[fltsim.0] title=McDonnell Douglas MD83 Viasa sim=Super83 model=cone panel= sound= texture=via checklists= ui_manufacturer=McDonnell Douglas ui_type=MD83 ui_variation=Viasa description=Model sga By Erick Cantu, Repaint By Yemel VeneHacker Yarbouh atc_airline=Viasa atc_id=N005A [General] atc_type=MCDONNELDOUGLAS atc_model=MD80 performance=Engines: JT8D-217 @ 20,850lbs each\nMTOW = 147,000 lbs\nMLW = 128,000 lbs (55% fuel)\nZFW = 107,870 lbs\nVmo\/Mmo = 340KIAS\/M0.84\nRange = 2990nm\nCruise = .76 - .80 mach\nMax Alt = 37,000 ft\n(speed book enclosed)\n\n [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=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.200 aileron_effectiveness=1.100 rudder_effectiveness=1.100 elevator_trim_effectiveness=1.200 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [jet_engine] thrust_scalar=1.100 [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=107870.000000 empty_weight_roll_MOI=3300000.000000 empty_weight_pitch_MOI=3371337.000000 empty_weight_yaw_MOI=3766083.000000 empty_weight_coupled_MOI=1300.000000 max_gross_weight=161805.000000 [GeneralEngineData] engine_type= 1 Engine.0= -36.667, -9.400, 2.833 Engine.1= -36.667, 9.400, 2.833 fuel_flow_scalar= 1.000 min_throttle_limit=-0.409912 [SMOKESYSTEM] smoke.0=2.833, -45.000, -9.400, SMOKE_JT8D smoke.1=2.833, -45.000, 9.400, SMOKE_JT8D [TurbineEngineData] fuel_flow_gain= 0.0032 inlet_area= 25.000 rated_N2_rpm= 29920.000 static_thrust= 20000.000 afterburner_available= 0 reverser_available= 1 [airplane_geometry] wing_area= 1315.000 wing_span= 107.000 wing_root_chord= 12.250 wing_dihedral= 2.999 wing_incidence= 0.000 wing_twist= -0.302 oswald_efficiency_factor= 0.887 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 381.000 htail_span= 40.167 htail_pos_lon= -60.50 htail_pos_vert= 19.55 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 224.000 vtail_span= 17.065 vtail_sweep= 0.000 vtail_pos_lon= -57.50 vtail_pos_vert= 10.55 elevator_area= 95.250 aileron_area= 52.600 rudder_area= 38.080 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.996 spoiler_limit= 59.989 spoilerons_available= 1 aileron_to_spoileron_gain= 3.000 min_ailerons_for_spoilerons= 9.969 min_flaps_for_spoilerons= 0.000 [Reference Speeds] flaps_up_stall_speed= 145.000 full_flaps_stall_speed= 116.000 cruise_speed= 428.885 max_indicated_speed=341.000000 max_mach=0.839990 //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=1.000, 73.000, 0.000, -7.200, 1574.80, 0.00, 2.20, 70.08, 0.29, 2.50, 0.87, 5.00, 5.00, 0.00, 0.00, 0.00 point.1=1.000, -3.850, 9.500, -8.100, 1574.80, 1.00, 2.20, 0.00, 0.29, 2.50, 0.87, 5.00, 5.00, 2.00, 0.00, 0.00 point.2=1.000, -3.850, -9.500, -8.100, 1574.80, 2.00, 2.20, 0.00, 0.29, 2.50, 0.87, 5.00, 5.00, 2.00, 0.00, 0.00 point.3=2.000, -18.600, -54.150, 2.050, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4=2.000, -18.600, 54.150, 2.050, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5=2.000, 81.800, 0.000, -0.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6=2.000, -68.500, 0.000, 19.550, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 0.000 static_cg_height= 7.800 gear_system_type=0 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 2 , 0 gear_motor=0, 2 , 0 autopilot=0, 2 , 0 avionics_bus=0, 2 , 0 avionics=0, 2 , 0 pitot_heat=0, 2 , 0 additional_system=0, 2 , 0 marker_beacon=0, 2 , 0 gear_warning=0, 2 , 0 fuel_pump=0, 2 , 0 starter1=0, 2 , 0 starter2=0, 2 , 0 starter3=0, 2 , 0 starter4=0, 2 , 0 light_nav=0, 2 , 0 light_beacon=0, 2 , 0 light_landing=0, 2 , 0 light_taxi=0, 2 , 0 light_strobe=0, 2 , 0 light_panel=0, 2 , 0 prop_sync=0, 2 , 0 auto_feather=0, 2 , 0 auto_brakes=0, 2 , 0 standby_vacuum=0, 2 , 0 hydralic pump=0, 2 , 0 fuel_transfer_pump=0, 2 , 0 propeller_deice=0, 2 , 0 propeller_deice=0, 2 , 0 light rocognition=0, 2 , 0 light_wing=0, 2 , 0 light_logo=0, 2 , 0 [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [TailHook] //landing lights (normally shift+T) tailhook_length= 4 tailhook_position= 0.0, 0.0, 0.0 cable_force_adjust= 0.5 [folding_wings] //Airstairs (normally shift+F) wing_fold_system_type= 4 fold_rates= 0.110,0.110 [Views] eyepoint=70.0, -1.8, 5.1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -14.00, 53.20, 2.40, fx_navgre , //right wing nav light.1=3, -14.00, -53.20, 2.40, fx_navred , //left wing nav light.2=2, -14.80, 53.95, 2.40, fx_strobe , //right wing strobe light.3=2, -14.80, -53.95, 2.40, fx_strobe , //left wing strobe light.4=1, -1.55, 0.00, -4.05, fx_beaconb , //lower beacon/strobe light.5=1, -0.90, 0.00, 8.30, fx_beacon , //upper beacon/strobe light.6=5, -21.50, 5.42, 1.35, fx_navwhi , //right engine inspection light light.7=5, -21.50, -5.42, 1.35, fx_navwhi , //left engine inspection light light.8=5, 40.10, 4.70, -.80, fx_navwhi , //right landing light light.9=5, 40.10, -4.70, -.80, fx_navwhi , //left landing light light.10=3, -18.10, 54.10, 2.40, fx_navwhi , //right wing id light light.11=3, -18.10,-54.10, 2.40, fx_navwhi , //left wing id light [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [direction_indicators] direction_indicator.0=3,0 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center1 = 0.000, 0.000, 0.000, 2728.000, 0.000 LeftMain= -1.000, -25.000, 0.000, 1391.000, 0.000 RightMain= -1.000, 25.000, 0.000, 1391.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1200.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=99.000000 pitch_takeoff_ga=8.000000 use_no_default_pitch=1 use_no_default_bank=1 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 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 20.000 system_type= 1 damaging-speed= 280.000 blowout-speed= 320.000 lift_scalar= 1.200 drag_scalar= 1.100 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 4.875, 0.000 flaps-position.2= 9.750, 0.000 flaps-position.3= 14.625, 0.000 flaps-position.4= 19.500, 0.000 flaps-position.5= 24.375, 0.000 flaps-position.6= 29.250, 0.000 flaps-position.7= 34.125, 0.000 flaps-position.8= 39.000, 0.000 [Flaps.1] type= 2 span-outboard= 0.000 extending-time= 2.000 system_type= 1 damaging-speed= 280.000 blowout-speed= 320.000 lift_scalar= 1.000 drag_scalar= 1.100 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 [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