[fltsim.0]
title=AI USPP Tu-154B Perm Airlines
sim=fde_Tu-154B2
model=
texture=pal
atc_airline=PERM AIR
ui_manufacturer=AI
ui_type=Tupolev Tu-154B-2
ui_variation=Perm Airlines
description=
atc_parking_codes=PG5


[General]
atc_type=TUPOLEV 
atc_model=TU154 
editable=1 
visual_damage=1
performance=

[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 = 150000
empty_weight = 80170
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 6, 0, 0
empty_weight_pitch_MOI = 3172439
empty_weight_roll_MOI = 2262183
empty_weight_yaw_MOI = 3337024
empty_weight_coupled_MOI = 0
max_number_of_stations = 0

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=1, -59.80, 0, 24.60, fx_beaconh ,
light.1=2, -37.30, 0, -6.00, fx_beaconb ,
light.2=2, 0.00, 0, 0.00, fx_strobe ,

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1
min_throttle_limit = -0.450000
engine.0 = 4.75, -16.1, -4.5
engine.1 = 4.75,  16.1, -4.5

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown=fx_touchdown_h, 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 = 0, 0, 0, 1, 0
LeftMain = -3, -19, 0, 1, 0
RightMain = -3, 19, 0, 1, 0


[contact_points]
point.0=1, 40.00,   0.00, -13.40, 1181.1, 0, 4.5, 55.92, 1.4, 0.600, 0.9, 11.4, 11.6, 0, 220.0, 250.0
point.1=1, -7.75,  -8.58, -13.45, 1574.8, 1, 4.5,  0.00, 1.9, 0.600, 0.9, 10.2, 10.8, 2, 220.0, 250.0
point.2=1, -7.75,   8.58, -13.45, 1574.8, 1, 4.5,  0.00, 1.9, 0.600, 0.9, 10.8, 11.1, 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=0.20
static_cg_height=12.20
gear_system_type=1


[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// 0,0,0,5.9527,1.6044,1.6044,0.8529,6.5081,3.2088,3.2088
//ACM_AREAW2// 1.7058,7.0636,4.8133,4.8133,2.5592,7.6191,6.4176,6.4176,3.4123,8.1745
//ACM_AREAW3// 8.0221,8.0221,4.2652,8.7299,9.6266,9.6266,5.1185,9.2854,11.2307,11.2307
//ACM_AREAW4// 5.9716,9.8409,12.8353,12.8353,6.8246,10.3963,14.4399,14.4399,7.6778,10.9518
//ACM_AREAH1// 0,0,0,4.2367,0.7059,0.7059,0.4074,4.4324,1.4119,1.4119
//ACM_AREAH2// 0.8151,4.6283,2.1182,2.1182,1.2230,4.8242,2.8243,2.8243,1.6304,5.0198
//ACM_AREAH3// 3.5306,3.5306,2.0383,5.2157,4.2367,4.2367,2.4460,5.4116,4.9428,4.9428
//ACM_AREAH4// 2.8536,5.6076,5.6489,5.6489,3.2613,5.8034,6.3550,6.3550,3.6691,5.9993
//ACM_AREAV1// 0,0,0,6.5043,0.7225,0.7225,0.6064,6.5904,1.4451,1.4451
//ACM_AREAV2// 1.2128,6.6764,2.1681,2.1681,1.8192,6.7624,2.8907,2.8907,2.4256,6.8487
//ACM_AREAV3// 3.6135,3.6135,3.0320,6.9348,4.3362,4.3362,3.6384,7.0208,5.0590,5.0590
//ACM_AREAV4// 4.2449,7.1069,5.7817,5.7817,4.8512,7.1929,6.5043,6.5043,5.4576,7.2789
//ACM_CAREAW1// 7.2199,7.2199,6.8151,8.0058,8.0221,8.0221,7.2417,8.3725,8.8240,8.8240
//ACM_CAREAW2// 7.6683,8.7398,9.6266,9.6266,8.0949,9.1068,10.4287,10.4287,8.5214,9.4736
//ACM_CAREAW3// 11.2307,11.2307,8.9477,9.8409,12.0332,12.0332,9.3745,10.2079,12.8353,12.8353
//ACM_CAREAW4// 9.8009,10.5747,13.6373,13.6373,10.2276,10.9419,14.4399,14.4399,10.6541,11.3090
//ACM_CAREAH1// 0,0,2.1182,4.2367,0.7059,0.7059,2.5260,4.5384,1.4119,1.4119
//ACM_CAREAH2// 2.9337,4.8400,2.1182,2.1182,3.3413,5.1420,2.8243,2.8243,3.7490,5.4436
//ACM_CAREAH3// 3.5306,3.5306,4.1567,5.7455,4.2367,4.2367,4.5644,6.0472,4.9428,4.9428
//ACM_CAREAH4// 4.9720,6.3488,5.6489,5.6489,5.3797,6.6508,6.3550,6.3550,5.7873,6.9524
//ACM_CAREAV1// 0,0,1.6260,4.8783,0.7225,0.7225,2.2325,5.2245,1.4451,1.4451
//ACM_CAREAV2// 2.8389,5.5707,2.1681,2.1681,3.4453,5.9169,2.8907,2.8907,4.0517,6.2631
//ACM_CAREAV3// 3.6135,3.6135,4.6581,6.6093,4.3362,4.3362,5.2645,6.9558,5.0590,5.0590
//ACM_CAREAV4// 5.8709,7.3020,5.7817,5.7817,6.4773,7.6483,6.5043,6.5043,7.0837,7.9945
wing_area = 1834
wing_span = 123.49
wing_root_chord = 19.53
wing_dihedral = 6.19
wing_incidence = 1.0
wing_twist = -0.5
oswald_efficiency_factor = 0.85
wing_winglets_flag = 0
wing_sweep = 35
wing_pos_apex_lon = 13.60
wing_pos_apex_vert = 0
htail_area = 449
htail_span = 35.32
htail_pos_lon = -62.99
htail_pos_vert = 0
htail_incidence = 0.0
htail_sweep = 45
vtail_area = 292
vtail_span = 21.34
vtail_sweep = 40
vtail_pos_lon = -38.86
vtail_pos_vert = 8.47
elevator_area = 70.5
aileron_area = 26.9
rudder_area = 56.2
elevator_up_limit = 15.00
elevator_down_limit = 19.5
aileron_up_limit = 20.0
aileron_down_limit = 20.0
rudder_limit = 26.0
elevator_trim_limit = 20.0
spoiler_limit = 60.0
aileron_to_spoileron_gain = 3
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 10
min_flaps_for_spoilerons = 0
spoilerons_available = 1

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 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=0.9 
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 

[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=20500                           //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 

[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 = 0.485  //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=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 = 0.1
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.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

[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.3 = 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 

[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=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

[Reference Speeds]
flaps_up_stall_speed=122.0                 //Knots True (KTAS)
full_flaps_stall_speed=103.0                 //Knots True (KTAS)
cruise_speed=477.0                 //Knots True (KTAS)
max_mach                = 0.86
max_indicated_speed     = 340                   //Red line (KIAS)

[stall_warning]
type=2