[fltsim.0] title=Beechcraft King Air C90B N904HB sim=C90B model= panel= sound= texture=n904hb kb_checklists= atc_id=N904HB description=A highly successful design in production for 40 years. Power 2 PT6A-21 550 shp. ui_manufacturer=Beechcraft ui_type=King Air C90B ui_variation=Brown Turqoise White [fltsim.1] title=Beechcraft King Air C90B N493VG sim=C90B model= panel= sound= texture=n493vg kb_checklists= atc_id=N493VG description=A highly successful design in production for 40 years. Power 2 PT6A-21 550 shp. ui_manufacturer=Beechcraft ui_type=King Air C90B ui_variation=Gold Green Black [fltsim.2] title=Beechcraft King Air C90B N313DW sim=C90B model= panel= sound= texture=n313dw kb_checklists= atc_id=N313DW description=A highly successful design in production for 40 years. Power 2 PT6A-21 550 shp. ui_manufacturer=Beechcraft ui_type=King Air C90B ui_variation=Blue Gold White [fltsim.3] title=Beechcraft King Air C90B N126XJ sim=C90B model= panel= sound= texture=n126xj kb_checklists= atc_id=N126XJ description=A highly successful design in production for 40 years. Power 2 PT6A-21 550 shp. ui_manufacturer=Beechcraft ui_type=King Air C90B ui_variation=Jaguar Edition [General] atc_type=KingAir atc_model=BE9L editable=0 performance=Maximum speed 249 kts, Maximum Range 1155 nm [WEIGHT_AND_BALANCE] max_gross_weight=10100 // (pounds) empty_weight=6803 // (pounds) reference_datum_position=0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=200, 5.0, -2.0, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=200, 5.0, 2.0, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=0, -2.1, -2.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=0, -2.1, 2.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=0, -5.3, -2.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=0, -5.3, 2.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=30000 empty_weight_roll_MOI=18200 empty_weight_yaw_MOI=36500 empty_weight_coupled_MOI=0.0 [fuel] LeftMain=0.0, -14.5, -1.0, 140.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux=0.0, -6.0, -1.5, 52, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=0.0, 14.5, -1.0, 140.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux=0.0, 6.0, -1.5, 52, 0.0 //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=1 [airplane_geometry] wing_area=294 wing_span=50.25 wing_root_chord=3.50 wing_dihedral=6.0 wing_incidence=1.66 wing_twist=0 wing_pos_apex_lon=1.4 wing_pos_apex_vert=-1 oswald_efficiency_factor=0.725 wing_winglets_flag=0 wing_sweep=0.0 htail_area=68 htail_span=18.42 htail_pos_lon=-15.0 htail_pos_vert=1.0 htail_incidence=0.0 htail_sweep=20.0 vtail_area=52.3 vtail_span=7.4 vtail_sweep=40.0 vtail_pos_lon=-20.5 vtail_pos_vert=4.1 elevator_area=17.0 aileron_area=13.5 rudder_area=7.3 elevator_up_limit=20.0 elevator_down_limit=14.0 aileron_up_limit=25.0 aileron_down_limit=15.0 rudder_limit=25.0 elevator_trim_limit=18.8 spoiler_limit=90.0 spoilerons_available=0 aileron_to_spoileron_gain=0 min_ailerons_for_spoilerons=0 min_flaps_for_spoilerons=0 [Reference Speeds] flaps_up_stall_speed=96.0 full_flaps_stall_speed=76.8 cruise_speed=249.0 max_indicated_speed=259.937500 max_mach=0.500000 [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=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-8.3, -4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-8.3, 4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=0.95 //Scalar for fuel flow efficiency min_throttle_limit=-0.250000 [propeller] thrust_scalar=0.992 propeller_type=0 propeller_diameter=8.2 propeller_blades=4 propeller_moi=20 gear_reduction_ratio=13.60 beta_max=40 beta_min=15.2 minimum_on_ground_beta=4 prop_reverse_available=1 minimum_reverse_beta=-30 min_gov_rpm=25000 prop_tc=0.004 fixed_pitch_beta=0 