[General]
atc_type=TUPOLEV
atc_model=TU134
editable=1
performance=
[Project AI]
Version=6.0
[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 = 103600
empty_weight = 64045
reference_datum_position = 5.0, 0.0, 0.0
empty_weight_CG_position = 1.0, 0.0, 0.0
max_number_of_stations =2
station_load.0 =25000.0, 7.0,0.0,0.0
;Moments of Inertia
empty_weight_pitch_MOI = 2500000.0
empty_weight_roll_MOI = 1900000.0
empty_weight_yaw_MOI = 2900000.0
empty_weight_coupled_MOI = 0.0
CG_forward_limit= 0.0
CG_aft_limit= 1.0
[flight_tuning]
cruise_lift_scalar=1.2
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness =1.4
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 = -29.1, -7.3, 1.1
Engine.1 = -29.1, 7.3, 1.1
fuel_flow_scalar = 1.0
min_throttle_limit = -0.15 //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
inlet_area = 15.3
rated_N2_rpm = 29920.0
static_thrust = 14990
afterburner_available = 0
reverser_available = 1
[jet_engine]
thrust_scalar =1.3
[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
[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 = 0.55 //Brake scalar
[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=62.2, -1.31, 3.8 //(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
[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
[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=2500
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 93
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 = 6.4, 0.0, -4.0, 2240.0, 0.0
LeftMain = -3.5, -8.9, -3.0, 1800.0, 0.0
RightMain = -3.5, 8.9, -3.0, 1800.0, 0.0
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 1370.3
wing_span = 95.2
wing_root_chord = 26.1
wing_dihedral = 2.0
wing_incidence = 1.0
wing_twist = -0.5
oswald_efficiency_factor= 0.74
wing_winglets_flag = 0
wing_sweep = 37.0
wing_pos_apex_lon = 14.1
wing_pos_apex_vert = -3.3
htail_area = 361.3
htail_span = 38.8
htail_pos_lon = -42.3
htail_pos_vert = 19
htail_incidence = 0.5
htail_sweep = 40.0
vtail_area = 212.9
vtail_span = 15.2
vtail_sweep = 43.0
vtail_pos_lon = -30.1
vtail_pos_vert = 4.7
elevator_area = 96.8
aileron_area = 58.1
rudder_area = 68.5
elevator_up_limit = 20
elevator_down_limit = 19
aileron_up_limit = 20.0
aileron_down_limit = 20.0
rudder_limit = 26.0
elevator_trim_limit = 18.0
spoiler_limit = 60.0
spoilerons_available = 1
aileron_to_spoileron_gain = 3.0
min_ailerons_for_spoilerons = 10.0
min_flaps_for_spoilerons = 0.0
[Reference Speeds]
flaps_up_stall_speed = 130.0
full_flaps_stall_speed = 103.0
cruise_speed =485
max_mach = 0.84 // cruise = .9 * Mmo
max_indicated_speed = 330 //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
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.6 // 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 = 20 // degrees
flaps-position.6 = 30 // degrees
flaps-position.7 = 35 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.6
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
//[flaps.1] //Outboard Leading Edge Slat
//type = 2 // 1 - tail, 2 - lead
//span-outboard = 0.9 // 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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1=1, 19.40, 0.00, 5.40, fx_beaconb ,
light.2=1, 17.20, 0.00, -5.40, fx_beaconb ,
[contact_points]
point.0=1.0, 43.4, 0.0, -11.0, 1181.1, 0.0, 1.1, 60.0,0.6, 2.8, 0.75, 4.0, 4.0, 0.0, 0.0, 0.0
point.1=1.0, -15.8, -9.3, -11.7, 1574.8, 1.0, 1.5, 0.0, 0.9, 2.3, 0.7, 6.9, 6.9, 2.0, 0.0, 0.0
point.2=1.0, -15.8, 9.3, -11.7, 1574.8, 2.0, 1.5, 0.0, 0.9, 2.3, 0.7, 7.1, 7.1, 3.0, 0.0, 0.0
point.3=2.0, -23.8, -47.8, -5, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2.0, -23.8, 47.8, -5, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2.0, -52.5, 0.000, 2.6, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2.0, 49.8, 0.000, -5.2, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0
max_number_of_points=7
static_pitch=-0.5
static_cg_height=11
gear_system_type=1 //Hydraulic
[fltsim.0]
title=TAI TU134 KOR
sim=paitu134v6
model=
panel=
sound=
texture=KOR
kb_checklists=
kb_reference=
atc_id=
atc_id_color=0xffffffff
atc_airline=Air Koryo
atc_flight_number=
atc_parking_codes=KOR
atc_parking_types=RAMP,GATE
ui_manufacturer=HAO AI
ui_type=TUPOLEV 134A-3
ui_variation=Air Koryo
atc_heavy=0
description=HAO AI AN24 Only for use with AI Traffic!
visual_damage=0
