[General]
atc_type=TUPOLEV
atc_model=TU134
editable=1
performance=Tu-134
Category=airplane

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[WEIGHT_AND_BALANCE]
max_gross_weight = 150000                      // (pounds)
empty_weight = 74170                           // (pounds)

reference_datum_position     =  0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -5, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 =   "170.0,  41.0, -1.5,	0.0, Pilot"              //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)        
station_load.1 =   "170.0,  41.0,  1.5,	0.0, Co-Pilot"           //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2 =   "510.0,   0.0,  0.0,	0.0, Crew"               //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3 =  "1360.0,  25.5,  0.0,	0.0, First Class"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.4 =  "8160.0,  11.0,  0.0,	0.0, Coach 3-10"         //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.5 =  "8160.0, -10.0,  0.0,	0.0, Coach 11-18"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.6 =  "7140.0, -30.5,  0.0,	0.0, Coach 19-25"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.7 = "10000.0,  20.5,  0.0,	0.0, Forward Baggage"    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.8 =  "4000.0, -27.5,  0.0,	0.0, Aft Baggage"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

;Moments of Inertia
empty_weight_pitch_MOI  = 3172439
empty_weight_roll_MOI   = 2262183
empty_weight_yaw_MOI    = 3337024
empty_weight_coupled_MOI = 0

[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                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 4.75, -16.1, -4.5                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 4.75,  16.1, -4.5                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1                            //Scalar for fuel flow efficiency
min_throttle_limit = -0.25                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature = -30                  //Temperature (deg C) below which contrails may appear

[TurbineEngineData]
fuel_flow_gain = 0.002                          //Gain on fuel flow
inlet_area = 19.6                               //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920                            //RPM, second stage compressor rated value
static_thrust = 23500                           //Lbs, max rated static thrust at Sea Level
afterburner_available = 0                       //Afterburner available?
reverser_available = 1                          //Thrust reverser available?

[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, 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

//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,  40.00,   0.00, -10.7, 1181.1, 0, 4.5, 55.92, 0.6, 2.5, 0.9, 4.0, 4.0, 0, 220.0, 250.0
point.1=1,  -7.75,  -8.58, -10.7, 1574.8, 1, 4.5,  0.00, 1.0, 2.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0
point.2=1,  -7.75,   8.58, -10.7, 1574.8, 1, 4.5,  0.00, 1.0, 2.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0


point.3=2, -14.17, -47.33,  0.00,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -14.17,  47.33,  0.00,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -54.00,   0.00,  2.83,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2,  42.67,   0.00, -3.75,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0


max_number_of_points=21

static_pitch=0.000
static_cg_height=10.7
gear_system_type=1

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  5.0     //Flap angle that activates warning at idle
flap_limit_power   = 25.5     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1         //Parking brake available
toe_brakes_scale = 0.885  //Brake scalar
auto_brakes=4

[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[Views]
eyepoint=43.7, -1.31, 3.7   //(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 20                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 1                                    // degrees
flaps-position.2 = 2                                    // degrees
flaps-position.3 = 5                                    // degrees
flaps-position.4 = 10                                   // degrees
flaps-position.5 = 15                                   // degrees
flaps-position.6 = 25                                   // degrees
flaps-position.7 = 30                                   // degrees
flaps-position.8 = 40                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[flaps.1]       //Inboard Leading Edge Flaps
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 2                                    // seconds
flaps-position.0 = 0                                    // 
flaps-position.1 = 1.0                                  // 
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic


[flaps.2]       //Outboard Leading Edge Slat
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 3                                    // seconds
flaps-position.0 = 0                                    // 
flaps-position.1 = 0.5                                  // 
flaps-position.4 = 1.0                                  // 
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[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

[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=0,0

[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=SKJ_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;
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=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
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 = 1.0

[fuel]
Center1    = 0,   0, 0, 2313, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  = -3, -19, 0, 1500, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3,  19, 0, 1500, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=0

[airplane_geometry]
wing_area               = 1137.0                //Square feet
wing_span               = 94.75                 //Feet
wing_root_chord         = 18.0                  //Feet
wing_dihedral           = 6.2                   //Degrees
wing_incidence          = 1.0                   //Degrees
wing_twist              = -0.5                  //Degrees
oswald_efficiency_factor= 0.75                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 25.0                  //Degrees, wing leading edge
wing_pos_apex_lon       = 8.0                   //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              = 338.0                 //Square feet
htail_span              = 41.7                  //Feet
htail_pos_lon           = -35.0                 //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         = 0.0                   //Degrees
htail_sweep             = 30.0                  //Degrees, horizontal tail leading edge
vtail_area              = 224.0                 //Square feet
vtail_span              = 20.0                  //Feet, tip to body
vtail_sweep             = 35.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -35.8                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 5.8                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 70.5                  //Square feet
aileron_area            = 26.9                  //Square feet
rudder_area             = 56.2                  //Square feet
elevator_up_limit       = 22.5                  //Degrees
elevator_down_limit     = 19.5                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 20.0                  //Degrees
rudder_limit            = 26.0                  //Degrees
elevator_trim_limit     = 20.0                  //Degrees
spoiler_limit           = 60.0                  //Degrees
spoilerons_available    = 1                     //Spoilerons Available?
aileron_to_spoileron_gain = 3                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10                //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000

[Reference Speeds]
flaps_up_stall_speed    = 142.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 113.0                 //Knots True (KTAS)
cruise_speed            = 477.0                 //Knots True (KTAS)
max_mach                = 0.82
max_indicated_speed     = 340                   //Red line (KIAS)

[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

[stall_warning]
type=2
stick_shaker=1

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -21.60,   47.57,   -3.28, fx_navgreh ,
light.1 = 3, -21.60,  -47.57,   -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 ,
light.5 = 7, -30.25 , -6.1 , 1.0 , fx_nicksmokeAI_747 // Engine 1 
light.6 = 7, -30.25 , 6.1 , 1.0 , fx_nicksmokeAI_747 // Engine 2
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0