[General]
atc_type=TUPOLEV 
atc_model=TU154 
editable=1 
performance=by Sanovich

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

[weight_and_balance]

// ACM V2.5
max_gross_weight = 216053
//empty_weight = 111774
empty_weight = 216053
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -20.33, 0, 1.2
empty_weight_pitch_MOI = 3399586
empty_weight_roll_MOI = 906110
empty_weight_yaw_MOI = 2846825
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.000
CG_aft_limit = 1.000
max_number_of_stations = 1

station_load.0 = 39683, -20.33, -0.02, 1.2


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 1, -68.91, 0, 27.27, fx_beaconh
light.1 = 1, -51.29, 0, -2.25, fx_beaconb
light.2 = 3, -40.61, -61.38, -2.19, fx_navredm
light.3 = 3, -40.61, 61.38, -2.19, fx_navgrem
light.4 = 3, -73.09, 0, 2.33, fx_navwhih
light.5 = 2, -59.14, 9.18, 3.15, fx_tcai154smoke2
light.6 = 2, -59.14, -9.18, 3.15, fx_tcai154smoke2
light.7 = 2, -73.37, 0, 4.91, fx_tcai154smoke2
light.8 = 1, -59.14, 9.18, 3.15, fx_tcai154smoke1
light.9 = 1, -59.14, -9.18, 3.15, fx_tcai154smoke1
light.10 = 1, -73.37, 0, 4.91, fx_tcai154smoke1

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.000
min_throttle_limit = -0.15
max_contrail_temperature = -30
engine.0 = -48.44, -9.77, 3.56,
engine.1 = -62.45, 0, 5.08,
engine.2 = -48.40, 9.68, 3.56,

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tcai154tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 0

Center1 = -20, -0.02, -2, 4487, 0
LeftMain = -20, -10.17, 0, 4487, 0
RightMain = -20, 9.35, 0, 4487, 0


[contact_points]
static_pitch = 0
static_cg_height = 10.15
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 3


point.0 = 1, 37.9207, 0, -11.7043, 1181.1, 0, 1.35, 55.92, 1.3, 1.9231, 0.9, 11.4, 11.6, 0, 220, 250
point.1 = 1, -23.4, -18.85, -11.4291, 1574.8, 1, 1.55, 0, 1.9, 1.1, 0.9, 10.2, 10.8, 2, 220, 250
point.2 = 1, -23.414, 18.85, -11.4291, 1574.8, 1, 1.55, 0, 1.9, 1.1, 0.9, 10.8, 11.1, 2, 220, 250


