[fltsim.0] title=Tupolev Tu-124V circa 1962 sim=Tu-124 model= panel= sound= texture=60s kb_checklists= kb_reference= atc_id=45035 atc_airline= atc_flight_number=1259 ui_manufacturer=Tupolev ui_type="Tu-124" ui_variation="Aeroflot 1962-1974" description=Aeroflot 1962-1974 livery\nSCS & Samdim Design\nModel by Dimitri Samborski, panel by Michael Mitin, FDE by Oleg Tchernikov visual_damage=0 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 [fltsim.1] title=Tupolev Tu-124V circa 1974 sim=Tu-124 model= panel= sound= texture=70s kb_checklists= kb_reference= atc_id=45035 atc_airline= atc_flight_number=1259 ui_manufacturer=Tupolev ui_type="Tu-124" ui_variation="Aeroflot 1974-1980" description=Classic 70-ies Aeroflot livery\nSCS & Samdim Design\nModel by Dimitri Samborski, panel by Michael Mitin, FDE by Oleg Tchernikov visual_damage=0 atc_id_font=Verdana,-11,1,600,0 [fltsim.2] title=Tupolev Tu-124V CSA sim=Tu-124 model= panel= sound= texture=CSA kb_checklists= kb_reference= atc_id=OK-TEA atc_airline= atc_flight_number=1259 ui_manufacturer=Tupolev ui_type="Tu-124" ui_variation="CSA" description=Ceskoslovenske Avialinie, 1965\nSCS & Samdim Design\nModel by Dimitri Samborski, panel by Michael Mitin, FDE by Oleg Tchernikov visual_damage=0 atc_id_font=Verdana,-11,1,600,0 [General] atc_type=TUPOLEV atc_model=Tu-124 editable=0 performance="Maximum range: 1134 nm\nMaximum range ceiling: 33100 ft\nCruise speed : M 0.74\nPassengers: 56\nMTOW: 84260 lbs\nTakeoff distance: 7550 ft" Category=airplane [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [weight_and_balance] // ACM V2.5 max_gross_weight = 84435 empty_weight = 49590 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 752312 empty_weight_roll_MOI = 227631 empty_weight_yaw_MOI = 666771 empty_weight_coupled_MOI = 0 max_number_of_stations = 3 station_load.0 = 530.0, 36.7, 0.0, 0.0, station_load.1 = 9270, 2.53, 0, 0 station_load.2 = 3973, 1.62, 0, 0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -16.21, -42.14, -3.63, fx_navredm , light.1 = 3, -16.01, 42.15, -3.66, fx_navgrem , light.2 = 3, -52.26, 0.00, 3.50, fx_navwhih , light.3 = 2, 11.70, 0.00, 6.71, fx_beaconh , light.4 = 2, 21.41, 0.00, -3.29, fx_beaconb , light.5 = 4, 35.08, 0.00, 4.01, fx_vclighth , light.6 = 4, 41.47, 0.00, 0.25, fx_vclight_yellow , light.7 = 4, 25.05, 0.00, 4.70, fx_vclight_yellow , light.8 = 4, -25.11, 0.00, 4.43, fx_vclight_yellow , light.9 = 4, 20.00, 0.00, 5.80, fx_vclight_yellow , light.10 = 4, 2.90, 0.00, 5.80, fx_vclight_yellow , light.11 = 4, -18.00, 0.00, 5.80, fx_vclight_yellow , [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 1.226 min_throttle_limit = -0.250000 engine.0 = 4.75, -7.33, -1.0 engine.1 = 4.75, 7.33, -1.0 [smokesystem] smoke.0 = 4.75, -7.33, -1.0, fx_hjg_cv990a smoke.1 = 4.75, 7.33, -1.0, fx_hjg_cv990a [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 2 electric_pump = 1 Center1 = 1.26, 0, 0, 1151.7, 0 LeftAux = -8, -26.5, 0, 393.27, 0 LeftTip = -15, -34.5, 0, 125, 0 RightAux = -8, 26.5, 0, 393.27, 0 RightTip = -15, 34.5, 0, 125, 0 External1 = 0, -11.6, 0, 633.43, 0 External2 = 0, 11.6, 0, 633.43, 0 [contact_points] static_pitch = 0.04 static_cg_height = 9.5 tailwheel_lock = 0 gear_system_type = 0 max_number_of_points = 8 point.0 = 1, 31.7681, 0, -10.5, 910, 0, 1.082, 35, 0.37, 2.8, 0.78, 10.9, 10.9, 0, 237.5, 260 point.1 = 1, -2.67, -15.6658, -10.0, 1075, 1, 1.418, 0, 0.393, 1.17, 0.79, 12, 11.8, 2, 237.5, 260 point.2 = 1, -2.67, 15.6658, -10.0, 1075, 2, 1.418, 0, 0.393, 1.17, 0.79, 12, 11.9, 3, 237.5, 260 point.3 = 2, -15.2798, -41.9733, -4.0149, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -15.2798, 