[fltsim.0]

title=Antonov An-148 Turkish airlines
sim=Antonov An-148
model=
panel=
sound=
texture=thy
checklists=
ui_manufacturer=Antonov
ui_type=An-148
ui_variation=Turkish Airlines
description=Antonov An-148
atc_id_color=0x00000000
atc_heavy=1
atc_id_enable=1
atc_id_font=Tahoma,-24,1,800,0
visual_damage=1
atc_id=
atc_airline=Turkish
atc_flight_number=
atc_heavy=0

[General]
performance=Samdim Design.\nAntonov An-148\nYear: 2005 Crew: 2 
editable=1 
Category=airplane

[weight_and_balance]

// ACM V2.5
max_gross_weight = 58201.5
empty_weight = 38801
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 3072439
empty_weight_roll_MOI = 2063372
empty_weight_yaw_MOI = 2088164
empty_weight_coupled_MOI = 0
max_number_of_stations = 1

station_load.0 = 0.000000,0.000000,0.000000,0.000000


[lights]

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

light.0 = 1, -34.16, 0, 6.5, fx_beaconh
light.1 = 5, -2.77, -5.32, -4.78, fx_landing
light.2 = 5, 33.05, 0.11, -4.90, fx_landing
light.3 = 10, 27.51, 0, 2.27, fx_vclight
light.4 = 5, -2.27, 5.32, -4.78, fx_landing

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.000000
min_throttle_limit = -0.149902
engine.0 = 6, -16, 4.91, 
engine.1 = 6, 16, 4.91, 

[effects]
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 = 1

LeftMain = 0, 0, 0, 733, 0
RightMain = 0, 0, 0, 733, 0


[contact_points]
static_pitch = 0.488892
static_cg_height = 10.5
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7

point.0 = 1, 26.6184, 0, -8.9652, 1800, 0, 1.1, 56, 0.5, 1.58, 0.660489, 4, 4, 0, 0, 300
point.1 = 1, -10.8058, -6.7, -9.5354, 2000, 1, 1.73, 0, 1.1, 1.54, 0.896493, 4, 5, 2, 0, 300
point.2 = 1, -10.8139, 6.7, -9.559, 2000, 2, 1.73, 0, 1.1, 1.54, 0.896493, 4, 5, 3, 0, 300
point.3 = 2, -16.3078, -49.9193, 2.5671, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -16.2136, 50.229, 2.5668, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -53.2731, 0, 0.8687, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 34.4673, 0, -4.6423, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0


[keyboard_response]
elevator = 150.000000, 250.000000
aileron = 150.000000, 250.000000
rudder = 150.000000, 250.000000


[forcefeedback]

