[fltsim.0] title=FFX DC-10-30 United Airlines NC sim=FFXDC1030 model=30 panel= sound= texture=ua90 kb_checklists= kb_reference= ui_manufacturer=FFX ui_type=DC10-30 ui_variation=United 90 visual_damage=0 description=FFX DC10-30 United Airlines NC by Mike Baumann atc_heavy=1 atc_id=N1855U atc_airline=United atc_flight_number=103 [General] atc_type=MCDONNELDOUGLAS atc_model=DC10 editable=0 performance=Engines: SEE ENGINE SECTION\nFuel capacity: 36,554 USG (244,912 lb @ 6.7 lb USG)\nMax speed: 350 kts IAS or Mach 0.88\nFlap settings: 5-15-22-35-50\nMax operating altitude: 42,000 Ft\nTypical cruise setting: FL310-370 @ Mach 0.82 [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 [flight_tuning] cruise_lift_scalar= 1.10 parasite_drag_scalar= 1.20 induced_drag_scalar= 1.10 elevator_effectiveness= 0.90 aileron_effectiveness= 0.90 rudder_effectiveness= 1.00 pitch_stability= 1.20 roll_stability= 1.20 yaw_stability= 1.00 elevator_trim_effectiveness= 1.20 aileron_trim_effectiveness= 1.00 rudder_trim_effectiveness= 1.00 //Series 30// //Design gross weight (ramp) 575,000 lb (260,820 kg) //Maximum takeoff weight 572,000 lb (259,459 kg) //Design landing weight (1) 405,000 lb (182,766 kg) //Maximum zero fuel weight 368,000 lb (166,924 kg) //Operator's empty weight 267,996 lb (121,563 kg) //Fuel capacity 36,650 USgal (138,735L) //245,566 lb //(111,388 kg) //Weight limited payload 100,809 lb (45,726 kg) //Level flight speed 600+ mph (965 km/h) //FAA takeoff field lgth-std.wght 9,650 ft(2,847 m) //FAA landing field lgth-std.wght 5,960 ft(1,758 m) //Design range (2) 5,860 mi //5,096 nmi //9,429 km // (1)Higher weights are available. // (2)277 passengers and baggage; domestic reserves. // Passenger Capacity 250-380 [WEIGHT_AND_BALANCE] max_gross_weight= 575000.00 empty_weight= 267996.00 reference_datum_position= 0.00, 0.00, 0.00 empty_weight_CG_position= 0.00, 0.00, 0.00 station_load.0= 2400, 65.50,-5.00, 1.50 station_load.1= 2900, 65.50, 5.00, 1.50 station_load.2= 1000, 59.00,-5.00, 1.50 station_load.3= 2100, 59.00, 5.00, 1.50 station_load.4= 3200, 52.50,-5.00, 1.50 station_load.5= 850, 52.50, 5.00, 1.50 station_load.6= 2100, 46.00,-5.00, 1.50 station_load.7= 2050, 46.00, 5.00, 1.50 station_load.8= 1000, 39.50,-5.00, 1.50 station_load.9= 1250, 39.50, 5.00, 1.50 station_load.10= 2200, 33.00,-5.00, 1.50 station_load.11= 1450, 33.00, 5.00, 1.50 station_load.12= 2050, 26.50,-5.00, 1.50 station_load.13= 1700, 26.50, 5.00, 1.50 station_load.14= 1650, 20.00,-5.00, 1.50 station_load.15= 2000, 20.00, 5.00, 1.50 station_load.16= 3000, -15.00,-5.00, 1.50 station_load.17= 2450, -15.00, 5.00, 1.50 station_load.18= 1100, -21.00,-5.00, 1.50 station_load.19= 2000, -21.00, 5.00, 1.50 station_load.20= 2800, -27.00,-5.00, 1.50 station_load.21= 1000, -27.00, 5.00, 1.50 station_load.22= 2000, -33.00,-5.00, 1.50 station_load.23= 2150, -33.00, 5.00, 1.50 station_load.24= 1150, -39.00,-5.00, 1.50 station_load.25= 1700, -39.00, 5.00, 1.50 station_load.26= 500, 77.00,-3.00, 9.50 station_load.27= 500, 77.00, 3.00, 9.50 station_load.28= 1020, 56.66,-4.00, 9.50 station_load.29= 680, 56.66, 0.00, 9.50 station_load.30= 1260, 56.66, 4.00, 9.50 station_load.31= 1020, 36.31,-6.00, 