[fltsim.0] title=McDonnell-Douglas/Boeing MD-83 Shamrock sim=MD_83 model= panel= sound= texture=s2 kb_checklists=MD_83_check kb_reference=MD_83_ref atc_id=N6275S atc_id_color= atc_airline=Shamrock atc_flight_number=125 ui_manufacturer=McDonnell-Douglas/Boeing ui_type=MD-83 ui_variation=Shamrock Airways description=Shamrock Airways serves the eastern half of the United States and also offers flights between Boston and Ireland. This is the heritage scheme, an updating of the colors worn by the DC-3s with which the line was founded. [fltsim.1] title=McDonnell-Douglas/Boeing MD-83 O'Donoghue sim=MD_83 model= panel= sound= texture=o kb_checklists=MD_83_check kb_reference=MD_83_ref atc_id=N7580O atc_id_color= atc_airline= atc_flight_number=1 ui_manufacturer=McDonnell-Douglas/Boeing ui_type=MD-83 ui_variation=O'Donoghue Industries description=O'Donoghue Industries is a world spanning concern founded in the late 1800's. This is what one of their corporate aircraft might look like if they decided to upgrade from a Gulfstream or Citation. [fltsim.2] title=McDonnell-Douglas/Boeing MD-83 Goose Bay sim=MD_83 model= panel= sound= texture=gb kb_checklists=MD_83_check kb_reference=MD_83_ref atc_id=N724GB atc_id_color=0xffffffff atc_airline=Goose_Bay atc_flight_number=54 ui_manufacturer=McDonnell-Douglas/Boeing ui_type=MD-83 ui_variation=Goose Bay Airlines description=Goose Bay Airlines operates out of Goose Bay Newfoundland and serves most of Canada and some parts of the United States. [General] atc_type=Boeing atc_model=MD80 editable=0 performance= [WEIGHT_AND_BALANCE] max_gross_weight=160000 // (pounds) empty_weight=79686 // (pounds) reference_datum_position=77.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-74.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=33000, -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 [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, 25.0, 1.00, 2.5, 0.9, 7.0, 5.0, 0, 120, 250 point.1=1, -83.10, -8.33, -9.4, 3000, 1, 1.85, 0.0, 1.50, 2.5, 0.8, 7.0, 7.0, 2, 120, 250 point.2=1, -83.10, 8.33, -9.4, 3000, 2, 1.85, 0.0, 1.50, 2.5, 0.8, 7.0, 7.0, 3, 120, 250 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=-0.9 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=7.9 //feet, altitude of CG when at rest on the ground [Views] eyepoint=-13.3, -1.82, 5.0 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=20 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=10 // degrees, KIAS flaps-position.2=20 // degrees, KIAS flaps-position.3=30 // degrees, KIAS flaps-position.4=40 // degrees, KIAS damaging-speed=250 // KIAS blowout-speed=300 // KIAS [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, -96.00, 53.70, -0.60, fx_navgrem , light.1=3, -96.00, -53.70, -0.60, fx_navredm , light.2=2, -96.50, -54.20, -0.60, fx_strobeh , light.3=2, -96.50, 54.20, -0.60, fx_strobeh , light.4=4, -12.00, 0.00, 4.50, fx_vclighth , [SMOKESYSTEM] smoke.0=0.00,-130.00,12.00, fx_engsmoke [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 [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=437.7 //Knots True (KTAS) [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; [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
