[fltsim.0]
title=Tu-134_UBL
sim=Tu134ubl
model=
panel=
sound=
texture=30
checklists=
kb_reference=
atc_id=63530
atc_airline=AIR FORCE
atc_heavy=0
ui_manufacturer=Tupolev
ui_variation=63530
ui_type=AI Tu-134UBL
description=
atc_flight_number=
atc_parking_types=
atc_parking_codes=UBL
visual_damage=0

[fltsim.1]
title=Tu-134_UBL 63531
sim=Tu134ubl
model=
panel=
sound=
texture=31
checklists=
kb_reference=
atc_id=63531
atc_airline=AIR FORCE
atc_heavy=0
ui_manufacturer=Tupolev
ui_variation=63531
ui_type=AI Tu-134UBL
description=
atc_flight_number=
atc_parking_types=
atc_parking_codes=UBL
visual_damage=0


[General]
atc_type=AIR FORCE
atc_model=AI Tu-134UBL 
editable=0 
performance=\n

[contact_points]
point.0= 1.000, 48.400, 0.000, -10.390, 1181.102, 0.000, 1.235, 59.760, 0.541, 1.100, 0.600, 11.000, 11.000, 0.000, 216.000, 250.000
point.1= 1.000, -3.500, -15.500, -10.600, 1574.803, 1.000, 1.235, 0.000, 0.404, 1.040, 0.690, 10.000, 11.000, 2.000, 216.000, 250.000
point.2= 1.000, -3.500, 15.000, -10.600, 1574.803, 2.000, 1.235, 0.000, 0.404, 1.040, 0.690, 10.000, 11.000, 3.000, 216.000, 250.000
point.3= 1.000, 0.000, -15.000, -10.600, 1574.803, 1.000, 1.235, 0.000, 0.404, 1.040, 0.690, 10.000, 11.000, 2.000, 216.000, 250.000
point.4= 1.000, 0.000, 15.500, -10.600, 1574.803, 2.000, 1.235, 0.000, 0.404, 1.040, 0.690, 10.000, 11.000, 3.000, 216.000, 250.000
point.5= 2.000, -23.167, -47.583, -5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.6= 2.000, -16.980, -47.200, -5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.7= 2.000,  16.300,  -5.000, -4.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.8= 2.000,  -8.233,  -5.000, -5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.9= 2.000, -23.167,  47.583, -5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.10= 2.000, -16.980,  47.200, -5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.11= 2.000,  16.300,   5.000, -4.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.12= 2.000,  -8.233,  5.000, -5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.13= 2.000, -47.500, 0.000, 3.200, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.14= 2.000, 61.033, 0.000, -1.700, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.15= 2.000, -53.800, 0.000, 18.400, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
static_pitch= 0.000
static_cg_height= 10.180
gear_system_type=1      //Hydraulic

[LIGHTS]
light.0=2,  22.2,    0.00, -4.9, fx_beaconb ,
light.1=2,  24.40,   0.00,  4.90, fx_beaconh ,
light.2=4,  52.20,   0.00,  2.70, fx_vclighth ,

[pitot_static]
vertical_speed_time_constant = 1

[WEIGHT_AND_BALANCE]
max_gross_weight = 162900
empty_weight = 82400
reference_datum_position =  0.0, 0.0, 0.0
empty_weight_CG_position =  1.3, 0.0, 0.0   
max_number_of_stations = 50

station_load.0 = "170.0,   41.91, -2.0, 1.64, Pilot"         
station_load.1 = "170.0,   41.91,  2.0, 1.64, Co-Pilot"      
station_load.2 = "11115.0,  18.9,  0.0, 1.64, Front cabin"      
station_load.3 = "3505.0,  29.17,  0.0, -3.28, Front cargo"     
station_load.4 = "4000.0, -50.45,  0.0, 3.05, Rear cargo"       
station_load.5 = "11310.0, -18.49,  0.0, 1.64, Rear cabin"      

;Moments of Inertia
empty_weight_roll_MOI    = 1725000
empty_weight_pitch_MOI   = 2450000
empty_weight_yaw_MOI     = 1950000
empty_weight_coupled_MOI = 0