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[airplane_geometry]
//ACM_AREAW1// 0,0,0,8.0162,1.8286,1.8286,1.3286,8.9441,3.6575,3.6575
//ACM_AREAW2// 2.6572,9.8718,5.4864,5.4864,3.9860,10.7999,7.3151,7.3151,5.3147,11.7277
//ACM_AREAW3// 9.1440,9.1440,6.6434,12.6555,10.9728,10.9728,7.9720,13.5832,12.8015,12.8015
//ACM_AREAW4// 9.3009,14.5114,14.6302,14.6302,10.6295,15.4392,16.4591,16.4591,11.9582,16.3672
//ACM_AREAH1// 0,0,0,3.6372,0.6061,0.6061,0.4909,3.9463,1.2122,1.2122
//ACM_AREAH2// 0.9818,4.2553,1.8186,1.8186,1.4723,4.5643,2.4247,2.4247,1.9636,4.8734
//ACM_AREAH3// 3.0309,3.0309,2.4544,5.1824,3.6372,3.6372,2.9453,5.4913,4.2434,4.2434
//ACM_AREAH4// 3.4363,5.8003,4.8495,4.8495,3.9272,6.1093,5.4559,5.4559,4.4180,6.4186
//ACM_AREAV1// 0,0,0,6.8579,0.7619,0.7619,1.0880,7.3976,1.5239,1.5239
//ACM_AREAV2// 2.1763,7.9372,2.2860,2.2860,3.2646,8.4764,3.0478,3.0478,4.3529,9.0164
//ACM_AREAV3// 3.8099,3.8099,5.4411,9.5558,4.5720,4.5720,6.5293,10.0956,5.3337,5.3337
//ACM_AREAV4// 7.6177,10.6351,6.0959,6.0959,8.7059,11.1745,6.8579,6.8579,9.7938,11.7144
//ACM_CAREAW1// 8.2292,8.2292,9.9870,11.5902,9.1440,9.1440,10.6513,12.1745,10.0584,10.0584
//ACM_CAREAW2// 11.3156,12.7587,10.9728,10.9728,11.9799,13.3430,11.8872,11.8872,12.6443,13.9272
//ACM_CAREAW3// 12.8015,12.8015,13.3090,14.5114,13.7159,13.7159,13.9729,15.0956,14.6302,14.6302
//ACM_CAREAW4// 14.6377,15.6798,15.5445,15.5445,15.3020,16.2639,16.4591,16.4591,15.9664,16.8481
//ACM_CAREAH1// 0,0,1.8186,3.6372,0.6061,0.6061,2.3094,4.0370,1.2122,1.2122
//ACM_CAREAH2// 2.8004,4.4372,1.8186,1.8186,3.2913,4.8371,2.4247,2.4247,3.7822,5.2371
//ACM_CAREAH3// 3.0309,3.0309,4.2729,5.6371,3.6372,3.6372,4.7638,6.0370,4.2434,4.2434
//ACM_CAREAH4// 5.2547,6.4369,4.8495,4.8495,5.7458,6.8369,5.4559,5.4559,6.2367,7.2368
//ACM_CAREAV1// 0,0,1.7144,5.1434,0.7619,0.7619,2.8027,5.9573,1.5239,1.5239
//ACM_CAREAV2// 3.8907,6.7712,2.2860,2.2860,4.9791,7.5851,3.0478,3.0478,6.0672,8.3992
//ACM_CAREAV3// 3.8099,3.8099,7.1557,9.2131,4.5720,4.5720,8.2439,10.0270,5.3337,5.3337
//ACM_CAREAV4// 9.3322,10.8409,6.0959,6.0959,10.4202,11.6548,6.8579,6.8579,11.5087,12.4687
wing_area = 2250
//wing_area = 2044,4
wing_span = 123.2
wing_root_chord = 16.4
wing_dihedral = -1
wing_incidence = 3.000
wing_twist = -4.000
oswald_efficiency_factor = 0.804921551
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = -16.00
wing_pos_apex_vert = -1.25
htail_area = 436.000
htail_span = 44
htail_pos_lon = -67
htail_pos_vert = 25.24
htail_incidence = -3.000
htail_sweep = 40
vtail_area = 341.000
vtail_span = 18.53
vtail_sweep = 45
vtail_pos_lon = -46.15
vtail_pos_vert = 8.18
elevator_area = 91.0296
aileron_area = 37.500
rudder_area = 62.500
elevator_up_limit = 29.000
elevator_down_limit = 16.000
aileron_up_limit = 20.000
aileron_down_limit = 20.000
rudder_limit = 26.000
elevator_trim_limit = 20.000
spoiler_limit = 60.000
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 1

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[flight_tuning]
cruise_lift_scalar=1.000 
parasite_drag_scalar=1.000 
induced_drag_scalar=1.000 
elevator_effectiveness=1.000 
aileron_effectiveness=1.000 
rudder_effectiveness=1.000 
pitch_stability=1.000 
roll_stability=1.000 
yaw_stability=1.000 
elevator_trim_effectiveness=1.000 
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.000 

[TurbineEngineData]
fuel_flow_gain=0.002 
inlet_area=27,696
rated_N2_rpm=29920.000 
static_thrust=19000.000 
//static_thrust=1600.000 
afterburner_available=0 
reverser_available=1.000 

[jet_engine]
thrust_scalar=1.000 

[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 = 0.3  //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=60.0, -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 

[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

[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

[Reference Speeds] 
flaps_up_stall_speed=120 
full_flaps_stall_speed=100.000 
cruise_speed=480.000 
max_mach=0.90 
max_indicated_speed=370                   //Red line (KIAS) 

[stall_warning]
type=2
[Flaps.0]
type= 1
span-outboard= 0.630
extending-time= 20.000
damaging-speed= 161.900
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= 15.000, 0.000
flaps-position.2= 28.000, 0.000
flaps-position.4= 45.000, 0.000