9.50 station_load.32= 850, 36.31, 0.00, 9.50 station_load.33= 680, 36.31, 6.00, 9.50 station_load.34= 1200, 18.97, 0.00, 9.50 station_load.35= 1200, 15.97, 0.00, 9.50 station_load.36= 120,-10.64, 0.00, 9.50 station_load.37= 120,-10.64, 0.00, 9.50 station_load.38= 10220,-24.73,-6.00, 9.50 station_load.39= 10220,-24.73, 0.00, 9.50 station_load.40= 10220,-24.73, 6.00, 9.50 station_load.41= 1200,-45.07,-3.00, 9.50 station_load.42= 1220,-45.07, 3.00, 9.50 station_load.43= 8900, 14.00,-29.25,-2.80 station_load.44= 8900,-78.50, 0.00, 22.50 station_load.45= 8900, 14.00, 29.25,-2.80 station_load.46= 240, 87.75,-2.30, 9.50 station_load.47= 180, 87.75, 2.30, 9.50 station_load.48= 225, 86.75, 2.00, 9.50 station_load.49= 5500, -50.00, 0.00, 2.50 max_number_of_stations= 50 empty_weight_pitch_MOI= 28900000.00 empty_weight_roll_MOI= 15400000.00 empty_weight_yaw_MOI= 45100000.00 empty_weight_coupled_MOI= 401000.00 [GeneralEngineData] engine_type= 1 Engine.0= 14.00, -29.25, -2.80 Engine.1= -78.50, 0.00, 22.50 Engine.2= 14.00, 29.25, -2.80 fuel_flow_scalar= 0.600 //Series 30 GECF6-50C 51000 LBS MAX [TurbineEngineData] bypass_ratio= 4.8000 fuel_flow_gain= 0.002 inlet_area= 61.000 rated_N2_rpm= 29920.000 static_thrust= 51000.000 afterburner_available= 0 reverser_available= 1 [jet_engine] thrust_scalar= 1.20 [airplane_geometry] wing_area= 3647.00 wing_span= 165.40 wing_root_chord= 39.35 wing_dihedral= 4.20 wing_incidence= 0.70 wing_twist= 0.00 oswald_efficiency_factor= 0.90 wing_winglets_flag= 0 wing_sweep= 35.00 wing_pos_apex_lon= 20.50 wing_pos_apex_vert= 2.60 htail_area= 844.88 htail_span= 71.20 htail_pos_lon= -56.00 htail_pos_vert= 10.00 htail_incidence= 0.80 htail_sweep= 35.00 vtail_area= 452.60 vtail_span= 35.20 vtail_sweep= 35.00 vtail_pos_lon= -60.50 vtail_pos_vert= 28.50 elevator_area= 60.35 aileron_area= 50.28 rudder_area= 40.32 elevator_up_limit= 26.00 elevator_down_limit= 26.00 aileron_up_limit= 26.00 aileron_down_limit= 26.00 rudder_limit= 26.00 elevator_trim_limit= 17.00 spoiler_limit= 60.00 spoilerons_available= 1 aileron_to_spoileron_gain= 1.00 min_ailerons_for_spoilerons= 1.00 min_flaps_for_spoilerons= 0 [Reference Speeds] //AI USE ONLY!! No effect on normal flight. flaps_up_stall_speed= 140 full_flaps_stall_speed= 120 cruise_speed= 600 [contact_points] point.0=1, 67.00, 0.00, -11.90, 1200, 0, 2.0, 68, 0.900, 2.0, 0.7, 8.0, 9.0, 0, 180, 250 //nose point.1=1, -12.00, -18.20, -11.70, 1500, 1, 2.0, 0, 0.887, 2.5, 0.6, 9.9, 10.9, 2, 180, 250 //left main point.2=1, -12.00, 18.20, -11.70, 1500, 2, 2.0, 0, 0.887, 2.5, 0.6, 9.1, 10.1, 3, 180, 250 //right main point.3=1, -11.00, 0.00, -11.70, 1500, 0, 2.0, 0, 0.887, 2.5, 0.6, 9.6, 10.6, 3, 180, 250 //center main point.4=2, -34.00, -86.00, 8.40, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 5, 0, 0 //left wing point.5=2, -34.00, 86.00, 8.40, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 6, 0, 0 //right wing point.6=2, -97.50, 0.00, 6.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 9, 0, 0 //nose point.7=2, -93.50, 0.00, 25.