[fltsim.0] title=FSP Advanced Products MD-11 Continental sim=md11 model=vc panel= sound= texture=1 atc_id=CAL atc_airline=Continental atc_flight_number=950 ui_manufacturer=McDonnell-Douglas/Boeing ui_type=McDonnell Douglas MD-11 ui_variation=Continental V2 No VC description=Overland Co.,Ltd. Products --- McDonnell Douglas MD-11\n\nL1 L2 Cabin Door [Shift+E] then [1]\nCargo Door [Shift+E] then [2]\nL4/R4 Cabin Door Wing Fold/Extend [General] visual_damage=0 // 0=off, 1=on atc_type=MD atc_model=MD11 editable=0 performance=Cruise Speed\t 473kt\nMaximum Range\t6,821 nm\nService Ceiling\t32,400 ft\nMax Takeoff Weight\t602,555 lb\nSeating\t\t270 to 405\nCargo Capacity\t3,552 CU ft\n [WEIGHT_AND_BALANCE] max_gross_weight=602555 // (pounds) empty_weight=286965 // (pounds) reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0= 2376, 0, 0, 1.75, Crew station_load.1= 17300, 0, 0, 1.75, Cargo station_load.2= 3168, 0, 0, 0.00, Farst station_load.3= 7524, 0, 0, 0.00, Business station_load.4= 26136, 0, 0, 0.00, Economy ;Moments of Inertia empty_weight_pitch_MOI= 8000000 empty_weight_roll_MOI= 15500000 empty_weight_yaw_MOI= 12300000 empty_weight_coupled_MOI=0.0 [flight_tuning] cruise_lift_scalar=1.1 parasite_drag_scalar=1.16 induced_drag_scalar=1.200 elevator_effectiveness=1.08 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 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0= 10.2, -26.6, -8.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-87.5, 0.0, 14.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.2= 10.2, 26.6, -8.4 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1 //Scalar for fuel flow efficiency min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.00200 //Gain on fuel flow inlet_area=76.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=60000 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=1.00 [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, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 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, 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 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0=1, 75.42, 0.00, -15.50, 1181.1, 0, 2.220, 70.0, 1.43, 2.0, 0.8235, 7.0, 8.0, 0, 185.0, 250.0 //nose point.1=1, -7.50, -18.00, -15.80, 1574.8, 1, 2.520, 0.0, 1.15, 2.8, 0.8470, 8.1, 10.1, 2, 185.0, 250.0 //left main point.2=1, -7.50, 18.00, -15.80, 1574.8, 2, 2.520, 0.0, 1.15, 2.8, 0.8470, 8.1, 10.1, 3, 185.0, 250.0 //right main point.3=1, -7.75, 0.00, -15.60, 1574.8, 0, 2.520, 0.0, 1.55, 2.8, 0.8470, 8.1, 10.1, 0, 185.0, 250.0 //center main point.4=2, -14.17, -84.80, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 //left wing point.5=2, -14.17, 84.80, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 //right wing point.6=2, -83.33, 0.00, 2.50, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, point.7=2, 96.67, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 //aft fuselage scrape static_pitch=-0.16 static_cg_height=14.8 gear_system_type=0 [Views] eyepoint=91.8, -1.55, 5.6, [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.2 // 0.0 .. 1.0 extending-time=25 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=15 // degrees flaps-position.3=22 // degrees flaps-position.4=25 // degrees flaps-position.5=28 // degrees flaps-position.6=35 // degrees flaps-position.7=50 // degrees damaging-speed=255 // KIAS blowout-speed=300 // KIAS lift_scalar=0.55 drag_scalar=0.55 pitch_scalar=0.55 system_type=1 //Hydraulic [flaps.1] type=1 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=23 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=15 // degrees flaps-position.3=22 // degrees flaps-position.4=25 // degrees flaps-position.5=28 // degrees flaps-position.6=35 // degrees flaps-position.7=50 // degrees damaging-speed=255 // KIAS blowout-speed=300 // KIAS lift_scalar=0.35 drag_scalar=0.35 pitch_scalar=0.35 system_type=1 //Hydraulic [flaps.2] type=2 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=4 // seconds