[fltsim.0] title=FFX DC-10-10 Continental "Meatball" sim=SGA1010 model=10 panel= sound= texture=COA kb_checklists=DC10CL kb_reference= ui_manufacturer=McDonnell Douglas ui_type=DC10-10 ui_variation=CONTINENTAL "MEATBALL" visual_damage=1 description=The first DC10 Series 10 flight took place on August 29, 1970. FAA certification was received July 29th, 1971, with initial delivery to launch customers American and United that same month. First revenue flight was by American Airlines (N101AA) on August 5th, 1971. Designed as a medium range transport, a total of 131 Series 10s were produced, including 9 Series 10CF (Convertible Frieghters) which were first delivered in 1973. The Series 10, built around the General Electric CF6-6D engine can carry 270 passengers over 3,630 nautical miles from runways in the 8,900 foot class. repainted by Aki Matsumura atc_heavy=1 atc_id=N68046 atc_airline=CONTINENTAL atc_flight_number=680 atc_parking_types=GATE atc_parking_codes=COA [fltsim.1] [fltsim.2] [General] atc_type=MCDONNELDOUGLAS atc_model=DC10 editable=0 performance=Engines: SEE ENGINE SECTION\nFuel capacity: 21,700 USG (145,810 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= 1.00 parasite_drag_scalar= 1.20 induced_drag_scalar= 1.20 elevator_effectiveness= 0.90 aileron_effectiveness= 0.90 rudder_effectiveness= 1.00 pitch_stability= 1.20 roll_stability= 1.20 yaw_stability= 1.20 elevator_trim_effectiveness= 1.20 aileron_trim_effectiveness= 1.00 rudder_trim_effectiveness= 1.00 [WEIGHT_AND_BALANCE] max_gross_weight= 443000.00 empty_weight= 249600.00 reference_datum_position= 0.00, 0.00, 0.00 empty_weight_CG_position= 0.00, 0.00, 0.00 station_load.0= 15000, 40.00,-5.00, 0.00 station_load.1= 15000, 40.00, 5.00, 0.00 station_load.2= 15000, 10.00,-5.00, 0.00 station_load.3= 15000, 10.00, 5.00, 0.00 station_load.4= 15000,-20.00,-5.00, 0.00 station_load.5= 15000,-20.00, 5.00, 0.00 max_number_of_stations= 6 empty_weight_pitch_MOI= 33898870.00 empty_weight_roll_MOI= 34178600.00 empty_weight_yaw_MOI= 30897370.00 empty_weight_coupled_MOI= 1300.00 [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= 0.500 min_throttle_limit=-0.299927 [TurbineEngineData] bypass_ratio= 1.000 fuel_flow_gain= 0.0019 inlet_area= 61.000 rated_N2_rpm= 29920.000 static_thrust= 40000.000 afterburner_available= 0 reverser_available= 1 [jet_engine] //**FS2002 USERS CHANGE THIS VALUE TO 1.30** thrust_scalar= 1.10 [airplane_geometry] wing_area= 3550.00 wing_span= 155.40 wing_root_chord= 39.35 wing_dihedral= 6.00 wing_incidence= 0.00 wing_twist= -1.00 oswald_efficiency_factor= 0.93 wing_winglets_flag= 0 wing_sweep= 35.00 wing_pos_apex_lon= 20.50 wing_pos_apex_vert= 2.60 htail_area= 422.44 htail_span= 71.20 htail_pos_lon= -56.00 htail_pos_vert= 10.00 htail_incidence= 0.00 htail_sweep= 35.00 vtail_area= 452.00 vtail_span= 24.25 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= 20.60 aileron_up_limit= 19.50 aileron_down_limit= 20.60 rudder_limit= 23.50 elevator_trim_limit= 19.50 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] flaps_up_stall_speed= 140 full_flaps_stall_speed= 120 cruise_speed= 600 max_indicated_speed= 350 max_mach= 0.88 [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 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 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 point.3=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 point.4=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 point.5=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 point.6=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 