[fuel]
LeftMain =   -0.82,  -6.16, -0.82, 1829.5, 0.0
RightMain =  -0.82,   6.16, -0.82, 1829.5, 0.0
LeftAux =    -4.93, -26.7,   0.82,  232.0, 0.0
RightAux =   -4.93,  26.7,   0.82,  232.0, 0.0
Center1 =     0.0,    0.0,  -4.11, 2180.0, 0.0

fuel_type = 2          
number_of_tank_selectors = 1
electric_pump = 0

[airplane_geometry]
wing_area=1317.5
wing_span=111.25
wing_root_chord=17.67
wing_dihedral=4.499
wing_incidence=-0.784
wing_twist=0.0
oswald_efficiency_factor=0.75
wing_winglets_flag=1
wing_sweep=25.0
wing_pos_apex_lon=16.0
wing_pos_apex_vert=0.0
htail_area=337.0
htail_span=41.67
htail_pos_lon=-50.0
htail_pos_vert=0.0
htail_incidence=0.0
htail_sweep=0.0
vtail_area=249.0
vtail_span=17.992
vtail_sweep=0.0
vtail_pos_lon=-35.83
vtail_pos_vert=5.83
elevator_area=70.5
aileron_area=26.8
rudder_area=56.2
elevator_up_limit=23.0
elevator_down_limit=20.0
aileron_up_limit=18.0
aileron_down_limit=20.0
rudder_limit=25.0
elevator_trim_limit=18.5
spoiler_limit=45.0
spoilerons_available=1          
aileron_to_spoileron_gain=1.10        
min_ailerons_for_spoilerons=11             
min_flaps_for_spoilerons=30         

[Reference Speeds]
flaps_up_stall_speed     = 155.0	
full_flaps_stall_speed   = 120.0	
cruise_speed             = 459
max_indicated_speed      = 350.0
max_mach=0.88

[Flaps.0]
type=1
span-outboard         = 0.8
extending-time        = 21.0
flaps-position.0      = 0.0
flaps-position.1      = 1.0
flaps-position.2      = 3.0
flaps-position.3      = 5.0
flaps-position.4      = 10.0
flaps-position.5      = 12.0
flaps-position.6      = 13.0
flaps-position.7      = 14.0
flaps-position.8      = 15.0
damaging-speed        = 250.0		
blowout-speed         = 270.0		
lift_scalar           = 0.85
drag_scalar           = 0.8
pitch_scalar          = 1.1
system_type           = 1           

[flaps.1]     
type=2
span-outboard         = 0.8
extending-time        = 18
flaps-position.0      = 0.0
flaps-position.1      = 1.0
flaps-position.2      = 3.0
flaps-position.3      = 5.0
flaps-position.4      = 10.0
flaps-position.5      = 12.0
flaps-position.6      = 13.0
flaps-position.7      = 14.0
flaps-position.8      = 15.0
damaging-speed        = 260	
blowout-speed         = 270	
lift_scalar           = 0.4
drag_scalar           = 0.3
pitch_scalar          = 1.2
system_type           = 1 

[flight_tuning]
cruise_lift_scalar          = 1.0
parasite_drag_scalar        = 1.0
induced_drag_scalar         = 1.0
elevator_effectiveness      = 0.80
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 = -50.98, -10.7, -4.4
Engine.1 = -50.98,  10.7, -4.4
fuel_flow_scalar = 1.055      
min_throttle_limit = -0.35;   

[TurbineEngineData]
fuel_flow_gain         = 0.002
inlet_area             = 29.0
rated_N2_rpm           = 29920
static_thrust          = 19500
afterburner_available  = 0
reverser_available     = 1

[jet_engine]
thrust_scalar=1.0

[autopilot]
autopilot_available                   = 1
flight_director_available             = 1
default_vertical_speed                = 800.0
autothrottle_available                = 1
autothrottle_arming_required          = 1
autothrottle_takeoff_ga               = 1
autothrottle_max_rpm                  = 100
pitch_takeoff_ga                      = 8.0
autoland_available                    = 1
use_no_default_pitch                  = 1
use_no_default_bank                   = 1
default_pitch_mode                    =0
default_bank_mode                     =0
max_pitch                             = 0.7
max_pitch_acceleration=15.0
max_pitch_velocity_lo_alt=0.78
max_pitch_velocity_hi_alt=1.0
max_pitch_velocity_lo_alt_breakpoint  = 5000.0
max_pitch_velocity_hi_alt_breakpoint  = 20000.0
max_bank                              = 25.00
max_bank_acceleration                 = 1.80
max_bank_velocity                     = 3.00
max_throttle_rate                     = 0.10
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                       = 0.00

[gear_warning_system]
gear_warning_available = 0  
pct_throttle_limit =  0.1   
flap_limit_idle    =  5.0   
flap_limit_power   = 25.5   

[brakes]
toe_brakes_scale=0.15
parking_brake=1

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

[Views]
eyepoint=43.22074,-1.723061,4.355627              ; Longitude, Latitude and Vertical position from Reference Point, (FEET)

[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, 0, 17.0
avionics=1, 0 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 0, 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, 0 , 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, 0 , 17.0

[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

[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 = 2 
attitude_indicator.1 = 1 

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

[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

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

[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

[folding_wings]
wing_fold_system_type=4
fold_rates=0.11,0.13