[fltsim.0] title=AI Tupolev Tu-134A-3 RusAir sim=TU134 model= panel= sound= texture=RusAir checklists= atc_id=RA-65908 atc_airline=CGI-RUSAIR atc_flight_number= atc_heavy=0 ui_manufacturer=AI_Plane ui_variation=RusAir ui_type=Tu-134A-3 description=AI Tu-134A-3 by George Sukhykh atc_parking_types=GATE,RAMP atc_parking_codes=CGI [General] atc_type=TU atc_model=Tu134A-3 editable=0 performance=Length: 121 ft 6.5 in\nWing span: 95 ft 2 in\nWeight:104,785 lbs (Max T\/O Weight)\nPower: 2 X 12600 lb st Soloviev D-30 III\nPassengers: 84\nCrew:3\nMax cruising speed .82 mach\nMax Ceiling 39,000 ft\nRange: 1,876 miles [pitot_static] vertical_speed_time_constant = 1 [WEIGHT_AND_BALANCE] max_gross_weight = 162900 empty_weight = 82400 reference_datum_position = 0.0, 0.0, 0.0 empty_weight_CG_position = 1.3, 0.0, 0.0 max_number_of_stations = 50 station_load.0 = "170.0, 41.91, -2.0, 1.64, Pilot" station_load.1 = "170.0, 41.91, 2.0, 1.64, Co-Pilot" station_load.2 = "11115.0, 18.9, 0.0, 1.64, Front cabin" station_load.3 = "3505.0, 29.17, 0.0, -3.28, Front cargo" station_load.4 = "4000.0, -50.45, 0.0, 3.05, Rear cargo" station_load.5 = "11310.0, -18.49, 0.0, 1.64, Rear cabin" ;Moments of Inertia empty_weight_roll_MOI = 1725000 empty_weight_pitch_MOI = 2450000 empty_weight_yaw_MOI = 1950000 empty_weight_coupled_MOI = 0 [fuel] LeftMain = -0.82, -6.16, -0.82, 1829.5, 0.0 RightMain = -0.82, 6.16, -0.82, 1829.5, 0.0 LeftAux = -4.93, -26.7, 0.82, 232.0, 0.0 RightAux = -4.93, 26.7, 0.82, 232.0, 0.0 Center1 = 0.0, 0.0, -4.11, 2180.0, 0.0 fuel_type = 2 number_of_tank_selectors = 1 electric_pump = 0 [airplane_geometry] wing_area=1317.5 wing_span=111.25 wing_root_chord=17.67 wing_dihedral=4.499 wing_incidence=-0.784 wing_twist=0.0 oswald_efficiency_factor=0.75 wing_winglets_flag=1 wing_sweep=25.0 wing_pos_apex_lon=16.0 wing_pos_apex_vert=0.0 htail_area=337.0 htail_span=41.67 htail_pos_lon=-50.0 htail_pos_vert=0.0 htail_incidence=0.0 htail_sweep=0.0 vtail_area=249.0 vtail_span=17.992 vtail_sweep=0.0 vtail_pos_lon=-35.83 vtail_pos_vert=5.83 elevator_area=70.5 aileron_area=26.8 rudder_area=56.2 elevator_up_limit=23.0 elevator_down_limit=20.0 aileron_up_limit=18.0 aileron_down_limit=20.0 rudder_limit=25.0 elevator_trim_limit=18.5 spoiler_limit=45.0 spoilerons_available=1 aileron_to_spoileron_gain=1.10 min_ailerons_for_spoilerons=11 min_flaps_for_spoilerons=30 [Reference Speeds] flaps_up_stall_speed = 155.0 full_flaps_stall_speed = 120.0 cruise_speed = 459 max_indicated_speed = 350.0 max_mach=0.88 [Flaps.0] type=1 span-outboard = 0.8 extending-time = 21.0 flaps-position.0 = 0.0 flaps-position.1 = 1.0 flaps-position.2 = 3.0 flaps-position.3 = 5.0 flaps-position.4 = 10.0 flaps-position.5 = 12.0 flaps-position.6 = 13.0 flaps-position.7 = 14.0 flaps-position.8 = 15.0 damaging-speed = 250.0 blowout-speed = 270.0 lift_scalar = 0.85 drag_scalar = 0.8 pitch_scalar = 1.1 system_type = 1 [flaps.1] type=2 span-outboard = 0.8 extending-time = 18 flaps-position.0 = 0.0 flaps-position.1 = 1.0 flaps-position.2 = 3.0 flaps-position.3 = 5.0 flaps-position.4 = 10.0 flaps-position.5 = 12.0 flaps-position.6 = 13.0 flaps-position.7 = 14.0 flaps-position.8 = 15.0 damaging-speed = 260 blowout-speed = 270 lift_scalar = 0.4 drag_scalar = 0.3 pitch_scalar = 1.2 system_type = 1 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 0.80 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 [GeneralEngineData] engine_type = 1 Engine.0 = -50.98, -10.7, -4.4 Engine.1 = -50.98, 10.7, -4.4 fuel_flow_scalar = 1.055 min_throttle_limit = -0.35; [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 29.0 rated_N2_rpm = 29920 static_thrust = 19500 afterburner_available = 0 reverser_available = 1 [jet_engine] thrust_scalar=1.0 [autopilot] autopilot_available = 1 flight_director_available = 1 default_vertical_speed = 800.0 autothrottle_available = 1 autothrottle_arming_required = 1 autothrottle_takeoff_ga = 1 autothrottle_max_rpm = 100 pitch_takeoff_ga = 8.0 autoland_available = 1 use_no_default_pitch = 1 use_no_default_bank = 1 default_pitch_mode =0 default_bank_mode =0 max_pitch = 0.7 max_pitch_acceleration=15.0 max_pitch_velocity_lo_alt=0.78 max_pitch_velocity_hi_alt=1.0 max_pitch_velocity_lo_alt_breakpoint = 5000.0 max_pitch_velocity_hi_alt_breakpoint = 20000.0 max_bank = 25.00 max_bank_acceleration = 1.80 max_bank_velocity = 3.00 max_throttle_rate = 0.10 nav_proportional_control = 9.00 nav_integrator_control = 0.25 nav_derivative_control = 0.00 nav_integrator_boundary = 2.50 nav_derivative_boundary = 0.00 gs_proportional_control = 9.52 gs_integrator_control = 0.26 gs_derivative_control = 0.00 gs_integrator_boundary = 0.70 gs_derivative_boundary = 0.00 yaw_damper_gain = 0.00 [gear_warning_system] gear_warning_available = 0 pct_throttle_limit = 0.1 flap_limit_idle = 5.0 flap_limit_power = 25.5 [brakes] toe_brakes_scale=0.15 parking_brake=1 [hydraulic_system] normal_pressure=3000.0 electric_pumps=0 engine_map=1,1,0,0 [Views] eyepoint=43.22074,-1.723061,4.355627 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 0, 17.0 avionics=1, 0 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 0, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 0 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 0 , 17.0 [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 = 2 attitude_indicator.1 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_td, 1 [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [stall_warning] type=2 [folding_wings] wing_fold_system_type=4 fold_rates=0.11,0.13 [LIGHTS] light.0 = 2, 24.4, 0.00, -4.9, fx_beaconb , light.1 = 2, 24.40, 0.00, 4.90, fx_beaconh , light.2 = 4, 52.20, 0.00, 2.70, fx_vclighth , light.3 = 3, -17.10, -47.47, -4.95, fx_navredm , light.4 = 3, -17.10, 47.47, -4.95, fx_navgrem , light.5 = 3, -53.95, 0.00, 18.4, fx_navwhih , [contact_points] point.0= 1.000, 48.400, 0.000, -10.320, 1181.102, 0.000, 1.235, 59.760, 0.541, 1.100, 0.600, 11.000, 11.000, 0.000, 216.000, 250.000 point.1= 1.000, -3.500, -15.500, -10.600, 1574.803, 1.000, 1.235, 0.000, 0.404, 1.040, 0.690, 10.000, 11.000, 2.000, 216.000, 250.000 point.2= 1.000, -3.500, 15.000, -10.600, 1574.803, 2.000, 1.235, 0.000, 0.404, 1.040, 0.690, 10.000, 11.000, 3.000, 216.000, 250.000 point.3= 1.000, 0.000, -15.000, -10.600, 1574.803, 1.000, 1.235, 0.000, 0.404, 1.040, 0.690, 10.000, 11.000, 2.000, 216.000, 250.000 point.4= 1.000, 0.000, 15.500, -10.600, 1574.803, 2.000, 1.235, 0.000, 0.404, 1.040, 0.690, 10.000, 11.000, 3.000, 216.000, 250.000 point.5= 2.000, -23.167, -47.583, -5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.6= 2.000, -16.980, -47.200, -5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.7= 2.000, 16.300, -5.000, -4.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.8= 2.000, -8.233, -5.000, -5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.9= 2.000, -23.167, 47.583, -5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.10= 2.000, -16.980, 47.200, -5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.11= 2.000, 16.300, 5.000, -4.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.12= 2.000, -8.233, 5.000, -5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.13= 2.000, -47.500, 0.000, 3.200, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.14= 2.000, 61.033, 0.000, -1.700, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.15= 2.000, -53.800, 0.000, 18.400, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 static_pitch= 0.0500 static_cg_height= 10.470 gear_system_type=1 //Hydraulic