[airplane_geometry]
//ACM_AREAW1// 0,0,0,4.8768,1.6224,1.6224,0,4.6329,3.2455,3.2455
//ACM_AREAW2// 0,4.3891,4.8681,4.8681,0,4.1451,6.4910,6.4910,0,3.9014
//ACM_AREAW3// 8.1138,8.1138,0,3.6575,9.7363,9.7363,0,3.4137,11.3591,11.3591
//ACM_AREAW4// 0,3.1698,12.9820,12.9820,0,2.9260,14.6049,14.6049,0,2.6821
//ACM_AREAH1// 0,0,0,3.8099,0.6348,0.6348,0,3.6194,1.2697,1.2697
//ACM_AREAH2// 0,3.4289,1.9048,1.9048,0,3.2385,2.5399,2.5399,0,3.0480
//ACM_AREAH3// 3.1749,3.1749,0,2.8575,3.8099,3.8099,0,2.6670,4.4450,4.4450
//ACM_AREAH4// 0,2.4765,5.0798,5.0798,0,2.2860,5.7150,5.7150,0,2.0954
//ACM_AREAV1// 0,0,0,6.5478,0.7275,0.7275,0,6.0240,1.4550,1.4550
//ACM_AREAV2// 0,5.5001,2.1826,2.1826,0,4.9762,2.9100,2.9100,0,4.4524
//ACM_AREAV3// 3.6377,3.6377,0,3.9286,4.3652,4.3652,0,3.4047,5.0927,5.0927
//ACM_AREAV4// 0,2.8810,5.8203,5.8203,0,2.3571,6.5478,6.5478,0,1.8334
//ACM_CAREAW1// 7.3024,7.3024,2.4384,3.4137,8.1138,8.1138,2.4384,3.3649,8.9252,8.9252
//ACM_CAREAW2// 2.4384,3.3162,9.7363,9.7363,2.4384,3.2674,10.5480,10.5480,2.4384,3.2186
//ACM_CAREAW3// 11.3591,11.3591,2.4384,3.1698,12.1708,12.1708,2.4384,3.1210,12.9820,12.9820
//ACM_CAREAW4// 2.4384,3.0722,13.7936,13.7936,2.4384,3.0236,14.6049,14.6049,2.4384,2.9748
//ACM_CAREAH1// 0,0,1.9048,3.8099,0.6348,0.6348,1.9048,3.7146,1.2697,1.2697
//ACM_CAREAH2// 1.9048,3.6194,1.9048,1.9048,1.9048,3.5241,2.5399,2.5399,1.9048,3.4289
//ACM_CAREAH3// 3.1749,3.1749,1.9048,3.3336,3.8099,3.8099,1.9048,3.2385,4.4450,4.4450
//ACM_CAREAH4// 1.9048,3.1431,5.0798,5.0798,1.9048,3.0480,5.7150,5.7150,1.9048,2.9526
//ACM_CAREAV1// 0,0,1.6368,4.9109,0.7275,0.7275,1.6368,4.6489,1.4550,1.4550
//ACM_CAREAV2// 1.6368,4.3870,2.1826,2.1826,1.6368,4.1251,2.9100,2.9100,1.6368,3.8631
//ACM_CAREAV3// 3.6377,3.6377,1.6368,3.6013,4.3652,4.3652,1.6368,3.3394,5.0927,5.0927
//ACM_CAREAV4// 1.6368,3.0775,5.8203,5.8203,1.6368,2.8155,6.5478,6.5478,1.6368,2.5536
wing_area = 1131.000000
wing_span = 99.78
wing_root_chord = 5.64
wing_dihedral = -1.99
wing_incidence = 0.247192
wing_twist = 0.999756
oswald_efficiency_factor = 2.695767
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 0
wing_pos_apex_vert = 0
htail_area = 323.000000
htail_span = 37.5
htail_pos_lon = -42
htail_pos_vert = 0
htail_incidence = 0.000000
htail_sweep = 0
vtail_area = 355.000000
vtail_span = 13.56
vtail_sweep = 0
vtail_pos_lon = -38.41
vtail_pos_vert = 5.83
elevator_area = 45.750000
aileron_area = 35.400000
rudder_area = 29.240000
elevator_up_limit = 27.501974
elevator_down_limit = 20.626481
aileron_up_limit = 19.480565
aileron_down_limit = 14.896903
rudder_limit = 23.491270
elevator_trim_limit = 19.480565
spoiler_limit = 59.988681
aileron_to_spoileron_gain = 0.000000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000000
min_flaps_for_spoilerons = 0.000000
spoilerons_available = 0
auto_spoiler_available=0
spoiler_extension_time=5.000000
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

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 0

[radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1 
Com.1=1, 0 
Com.2=1, 0 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 0 
Adf.2=1, 0
Transponder.1=1 
Marker.1=1 

[Flaps.0]
type=1
span-outboard=2.500000
extending-time=12.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=10.0,0.000000
flaps-position.2=20.0,0.000000
flaps-position.3=35.0,0.000000

[Flaps.1]
type=2
span-outboard=0.500000
extending-time=4.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=20.0,0.000000

[Reference Speeds]
flaps_up_stall_speed=115.000000 
full_flaps_stall_speed=100.000000 
cruise_speed=260.00000 
max_indicated_speed=464.000000
max_mach=0.700000

[Views]
eyepoint=33.680610,-1.922367,3.6 

[autopilot]
autopilot_available=1 
flight_director_available=0 
default_vertical_speed=1000.000000 
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=95.000000
pitch_takeoff_ga=8.000000 
max_pitch=15.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=30.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[direction_indicators]
direction_indicator.0=3,0 

[TurbineEngineData]
fuel_flow_gain=0.002170 
inlet_area=6.132120 
rated_N2_rpm=29920.000000 
static_thrust=6800.100000 
// 5210 avant
afterburner_available=0 
reverser_available=1 

[brakes]
toe_brakes_scale=1.220740
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[flight_tuning]
cruise_lift_scalar=1.000 
pitch_stability=1.000 
roll_stability=1.000 
yaw_stability=1.000 
parasite_drag_scalar=1.000 
induced_drag_scalar=1.000 
elevator_effectiveness=1.000 
aileron_effectiveness=1.000 
rudder_effectiveness=1.000 
elevator_trim_effectiveness=1.200 
aileron_trim_effectiveness=1.200 
rudder_trim_effectiveness=1.000 

[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0