[fltsim.0] title=McBoeing MD-83 soar sim=MD_83 model= panel= sound= texture= kb_checklists=MD_83_check kb_reference=MD_83_ref atc_id=N831SA atc_id_color=0xffffffff atc_airline=SOAR atc_flight_number=92 ui_manufacturer=McDonnell-Douglas/Boeing ui_type="MD-83" ui_variation="SOAR Airlines" [fltsim.1] title=Boeing MD-83 AIRWAVE sim=MD_83 model= panel= sound= texture=1 kb_checklists=MD_83_check kb_reference=MD_83_ref atc_id=N714AW atc_id_color=0xffffffff atc_airline=AIRWAVE atc_flight_number=92 ui_manufacturer=McDonnell-Douglas/Boeing ui_type="MD-83" ui_variation="AIRWAVE AIRLINES" [fltsim.2] title=Boeing MD-83 PACIFICA sim=MD_83 model= panel= sound= texture=2 kb_checklists=MD_83_check kb_reference=MD_83_ref atc_id=N992PA atc_id_color=0xffffffff atc_airline=PACIFICA atc_flight_number=92 ui_manufacturer=McDonnell-Douglas/Boeing ui_type="MD-83" ui_variation="PACIFICA Airlines" [General] atc_type=Boeing atc_model=MD80 editable=1 performance=No. Of Engines: 2//Aircraft Type: Jet//Passenger Capacity (Max): 172//Passenger Capacity (Min): 137// Range (in Miles): 3,260//Cruising Speed (MPH): 576//Wingspan: 107//Height: 29//Takeoff Weight (in Lbs): 140,000//Cabin Type: pressurized//More than 1,100 MD-80s have been delivered since it entered service in 1980. It features commercial aviation's first digital flight guidance system and is available in five models: The MD-81, MD-82, MD-83, MD-88, MD-Super 80, and the smaller MD-87. [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 = 1.1 parasite_drag_scalar = 1.2 induced_drag_scalar = 1.4 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 = 1.7 aileron_trim_effectiveness = 1.2 rudder_trim_effectiveness = 1.0 [SMOKESYSTEM] smoke.0= 0.00, -125.00, -8.10, fx_747_jetsmoke14v6 smoke.1= 0.00, -125.00, 8.10, fx_747_jetsmoke14v6 [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 = .65 //Scalar for fuel flow efficiency min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser [TurbineEngineData] fuel_flow_gain = 0.012 //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, 5 , 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 2 , 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, 1800, 0, 1.08, 48.0, 1.00, 2.5, 0.9, 7.0, 5.0, 0, 180.0, 250.0 point.1 = 1, -83.10, -8.33, -9.4, 2800, 1, 1.85, 0.0, 1.50, 2.5, 0.9, 7.0, 7.0, 2, 180.0, 250.0 point.2 = 1, -83.10, 8.33, -9.4, 2800, 2, 1.85, 0.0, 1.50, 2.5, 0.9, 7.0, 7.0, 3, 180.0, 250.0 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 gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 15.0 //Flap angle that activates warning at idle flap_limit_power = 25.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.75 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [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 = 2 // degrees, KIAS flaps-position.2 = 5 // degrees, KIAS flaps-position.3 = 10 // degrees, KIAS flaps-position.4 = 15 // degrees, KIAS flaps-position.5 = 25 flaps-position.6 = 30 flaps-position.7 = 40 damaging-speed = 275 // KIAS blowout-speed = 295 // KIAS lift_scalar = 1.0 drag_scalar = .90 pitch_scalar= .95 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,0 [pitot_static] vertical_speed_time_constant = 5 //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 , light.5 = 3, -139.32, 0.00, 4.22, fx_navwhih , light.6 = 1, -136.20, 0.00, 20.0, fx_beaconh , light.7 = 1, -24.70, 0.00, 8.60, fx_beaconh , [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, 2860.0, 2.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -78.7, -12.1, -4.0, 2100.0, 2.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -78.7, 12.1, -4.0, 2100.0, 2.0 //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 = 2.5 //Degrees wing_twist = 0.0 //Degrees oswald_efficiency_factor= 0.9 //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 = -67.0 //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 = -2.0 //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) max_mach = 0.90 max_indicated_speed = 337 //Red line (KIAS) [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= 1200.0 autothrottle_available= 1 autothrottle_arming_required=1 autothrottle_max_rpm = 98 autothrottle_takeoff_ga= 1 pitch_takeoff_ga = 8; use_no_default_pitch=1 use_no_default_bank=1 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 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 = 1.0 default_pitch_mode=0 default_bank_mode=0 [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 [stall_warning] type=2 [direction_indicators] direction_indicator.0=3,0