42.1002, -4.0152, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -50.7378, 0, 1.6709, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 44.546, 0, 0.1633, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.7 = 5, -30.8999, 0.0428, -3.7279, 1600, 0, 0, 50, 0, 0, 1, 2, 2, 0, 0, 0 [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// 0,0,0,5.9253,1.4191,1.4191,0.9937,6.6227,2.8387,2.8387 //ACM_AREAW2// 1.9874,7.3204,4.2579,4.2579,2.9814,8.0179,5.6774,5.6774,3.9753,8.7156 //ACM_AREAW3// 7.0967,7.0967,4.9692,9.4131,8.5158,8.5158,5.9629,10.1106,9.9354,9.9354 //ACM_AREAW4// 6.9566,10.8083,11.3548,11.3548,7.9506,11.5059,12.7741,12.7741,8.9441,12.2033 //ACM_AREAH1// 0,0,0,3.3231,0.5536,0.5536,0.4986,3.6558,1.1073,1.1073 //ACM_AREAH2// 0.9973,3.9883,1.6612,1.6612,1.4960,4.3210,2.2155,2.2155,1.9946,4.6535 //ACM_AREAH3// 2.7692,2.7692,2.4934,4.9861,3.3231,3.3231,2.9923,5.3186,3.8770,3.8770 //ACM_AREAH4// 3.4909,5.6511,4.4310,4.4310,3.9897,5.9836,4.9850,4.9850,4.4885,6.3161 //ACM_AREAV1// 0,0,0,4.1146,0.4571,0.4571,0.4115,4.1971,0.9143,0.9143 //ACM_AREAV2// 0.8233,4.2796,1.3716,1.3716,1.2345,4.3621,1.8286,1.8286,1.6466,4.4446 //ACM_AREAV3// 2.2860,2.2860,2.0583,4.5272,2.7432,2.7432,2.4697,4.6096,3.2002,3.2002 //ACM_AREAV4// 2.8815,4.6921,3.6575,3.6575,3.2932,4.7746,4.1146,4.1146,3.7049,4.8571 //ACM_CAREAW1// 6.3870,6.3870,7.4348,8.6197,7.0967,7.0967,7.9317,9.0576,7.8063,7.8063 //ACM_CAREAW2// 8.4287,9.4953,8.5158,8.5158,8.9257,9.9329,9.2257,9.2257,9.4224,10.3704 //ACM_CAREAW3// 9.9354,9.9354,9.9195,10.8083,10.6450,10.6450,10.4160,11.2460,11.3548,11.3548 //ACM_CAREAW4// 10.9132,11.6836,12.0642,12.0642,11.4103,12.1211,12.7741,12.7741,11.9069,12.5590 //ACM_CAREAH1// 0,0,1.6612,3.3231,0.5536,0.5536,2.1603,3.7388,1.1073,1.1073 //ACM_CAREAH2// 2.6591,4.1546,1.6612,1.6612,3.1577,4.5700,2.2155,2.2155,3.6565,4.9857 //ACM_CAREAH3// 2.7692,2.7692,4.1552,5.4015,3.3231,3.3231,4.6539,5.8171,3.8770,3.8770 //ACM_CAREAH4// 5.1525,6.2328,4.4310,4.4310,5.6514,6.6483,4.9850,4.9850,6.1501,7.0640 //ACM_CAREAV1// 0,0,1.0283,3.0861,0.4571,0.4571,1.4400,3.3331,0.9143,0.9143 //ACM_CAREAV2// 1.8516,3.5801,1.3716,1.3716,2.2636,3.8273,1.8286,1.8286,2.6751,4.0742 //ACM_CAREAV3// 2.2860,2.2860,3.0868,4.3214,2.7432,2.7432,3.4986,4.5685,3.2002,3.2002 //ACM_CAREAV4// 3.9103,4.8154,3.6575,3.6575,4.3220,5.0626,4.1146,4.1146,4.7336,5.3097 wing_area = 1284.93 wing_span = 83.82 wing_root_chord = 19.44 wing_dihedral = -1.0 wing_incidence = 1.0 wing_twist = -1.5 oswald_efficiency_factor = 0.89 wing_winglets_flag = 0 wing_sweep = 35.0 wing_pos_apex_lon = 17.8 wing_pos_apex_vert = 0.0 htail_area = 285.79 htail_span = 32.71 htail_pos_lon = -36.70 htail_pos_vert = 3.70 htail_incidence = -1.0 htail_sweep = 42.0 vtail_area = 131.32 vtail_span = 13.5 vtail_sweep = 42.51 vtail_pos_lon = -39.0 vtail_pos_vert = 8.1 elevator_area = 71.69 aileron_area = 65.23 rudder_area = 61.61 elevator_up_limit = 29.0 elevator_down_limit = 19.9 aileron_up_limit = 20.0 aileron_down_limit = 20.0 rudder_limit = 26.0 elevator_trim_limit = 20.0 spoiler_limit = 52.0 aileron_to_spoileron_gain = 0 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 0 auto_spoiler_available=1 spoiler_extension_time=2.000000 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 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=1.0 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=0.821 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [TurbineEngineData] fuel_flow_gain=0.0010 //Gain on fuel flow inlet_area=8.9462 //Square Feet, engine nacelle inlet area rated_N2_rpm=11700.00 //RPM, second stage compressor rated value static_thrust=12141 //Lbs, max rated static thrust at Sea Level ----12141(12483) afterburner_available=0 //Afterburner available? reverser_available=0 //Thrust reverser available? bypass_ratio=1.00 [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 = 0.885 //Brake scalar auto_brakes=4 [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=36.7, -1.31, 5.5 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] //Trailing Edge Flaps type = 1 // 1 - tail, 2 - lead span-outboard = 0.61 // 0.0 .. 