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //#2 engine point.8=2, -85.50, 0.00, 11.50, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //aft fuselage point.9=2, -46.50, 0.00, -1.65, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //aft fuselage scrape max_number_of_points= 10 static_pitch= 0.050 static_cg_height= 10.90 [Flaps.0] type= 1 span-outboard= 0.800 extending-time= 15.000 damaging-speed= 280 blowout-speed= 300 lift_scalar= 0.900 drag_scalar= 1.200 pitch_scalar= 0.300 system_type= 1 flaps-position.0= 0.000 flaps-position.1= 5.000 flaps-position.2=15.000 flaps-position.3=22.000 flaps-position.4=35.000 flaps-position.5=50.000 [Flaps.1] type= 2 span-outboard= 0.990 extending-time= 5.000 damaging-speed= 280 blowout-speed= 300 lift_scalar= 0.900 drag_scalar= 0.900 pitch_scalar= 0.100 system_type= 1 flaps-position.0= 0.000 flaps-position.1= 5.000 flaps-position.2=15.000 flaps-position.3=22.000 flaps-position.4=35.000 [electrical] autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 17.0 light_nav = 0, 5 , 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, 5 , 17.0 pitot_heat = 0, 15, 17.0 additional_system = 0, 20, 17.0 marker_beacon = 1, 2, 17.0 starter1 = 0, 20, 17.0 starter2 = 0, 20, 17.0 starter3 = 0, 20, 17.0 auto_brakes = 0, 15, 17.0 hydraulic_pump = 0, 2, 17.0 fuel_transfer_pump = 0, 5, 17.0 max_battery_voltage = 28.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps= 60.0 electric_always_available = 1 [pitot_static] vertical_speed_time_constant=99 [exits] number_of_exits = 2 exit_rate.0 = 0.105 //L2 main exit door (shift+E) exit_rate.1 = 0.105 //L1 exit door (shift+E2) [TailHook] //landing lights (normally shift+T) tailhook_length= 4 tailhook_position= 0.0, 0.0, 0.0 cable_force_adjust= 0.5 [folding_wings] //cargo doors and R2+L4 galley service doors (normally shift+F) wing_fold_system_type= 4 fold_rates= 0.110,0.110 [Views] //PILOTS CORRECT VIEWPOINT! IF YOU WANT WING VIEWS, ADJUST YOUR PANEL CONFIG! eyepoint=89.75, -2.30, 11.20 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=nose gear light.0=1, -0.90, 0.00, 18.70, DC10BCNU , //upper beacon light.1=1, -30.70, 0.00, -3.00, DC10BCNL , //lower beacon light.2=3, -74.00, -12.00, 34.50, DC10logo , //left logo splash light.3=3, -74.00, 12.00, 34.50, DC10logo , //right logo splash light.4=5, 88.35, -14.50, -4.00, DC10landing , //left landing light splash light.5=5, 88.35, 14.50, -4.00, DC10landing , //right landing light splash light.6=6, 82.00, 0.00, -3.50, DC10wing , //nose gear splash [keyboard_response] elevator= 100, 200 aileron= 100, 200 rudder= 100, 200 [direction_indicators] direction_indicator.0=3,0 [fuel] Center1= 15.00, 0.00, 0.00, 9766, 0 //tank 2 Center2= 0.00, 0.00, 3.00, 13000, 0 //upper aux Center3= 0.00, 0.00, -1.00, 1642, 0 //lower aux LeftMain= -5.00, -27.50, 5.00, 6075, 0 //tank 1 RightMain= -5.00, 27.50, 5.00, 6075, 0 //tank 3 fuel_type= 2 number_of_tank_selectors= 1 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 800 autothrottle_available= 1 use_no_default_pitch= 1 use_no_default_bank= 1 pitch_takeoff_ga= 8 autothrottle_arming_required= 1 autothrottle_takeoff_ga= 1 autothrottle_max_rpm= 95 [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 [SMOKESYSTEM] [EFFECTS] wake= fx_wake water= fx_spray dirt= fx_tchdrt concrete= fx_sparks touchdown= fx_tchdwn, 1