low_speed_theory_limit=80 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=700 beta_feather=86.0 power_absorbed_cf=0.9 defeathering_accumulators_available=0 [TurbineEngineData] fuel_flow_gain=0.011 //Gain on fuel flow inlet_area=0.38 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=140 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar=1.0 //Scalar on Turboprop power maximum_torque=1315 //Maximum torque available (ft-lbs) [electrical] max_battery_voltage=24 generator_alternator_voltage=28 max_generator_alternator_amps=250 electric_always_available=0 flap_motor=0, 5, 17 gear_motor=2, 5, 17 autopilot=0, 5, 17 avionics_bus=2, 10, 17 avionics=1, 5, 17 pitot_heat=0, 2, 17 additional_system=0, 20, 17 marker_beacon=0, 2, 17 gear_warning=0, 2, 17 fuel_pump=0, 5, 17 starter1=0, 20, 17 starter2=0, 20, 17 light_nav=0, 5, 17 light_beacon=0, 5, 17 light_landing=0, 5, 17 light_taxi=0, 5, 17 light_strobe=0, 5, 17 light_panel=0, 5, 17 light_cabin = 0, 5 , 17 prop_sync=0, 15, 17 auto_feather=0, 15, 17 standby_vacuum=0, 15, 17 hydraulic_pump=0, 2, 17 fuel_transfer_pump=0, 5, 17 propeller_deice=0, 14, 17 light_recognition=0, 5, 17 light_wing=0, 5, 17 light_logo=0, 5, 17 //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, 10.75, 0.00, -4.65, 1181, 0, 0.596, 39.9, 0.296, 1.0, 3.0000, 4.8, 4.8, 0, 181.0, 204.0 point.1=1, -2.00, -8.58, -4.80, 1574, 1, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.5, 5.2, 2, 181.0, 204.0 point.2=1, -2.00, 8.58, -4.80, 1574, 2, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.8, 4.9, 3, 181.0, 204.0 point.3=2, -2.00, -24.85, 1.50, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -2.00, 24.85, 1.50, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -22.00, 0.00, 1.50, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 11.85, 0.00, 0.25, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch=-0.4 static_cg_height=4.2 gear_system_type=0 [Views] eyepoint=3.5, -1.20, 3.6 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees flaps-position.1=20 // degrees flaps-position.2=40 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS [Radios] Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 1 Adf.1=1 Adf.2=1 Transponder.1=1, 1 Marker.1=1 [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, 250 aileron=150, 250 rudder=150, 250 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=3,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -0.27, -24.85, 1.50, fx_navred , light.1=3, -0.27, 24.85, 1.50, fx_navgre , light.2=3, -22.57, 0.00, 2.70, fx_navwhi , light.3=2, -0.50, -25.00, 1.50, fx_strobe , light.4=2, -0.50, 25.00, 1.50, fx_strobe , light.5=1, -20.91, 0.00, 10.35, fx_beacon , light.6=1, -2.84, 0.00, -1.38, fx_beacon , light.7=4, 5.91, 0.00, 1.64, fx_vclight, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [autopilot] use_no_default_pitch=1 use_no_default_bank=1 autopilot_available=1 flight_director_available=1 default_vertical_speed=1000 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_max_rpm=0 autothrottle_takeoff_ga=0 max_throttle_rate=0.10 pitch_takeoff_ga=8 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000 max_pitch_velocity_hi_alt_breakpoint=28000 max_pitch=10 max_pitch_acceleration=1 max_pitch_velocity_lo_alt=2 max_bank=25 max_bank_acceleration=1.8 max_bank_velocity=3 max_throttle_rate=0.1 nav_proportional_control=9 nav_integrator_control=0.25 nav_derivative_control=0 nav_integrator_boundary=2.5 nav_derivative_boundary=0 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0 gs_integrator_boundary=0.7 gs_derivative_boundary=0 yaw_damper_gain=1.5 default_pitch_mode=0 default_bank_mode=0 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [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