[fltsim.0] title=FSP MD83 Austrian Airlines sim=fsp_md81 model= panel= sound= texture=aua atc_id=OE-LMD atc_airline=Austrian atc_flight_number=83 ui_manufacturer=AI_Plane ui_type="MD-83" ui_variation=Austrian Airlines description=REPAINT:Imre Kiss FD:hiro (http://www.nasuinfo.or.jp/freespace/yashiomi/) [fltsim.1] title=FSP MD83 Austrian Airlines dirty sim=fsp_md81 model= panel= sound= texture=aua dirty atc_id=OE-LMD atc_airline=Austrian atc_flight_number=83 ui_manufacturer=AI_Plane ui_type="MD-83" ui_variation=Austrian Airlines (dirty) description=REPAINT:Imre Kiss FD:hiro (http://www.nasuinfo.or.jp/freespace/yashiomi/) [General] atc_type=Boeing atc_model=MD83 editable=1 performance=Cruise Speed\t.74 Mach\nMaximum Range\t2,059 nm\nService Ceiling\t36,089 ft\nMax Takeoff Weight\t138,500 lb\nSeating\t\t147 to 168\nCargo Capacity\t1,373 CU ft\n [WEIGHT_AND_BALANCE] max_gross_weight=140000 // (pounds) empty_weight=59686 // (pounds) reference_datum_position=77.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-66.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=0.0, -69.5, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=1651967 empty_weight_roll_MOI=465681 empty_weight_yaw_MOI=1447094 empty_weight_coupled_MOI=0 [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=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=-103.6, -8.5, 0.6 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-103.6, 8.5, 0.6 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=10.4 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=21000 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=1.0 [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, -9.20, 0.00, -8.0, 1500, 0, 1.08, 65.0, 1.00, 2.5, 0.9, 7.0, 5.0, 0 point.1=1, -93.10, -8.33, -9.1, 3000, 1, 1.85, 1.6, 1.50, 2.5, 0.8, 7.0, 7.0, 2 point.2=1, -93.10, 8.33, -9.1, 3000, 2, 1.85, 1.6, 1.50, 2.5, 0.8, 7.0, 7.0, 3 point.3=2, -95.75, -53.92, -1.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5 point.4=2, -98.75, 53.92, -1.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6 point.5=2, -139.00, 0.00, 3.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9 point.6=2, -3.00, 0.00, 0.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4 max_number_of_points=21 static_pitch=-0.8 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=8.0 //feet, altitude of CG when at rest on the ground gear_system_type=0 [Views] eyepoint=-13.3, -1.82, 5.0 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.1] //Outboard Trailing Edge 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=5 // degrees flaps-position.3=15 // degrees flaps-position.4=20 // degrees flaps-position.5=25 // degrees flaps-position.6=30 // degrees damaging-speed=260 // KIAS blowout-speed=300 // KIAS lift_scalar=0.35 drag_scalar=0.35 pitch_scalar=0.35 system_type=1 //Hydraulic [flaps.2] //Inboard Leading Edge Slats 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 damaging-speed=260 // KIAS blowout-speed=300 // KIAS lift_scalar=0.25 drag_scalar=0.25 pitch_scalar=2.5 system_type=1 //Hydraulic [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -95.50, 57, 1.10, fx_navgrem , light.1=3, -95.50, -57, 1.10, fx_navredm , light.2=2, -96.50, -57.20, 1.10, fx_strobeh , light.3=2, -96.50, 57.20, 1.10, fx_strobeh , light.4=1, -48.00, 0.00, 8.00, fx_beaconb , light.5=1, -72.00, 0.00, -4.60, fx_beaconb , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [fuel] Center1=-76.2, 0.0, -6.0, 580.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2=-78.2, 0.0, -6.0, 580.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-78.7, -12.1, -4.0, 2920.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-78.7, 12.1, -4.0, 2920.0, 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=1209.0 //Square feet wing_span=107.8 //Feet wing_root_chord=23.1 //Feet wing_dihedral=3.0 //Degrees wing_incidence=1.3 //Degrees wing_twist=0.0 //Degrees oswald_efficiency_factor=0.8 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=24.5 //Degrees, wing leading edge wing_pos_apex_lon=-61.0 //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=341.0 //Square feet htail_span=40.0 //Feet htail_pos_lon=-134.0 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=0.0 //Degrees htail_sweep=30.0 //Degrees, horizontal tail leading edge vtail_area=168.0 //Square feet vtail_span=14.8 //Feet, tip to body vtail_sweep=25.0 //Degrees, vertical tail leading edge vtail_pos_lon=-131.8 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=10.9 //Feet, vertical distance from reference point, positive going up elevator_area=145.0 //Square feet aileron_area=38.0 //Square feet rudder_area=65.3 //Square feet elevator_up_limit=26.0 //Degrees elevator_down_limit=26.0 //Degrees aileron_up_limit=30.0 //Degrees aileron_down_limit=30.0 //Degrees rudder_limit=30.0 //Degrees elevator_trim_limit=20.0 //Degrees spoiler_limit=60.0 //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=142.0 //Knots True (KTAS) full_flaps_stall_speed=113.6 //Knots True (KTAS) cruise_speed=337.7 //Knots True (KTAS) max_indicated_speed=340.000000 max_mach=0.820020 [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=150.0, 250.0 aileron=150.0, 250.0 rudder=150.0, 250.0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8; 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 [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=0.885037 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=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
