[fltsim.0]
title=Tu-134A Factory
sim=Tu134A3_VVS_2K2
model=
panel=
sound=
texture=Pulkovo
checklists=
kb_reference=Tu134A3_ref
atc_id=65715
atc_airline=Aeroflot
ui_manufacturer=ANTK Tupolev
ui_variation=Pulkovo
ui_type=Tu-134A
description=Notes: 

[GENERAL]
atc_type=Tupolev
atc_model=Tu134
editable=1
performance=

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

[SMOKESYSTEM]
smoke.0=-7.667,-30.00,-7.08, fx_smoke_rx
                
smoke.1=-7.667,-30.00,7.08, fx_smoke_rx
[pitot_static]
vertical_speed_time_constant=10                //Increasing this value will cause a more instantaneous reaction in the VSI

[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

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//Light.0=3, -22.00,   47.70,   -3.28, fx_navgreh ,
//light.1=3, -22.00,  -47.70,   -3.28, fx_navredh ,
//light.2=4,  48.00,    0.00,    3.00, fx_vclighth ,
//Nose lights
//light.3=5,  52.90,   -2.20,   -3.98, fx_landing ,
//light.4=5,  52.90,    2.20,   -3.98, fx_landing ,
//Main gear lights
//light.5=5,  -2.95,  -13.72,   -4.80, fx_landing ,
//light.6=5,  -2.95,   13.72,   -4.80, fx_landing ,

[Views]
eyepoint=48.6,-1.82,2.45

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage=28.0
max_generator_alternator_amps=40.0
flap_motor=0, 0.5 , 17.0
gear_motor=0, 0.5 , 17.0
autopilot=1, 0.5 , 17.0
avionics_bus=0, 1.2, 17.0
avionics=1, 0.2 , 17.0
pitot_heat=0, 0.2 , 17.0
additional_system=0, 2.0, 17.0
marker_beacon=1, 0.5 , 17.0
gear_warning=0, 0.2 , 17.0
fuel_pump=0, 0.5 , 17.0
hydraulic_pump=0, 0.3, 17.0
starter1=0, 2.0, 17.0
starter2=0, 2.0, 17.0
light_nav=0, 0.5 , 17.0
light_beacon=0, 0.5 , 17.0
light_landing=0, 0.5 , 17.0
light_taxi=0, 0.5 , 17.0
light_strobe=0, 0.5 , 17.0
light_panel=0, 0.5 , 17.0

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000


[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight_roll_MOI=2300000.000000
empty_weight_pitch_MOI=3000000.000000
empty_weight_yaw_MOI=3400000.000000
empty_weight_coupled_MOI=1300.000000
empty_weight=75577.000000
//Real plane empty weight
//empty_weight=64045.000000
max_gross_weight=104785.000
//Real empty plus full fuel
//max_gross_weight=93257.000


[fuel]
LeftMain=5.000000,-8.000000,-2.500000,1297.000000,0.000000
LeftAux=-7.000000,-28.000000,-2.600000,883.000000,0.000000
RightMain=5.000000,8.000000,-2.500000,1297.000000,0.000000
RightAux=-7.000000,28.000000,-2.600000,883.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=1236.000000
wing_span=95.167
wing_root_chord=19.67
wing_dihedral=2.000
wing_incidence=1.302
wing_twist=-1.0000
oswald_efficiency_factor=1
wing_winglets_flag=0
wing_sweep=35.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=-3.000000
htail_area=330.000000
htail_span=38.750000
htail_pos_lon=-49.000000
htail_pos_vert=0.000000
htail_incidence=-2.300
htail_sweep=-40.000000
vtail_area=228.000000
vtail_span=17.216
vtail_sweep=-35.000000
vtail_pos_lon=-42.000000
vtail_pos_vert=14.167
elevator_area=68.98
aileron_area=80.520000
rudder_area=61.920000
elevator_up_limit=16.0
elevator_down_limit=12.0
aileron_up_limit=19.5
aileron_down_limit=14.5
rudder_limit=38
elevator_trim_limit=14
spoiler_limit=60
spoilerons_available=1889785610
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

//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]
//Gears
point.0=1.000000,41.333333,0.000000,-10.3300000,500.0,0.000000,1.164610,59.760000,0.3,2.500000,0.75,8.000000,8.000000,0.000000,0.000000,0.000000
point.1=1.000000,-7.333333,-16.583333,-10.333333,600.0,1.000000,1.164610,0.000000,0.25,2.500000,0.70,11.500000,11.500000,2.000000,0.000000,0.000000
point.2=1.000000,-7.333333,16.583333,-10.333333,600.0,2.000000,1.164610,0.000000,0.25,2.500000,0.70,11.800000,11.800000,3.000000,0.000000,0.000000
//Wingtips scrape points
point.3=2.000000,-23.166667,-47.583333,-2.833333,10.0,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-23.166667,47.583333,-2.833333,10.0,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
//Tail scrape point
point.5=2.000000,-39.833333,0.000000,1.083333,10.0,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,41.333333,0.000000,1.083333,10.0,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000

static_pitch=0.000000
static_cg_height=9.436614

[Flaps.0]
type=1
span-outboard=0.605000
extending-time=15.000000
system_type=0
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000000,0.000000
flaps-position.1=10.000004,0.000000
flaps-position.2=20.000009,0.000000
flaps-position.3=30.000013,0.000000
damaging-speed=221                                  // KIAS
blowout-speed=230                                  // KIAS

[GeneralEngineData]
engine_type=1
Engine.0=-27.000000,-7.083333,-7.666667
Engine.1=-27.000000,7.083333,-7.666667
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_scalar=1.000000
fuel_flow_gain=0.005500
inlet_area=10.20000
rated_N2_rpm=11700.000000
static_thrust=12600.000000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=178.000000
full_flaps_stall_speed=125.000000
//cruise_speed=288
// For on overstress crash if the wind quickly change airspeed
cruise_speed=330

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=200.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=95.000000
pitch_takeoff_ga=8.000000
//For no wing leveler when AP On
use_no_default_bank=1
//For no pitch holding when AP On
use_no_default_pitch=1
//Nothing autoland, only hand
autoland_available=0
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=3,0
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=95.000000
pitch_takeoff_ga=8.000000
//For no wing leveler when AP On
use_no_default_bank=1
//For no pitch holding when AP On
use_no_default_pitch=1
//Nothing autoland, only hand
autoland_available=0
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=3,0

//These are special effects for tu-134

//Extending lights
[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position = -15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0

//Stationar
[folding_wings]
wing_fold_system_type = 4                       ;0=None
fold_rates = 1,1                          ;Percent per second

[exits]
number_of_exits=2
exit_rate.0=0.2
exit_rate.1=0.2