flaps-position.0=0 // degrees flaps-position.1=0.5 // degrees flaps-position.2=0.5 // degrees flaps-position.3=0.5 // degrees flaps-position.4=0.5 // degrees flaps-position.5=1.0 // degrees flaps-position.6=1.0 // degrees flaps-position.7=1.0 // degrees damaging-speed=260 // KIAS blowout-speed=300 // KIAS lift_scalar=0.05 drag_scalar=0.05 pitch_scalar=0.05 system_type=1 //Hydraulic [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 [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 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.1 = 1, 11.30, 0.00, 12.20, fx_beaconb , light.2 = 1, 11.30, 0.00, 12.20, fx_beaconb , light.3 = 1, -38.00, 0.00, -8.00, fx_beaconh , light.4 = 1, -38.00, 0.00, -8.00, fx_beaconh , light.5 = 5, 28.48, 9.94, 1.78, fx_navwhi , light.6 = 5, 28.48,-9.94, 1.78, fx_navwhi , light.7 = 5, 30.48, 9.36, -1.32, fx_navwhi , light.8 = 5, 30.48,-9.36, -1.32, fx_navwhi , light.9= 4, 91.30, -1.15, 1.05, fx_vclighth1, light.10= 4, 89.80, -0.15, 4.55, fx_vclight, light.11= 5, 50.10, 5.65, 1.52, MD80_INSPEC , //right wing inspection light light.11= 5, 50.10, -5.65, 1.52, MD80_INSPEC , //left wing inspection light [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [fuel] Center1= -14.0, 0.0, -5.0, 9621.2, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2= 11.0, 0.0, -5.0,14727.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain= -4.0, -35.0, 0.0, 6107.5, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain= -4.0, 35.0, 0.0, 6107.5, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center3= 21.0, 0.0, -5.0, 1958.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=3648.8 //Square feet wing_span=169.6 //Feet wing_root_chord=34.0 //Feet wing_dihedral=6.2 //Degrees wing_incidence=1.0 //Degrees wing_twist=0.0 //Degrees oswald_efficiency_factor=0.85 //Measure of lift effeciency of wing wing_winglets_flag=1 //Are winglets available? wing_sweep=34.5 //Degrees, wing leading edge wing_pos_apex_lon=30.2 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=1.0 //Feet, vertical distance from reference point, positive going up htail_area=911.0 //Square feet htail_span=58.7 //Feet htail_pos_lon=-70.0 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=8.0 //Feet, vertical distance from reference point, positive going up htail_incidence=-1.2 //Degrees htail_sweep=32.0 //Degrees, horizontal tail leading edge vtail_area=623.0 //Square feet vtail_span=30.3 //Feet, tip to body vtail_sweep=35.0 //Degrees, vertical tail leading edge vtail_pos_lon=-62.3 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=12.0 //Feet, vertical distance from reference point, positive going up elevator_area=167.0 //Square feet aileron_area=120.0 //Square feet rudder_area=138.0 //Square feet elevator_up_limit=35.0 //Degrees elevator_down_limit=20.0 //Degrees aileron_up_limit=25.0 //Degrees aileron_down_limit=15.0 //Degrees rudder_limit=25.0 //Degrees elevator_trim_limit=20.0 //Degrees spoiler_limit=50.0 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=3 //Aileron to spoileron gain min_ailerons_for_spoilerons=10 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=150.0 //Knots True (KTAS) full_flaps_stall_speed=120.0 //Knots True (KTAS) cruise_speed=322.0 //Knots True (KTAS) max_indicated_speed=473.000000 max_mach=0.880000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1500.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8; use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode. default_pitch_mode=0 default_bank_mode=0 max_pitch=10.000000 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=25.000000 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 [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 [brakes] toe_brakes_scale=0.489926 ; brakes_scale 0 to none 1 to hard parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=2 [turn_indicators] turn_indicator.0=1,0 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.12,0.11 ;Percent per second [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0.0