1.0 extending-time = 21 // seconds flaps-position.0 = 0.0 // degrees flaps-position.1 = 10 // degrees flaps-position.2 = 15 // degrees flaps-position.3 = 30 // degrees flaps-position.4 = 30 // degrees damaging-speed = 216 // KIAS blowout-speed = 244 // KIAS lift_scalar = 1.32 drag_scalar = 0.65 pitch_scalar= 0.95 system_type = 0 //Electromechanic [flaps.1] //tormoznoy shchitok type = 2 // 1 - tail, 2 - lead span-outboard = 4.28 // 0.0 .. 1.0 extending-time = 3 // seconds flaps-position.0 = 0.0 // flaps-position.1 = 0.0 // degrees flaps-position.2 = 0.0 // degrees flaps-position.3 = 0.0 // flaps-position.4 = 40.0 // damaging-speed = 167 // KIAS blowout-speed = 216 // KIAS lift_scalar = 0.00 drag_scalar = 1.05 pitch_scalar= 0.0 system_type = 0 //Electromechanic [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, 0 Adf.1=1 Adf.2=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= 1 [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=7 ; max_pitch=12.0 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=162.0 //Knots True (KTAS) full_flaps_stall_speed=134.0 //Knots True (KTAS) cruise_speed=480.0 //Knots True (KTAS) max_mach = 0.85 max_indicated_speed = 345 //Red line (KIAS) [stall_warning] type=2 re feet wing_span = 83.82 //Feet wing_root_chord = 19.44 //Feet wing_dihedral = -1.0 //Degrees wing_incidence = 1.0 //Degrees wing_twist = -2.0 //Degrees oswald_efficiency_factor= 0.89 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 35.0 //Degrees, wing leading edge wing_pos_apex_lon = 6.6 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_area = 285.79 //Square feet htail_span = 32.71 //Feet htail_pos_lon = -40.36 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 5.19 //Feet, vertical distance from reference point, positive going up htail_incidence = -1.0 //Degrees htail_sweep = 42.0 //Degrees, horizontal tail leading edge vtail_area = 131.32 //Square feet vtail_span = 13.5 //Feet, tip to body vtail_sweep = 42.0 //Degrees, vertical tail leading edge vtail_pos_lon = -39.0 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 8.1 //Feet, vertical distance from reference point, positive going up elevator_area = 71.69 //Square feet aileron_area = 65.23 //Square feet rudder_area = 61.61 //Square feet elevator_up_limit = 29.0 //Degrees elevator_down_limit = 19.9 //Degrees aileron_up_limit = 20.0 //Degrees aileron_down_limit = 20.0 //Degrees rudder_limit = 26.0 //Degrees elevator_trim_limit = 20.0 //Degrees spoiler_limit = 52.0 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 0 //Aileron to spoileron gain min_ailerons_for_spoilerons = 0 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate stick_shaker=1 [Reference Speeds] flaps_up_stall_speed=162.0 //Knots True (KTAS) full_flaps_stall_speed=134.0 //Knots True (KTAS) cruise_speed=480.0 //Knots True (KTAS) max_mach = 0.85 max_indicated_speed = 345 //Red line (KIAS) [stall_warning] type=2 [TailHook] tailhook_length=4 tailhook_position = -15.0, 0.0, -1.0 cable_force_adjust = 1.0 [folding_wings] wing_fold_system_type=4 fold_rates=30,30 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0
