 2.000, -18.98, 63.86, 6.883, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //Vleugel l
point.5= 2.000, -50.62, 0.000, 2.228, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Staart-romp
point.6= 2.000, 23.48, 21.64, -4.032, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Motor l
point.7= 2.000, 23.48, -21.64, -4.032, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Motor r
point.9= 2.000, 59.92, 0.000, 1.417, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Romp Neus

max_number_of_points = 21

static_pitch=0
static_cg_height= 6.397
gear_system_type=0

[Views]
eyepoint=62.08, -1.31, 10.58   //(feet) longitudinal, lateral, vertical distance from reference datum

[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

[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

[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

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8;
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
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

[fuel]
Center1 = 11.81, 0.000, 3.281, 6100.000, 0.000 // Main fuel tank, fuse
Center2 = -63.02, 0.000, 20.34, 745.000, 0.000 // Tailfin ballast tank
LeftMain  = 7.874, -18.04, 3.281, 1908.000, 0.000 // Wing Tank
RightMain = 7.874, 18.04, 3.281, 1908.000, 0.000 // Wing Tank
fuel_type = 2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=0

[airplane_geometry]
wing_area               = 1958.000
wing_span               = 137.000
wing_root_chord         = 23.000
wing_dihedral           = 6.200
wing_incidence          = 1.000
wing_twist              = 0.000
oswald_efficiency_factor= 0.890
wing_winglets_flag      = 1
wing_sweep              = 28.000
wing_pos_apex_lon       = 0.000
wing_pos_apex_vert      = 0.000
htail_area              = 338.000
htail_span              = 41.700
htail_pos_lon           = -35.000
htail_pos_vert          = 0.000
htail_incidence         = 0.000
htail_sweep             = 30.000
vtail_area              = 224.000
vtail_span              = 20.000
vtail_sweep             = 35.000
vtail_pos_lon           = -35.800
vtail_pos_vert          = 5.800
elevator_area           = 70.500
aileron_area            = 26.900
rudder_area             = 56.200
elevator_up_limit       = 22.500
elevator_down_limit     = 19.500
aileron_up_limit        = 20.000
aileron_down_limit      = 20.000
rudder_limit            = 26.000
elevator_trim_limit     = 20.000
spoiler_limit           = 60.000
spoilerons_available    = 1
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000

[Reference Speeds]
flaps_up_stall_speed    = 142.000
full_flaps_stall_speed  = 113.000
cruise_speed            = 505.000
max_indicated_speed=345.000000
max_mach=0.860010

[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

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 5.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000

[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 2.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000

[Flaps.2]
type= 2
span-outboard= 0.800
extending-time= 3.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.500, 0.000
flaps-position.2= 1.000, 0.000

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=2, 4.337, 0, 0, fx_strobeh , // Beacon bottom
light.1=2,  20.01,  0,   14.34, fx_strobeh , //Beacon top
light.2=2, -15.92, -65.41,  7.677, fx_strobeh , //Strobe wing
light.3=2, -15.92,  65.41, 7.677, fx_strobeh , //Strobe wing
light.4=3, -15.92, -65.41,  7.677, fx_navredm , //Red Nav Wing
light.5=3, -15.92,  65.41, 7.677, fx_navgrem , //Green Nav Wing

[TailHook]    // #1 Door
tailhook_length=1                             
tailhook_position = 0.0, 0.0, 0.0            

[folding_wings]  // #3 door on 3 door version, #4 door on 4 door version.
wing_fold_system_type = 4                  
fold_rates = 0.4,0.4                       
cable_force_adjust = 1.0

//(C)Robert Versluys!
[brakes]
toe_brakes_scale=0.686666
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0

[fltsim.0]
title=RV Tu204RR Aeroflot
sim=tu204 - rb211
model=
panel=
sound=rr
texture=Aeroflot
kb_checklists=
kb_reference=
atc_id=RA-64007
atc_airline=Aeroflot
atc_flight_number=441
ui_manufacturer=Tupolev
ui_type=Tupolev 204-120
ui_variation=Aeroflot
description=Tupolev TU-204-120\nDynamics v1\nBy:Robert Versluys
atc_heavy=0