[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