point.7=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 point.8=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 max_number_of_points= 9 static_pitch= 0.050 static_cg_height= 10.90 gear_system_type=0 [Flaps.0] type= 1 span-outboard= 0.800 extending-time= 20.000 damaging-speed= 280 blowout-speed= 300 lift_scalar= 1.000 drag_scalar= 1.200 pitch_scalar= 0.500 system_type= 1 flaps-position.0= 0.000 flaps-position.1= 0.000 //LEADING EDGE SLATS EXTEND ONLY-TRAILING EDGE FLAPS REMAIN DOCKED flaps-position.2= 5.000 flaps-position.3=15.000 //UNDER MAX TAKEOFF WEIGHT-10,000FT+ EXTENDED LENGTH RUNWAYS-TAKEOFF CONFIGURATION flaps-position.4=22.000 //NORMAL FULL LOAD TAKEOFF CONFIGURATION (WITHIN TAKEOFF WEIGHT LIMITS) flaps-position.5=35.000 //NORMAL LANDING CONFIGURATION WITH APPROPRIATE AIRCRAFT LANDING WEIGHTS flaps-position.6=50.000 //USED ONLY ON WET RUNWAY SUFACES OR RUNWAYS WITH A LENGTH LESS THAN 7000 FEET [Flaps.1] type= 2 span-outboard= 0.990 extending-time= 10.000 damaging-speed= 280 blowout-speed= 300 lift_scalar= 1.000 drag_scalar= 1.200 pitch_scalar= 0.500 system_type= 1 flaps-position.0= 0.000 flaps-position.1=15.000 //NORMAL HALF EXTEND-TAKEOFF CONFIGURATION flaps-position.2=15.000 flaps-position.3=15.000 flaps-position.4=15.000 flaps-position.5=35.000 //FULL EXTEND-LANDING CONFIGURATION flaps-position.6=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_pump1 = 0, 5 , 17.0 fuel_pump2 = 0, 5 , 17.0 fuel_pump3 = 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 hydraulic_pump1 = 0, 2, 17.0 hydraulic_pump2 = 0, 2, 17.0 hydraulic_pump3 = 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 = 0 engine_generator_map= 1, 1, 1, 0 [pitot_static] vertical_speed_time_constant=2.0 [exits] number_of_exits = 2 exit_rate.0 = 0.105 exit_rate.1 = 0.105 [TailHook] //Extends Landing light pods 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 wing_fold_system_type= 4 fold_rates= 0.110,0.110 [Views] eyepoint= 89.20, -2.30, 11.30 //PILOTS CORRECT VIEWPOINT [LIGHTS] //Types: 1EBeacon,2EStrobe,3ENavigation,4ECockpit,5ELanding,6ETaxi,7ERecognition,8EWing,9ELogo,10ECabin (7-10 REQUIRE GAUGE) light.0=1, -0.90, 0.00, 18.70, DC10.4BCNU , light.1=1, -30.90, 0.00, -3.00, DC10.4BCNL , light.2=3, -74.00, -12.00, 34.50, DC10.4logo , light.3=3, -74.00, 12.00, 34.50, DC10.4logo , light.4=5, 80.50, -10.50, 1.10, DC10.4landing , light.5=5, 80.50, 10.50, 1.10, DC10.4landing , [keyboard_response] elevator= 100, 200 aileron= 100, 200 rudder= 100, 200 [direction_indicators] direction_indicator.0=3,0 [fuel] Center1= 0.00, 0.00, 0.00, 9550, 0 //tank 2 LeftMain= 0.00, -27.50, 0.00, 6075, 0 //tank 1 RightMain= 0.00, 27.50, 0.00, 6075, 0 //tank 3 fuel_type= 2 number_of_tank_selectors= 1 electric_pump=0 [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= 115 default_pitch_mode=0 default_bank_mode=0 max_pitch= 10.00 max_pitch_acceleration= 1.00 max_pitch_velocity_lo_alt= 2.00 max_pitch_velocity_hi_alt= 1.50 max_pitch_velocity_lo_alt_breakpoint=20000 max_pitch_velocity_hi_alt_breakpoint=28000 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= 1.00 [Radios] 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 Contrail= fx_contrail startup= fx_smkpuff_m, 1 windshield_rain_effect_available=1 //0= OFF, 1= ON [brakes] toe_brakes_scale= 0.559 parking_brake= 1 [gear_warning_system] gear_warning_available= 1 pct_throttle_limit= 0.099 flap_limit_power= 24.637 flap_limit_idle= 0.974 [hydraulic_system] electric_pumps= 0 engine_map= 1,1,1,0 normal_pressure= 3000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
