[fltsim.0] title=Bronco Air MD-90-30 sim=MD90 model= panel= sound= texture=BRA checklists= ui_manufacturer=McDonnell Douglas ui_type=MD-90-30 ui_variation=Bronco Air description=McDonnel Douglas MD90-30 [fltsim.1] title=McDonnell Douglas MD90 Delta 3 sim=MD90 model= panel= sound= texture=delta3 checklists= atc_airline=Delta atc_id=N9070A atc_flight_number=6247 atc_heavy=0 ui_manufacturer=McDonnell Douglas ui_type=MD-90-30 ui_variation=Delta 3 description=McDonnell Douglas MD-90-30 [General] atc_type=MCDONNELDOUGLAS atc_model=MD80 performance=Engines: V2525 @ 25,000 lb thrust \nLength 152 ft 6 in (46.5 m)\nWing Span: 107 ft 8 in (32.87 m)\nHeight: 30 ft 6 in (9.4 m)\nMike's MD80 FDE modded out to 90. I make no accuracy guarantees. [GROUND_REACTION] MAX_STEERING_ANGLE=70 main_gear_static_compression=0.3 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.25 // (feet), The distance the center gear strut is compressed when at rest on the ground main_gear_damping_ratio=1.0 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=1.0 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [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 max_number_of_stations=60 station_load.0=200,60.00,-1.90,4.00 station_load.1=190,60.00, 1.90,4.00 station_load.2=5216,14.50,-17.30,-4.10 station_load.3=5216,14.50, 17.30,-4.10 station_load.4=600,55.50,-2.50,3.80 station_load.5=600,55.50, 2.50,3.80 station_load.6=600,52.16,-2.50,3.80 station_load.7=340,48.82,-2.50,4.00 station_load.8=170,48.82,2.50,4.00 station_load.9=170,45.48,-2.50,4.00 station_load.10=170,45.48,2.50,4.00 station_load.11=170,42.14,-2.50,4.00 station_load.12=340,42.14,2.50,4.00 station_load.13=340,38.80,-2.50,4.00 station_load.14=510,38.80,2.50,4.00 station_load.15=170,35.46,-2.50,4.00 station_load.16=170,35.46,2.50,4.00 station_load.17=340,32.12,-2.50,4.00 station_load.18=510,28.78,-2.50,4.00 station_load.19=170,28.78,2.50,4.00 station_load.20=340,25.44,2.50,4.00 station_load.21=510,22.10,-2.50,4.00 station_load.22=340,22.10,2.50,4.00 station_load.23=170,18.76,-2.50,4.00 station_load.24=170,18.76,2.50,4.00 station_load.25=340,15.42,2.50,4.00 station_load.26=510,12.08,-2.50,4.00 station_load.27=170,12.08,2.50,4.00 station_load.28=170,8.74,-2.50,4.00 station_load.29=170,8.74,2.50,4.00 station_load.30=340,5.40,-2.50,4.00 station_load.31=510,5.40,2.50,4.00 station_load.32=510,2.06,-2.50,4.00 station_load.33=170,2.06,2.50,4.00 station_load.34=170,-1.28,-2.50,4.00 station_load.35=340,-1.28,2.50,4.00 station_load.36=170,-4.62,2.50,4.00 station_load.37=510,-7.96,-2.50,4.00 station_load.38=510,-7.96,2.50,4.00 station_load.39=170,-11.30,-2.50,4.00 station_load.40=170,-11.30,2.50,4.00 station_load.41=340,-14.64,-2.50,4.00 station_load.42=170,-17.98,2.50,4.00 station_load.43=510,-21.32,-2.50,4.00 station_load.44=170,-21.32,2.50,4.00 station_load.45=340,-24.66,2.50,4.00 station_load.46=340,-28.00,-2.50,4.00 station_load.47=340,-28.00,2.50,4.00 station_load.48=510,-31.34,-2.50,4.00 station_load.49=170,-31.34,2.50,4.00 station_load.50=170,-34.68,-2.50,4.00 station_load.51=340,-38.02,2.50,4.00 station_load.52=340,-41.36,-2.50,4.00 station_load.53=510,-41.36,2.50,4.00 station_load.54=170,-44.70,-2.50,4.00 station_load.55=170,-44.70,2.50,4.00 station_load.56=170,-48.04,2.50,4.00 station_load.57=1200,-51.50,0.00,3.80 station_load.58=4800,35.00,0.00,-1.00 station_load.59=5600,-25.00,0.00,-1.00 empty_weight_CG_position=0.000000,0.000000,0.000000 empty_weight=88958.000000 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=-0.249939 [SMOKESYSTEM] smoke.0= 1, -19.00, 54.15, fx_contrail_320 smoke.1= 1, -19.00, -54.15, fx_contrail_320 [TurbineEngineData] fuel_flow_gain= 0.0035 inlet_area= 25.000 rated_N2_rpm= 29920.000 static_thrust= 25000.000 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 //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) max_indicated_speed=341.000000 max_mach=0.839990 //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, -7.800, 1574.803, 0.000, 1.504, 75.000, 0.539, 2.500, 0.483, 6.500, 6.500, 0.000, 250.0, 280.0 point.1=1.000, -3.850, 9.500, -7.900, 1574.803, 1.000, 1.504, 0.000, 0.293, 2.500, 0.655, 6.900, 6.900, 2.000, 250.0, 280.0 point.2=1.000, -3.850, -9.500, -7.900, 1574.803, 2.000, 1.504, 0.000, 0.293, 2.500, 0.655, 7.100, 7.100, 3.000, 250.0, 280.0 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 [TailHook] tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=0.7 [Views] eyepoint=70.0, -1.8, 5.1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=1, -19.10, 53.80, 2.00, fx_navgrem , light.1=1, -19.10, -53.80, 2.00, fx_navredm , light.2=3, -20.00, 53.80, 2.00, fx_strobeh , light.3=3, -20.00, -53.80, 2.00, fx_strobeh , light.4=2, -23.00, 53.80, 2.00, fx_strobeh , light.5=2, -23.00, -53.80, 2.00, fx_strobeh , light.6=1, -23.00, 53.01, 2.00, fx_navwhih, light.7=1, -23.00, -53.40, 2.00, fx_navwhih, light.8=3, 24.8, 5.8, 2.1, fx_navwhih, light.9=3, 24.8, -5.8, 2.1, fx_navwhih, light.10=3, -27.9, 5.8, 2.3, fx_navwhih, light.11=3, -27.9, -5.8, 2.3, fx_navwhih, light.12=3, 39.8, 5.3, -0.8, fx_navwhih, light.13=3, 39.8, -5.3, -0.8, fx_navwhih, light.14=1, -1.75, 0.00, -4.20, fx_beaconb , light.15=1, -0.90, 0.00, 8.60, fx_beaconh , [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, 3058.000, 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