[fltsim.0] title=XB-19 sim=XB-19 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=8471 ui_manufacturer=Douglas ui_type="XB-19" ui_variation="USAAC" prop_anim_ratio=-1.8 description=The Douglas XB-19' with it's 212 foot wingspan was the largest airplane built until the advent of the B-36. atc_id_color=0x00000000 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 [General] atc_type=Douglas atc_model=XB-19 editable=0 performance="Cruise speed\n135 mph\n\nEngines\nFour Wright R-3350-5's\n\nMaximum range\n7710 miles\n\nService ceiling\n23,200 ft \n\nFuel capacity\n11194 gal \n\nEmpty weight\n86,000 lbs.\n\nMaximum gross weight \n 162,000 lbs.\n\nLength\n132 ft 4 inches\n\nWingspan\n212 ft.\n\nHeight\n42 ft.\n\nUseful load\n584000lbs\n\n GMAX mdl by A.F.Scrub June 2010 Category = airplane [CameraDefinition.0] Title = "Tail" Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c} Description = Looking forward from behind the aircraft Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.0 ShowWeather = Yes InitialXyz = 0, 3.0, -16.8 InitialPbh = 10, 0, 0 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.1] Title = "Right Wing" Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59} Description = View from the right wing tip looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.0 ShowWeather = Yes InitialXyz = 38.0, 2.0, -5.0 InitialPbh = 8, 0, 270 XyzAdjust = TRUE Category=Aircraft MomentumEffect = FALSE ClipMode=Minimum [CameraDefinition.2] Title = "Left Wing" Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de} Description = View from the left wing tip looking at the cockpit Origin = Center SnapPbhAdjust = None SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.0 ShowWeather = Yes InitialXyz = -38.0, 2.0, -5.0 InitialPbh = 8, 0, 90 XyzAdjust = TRUE Category=Aircraft MomentumEffect = No ClipMode=Minimum [CameraDefinition.001] Title = "Flight Deck" Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = Swivel PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.8 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.75, 0.0, -2 InitialPbh=8, 0, 180 ClipMode=Minimum [weight_and_balance] // ACM V2.5 max_gross_weight = 162000 empty_weight = 86000 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 1843201 empty_weight_roll_MOI = 2019024 empty_weight_yaw_MOI = 3252274 empty_weight_coupled_MOI = 0 max_number_of_stations = 2 station_load.0 = 170, 33.57, -2.94, 0 station_load.1 = 170, 32.94, 2.00, 0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -11.436, -103.411, 3.865, fx_navredm , light.1 = 3, -11.036, 103.411, 3.865, fx_navgrem , light.2 = 3, -82.82, -0.5, -0.831, fx_navwhi , light.3 = 1, -10.00, 0.00, 5.19, fx_beaconh , light.4 = 4, 31.95, -2.0, 1.5, fx_vclight, light.5 = 4, 31.95, 2.0, 1.5, fx_vclight, [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1.0 min_throttle_limit = 0.05 master_ignition_switch = 1 engine.0 = 14.76, -33.29, -1.48, engine.1 = 19.17, -16.02, -2.82, engine.2 = 19.17, 16.02, -2.82, engine.3 = 14.76, 33.29, -1.48, [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 startup = fx_engstrt_jenny windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 number_of_tank_selectors = 2 electric_pump = 1 Center1 = 0, 0, 0, 1500, 0 LeftMain = 0, 0, 0, 1500, 0 RightMain = 0, 0, 0, 2000, 0 //0 Class //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 [contact_points] static_pitch = 1 static_cg_height = 14.5 tailwheel_lock = 1 gear_system_type = 1 max_number_of_points = 7 point.0 = 1, 32.8548, 0, -15.0621, 1200, 0, 2.5, 22, 0.2, 1.25, 0.48, 8, 8, 0, 0, 0 point.1 = 1, -5.0813, -18.0473, -15.5217, 1600, 1, 4, 0, 0.704, 1.25, 0.56, 6, 6, 7, 166, 166 point.2 = 1, -4.7477, 18.048, -15.5359, 1600, 2, 4, 0, 0.704, 1.25, 0.56, 5, 5, 7, 166, 166 point.3 = 2, -27, -104.4368, 2.4151, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -27, 103.8082, 2.4149, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -84.2267, 0, -2.8, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 43.3094, 0, -6.1524, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 [keyboard_response] elevator = 200, 1000 aileron = 200, 1000 rudder = 200, 1000 [forcefeedback] ground_bumps_magnitude1 = 2600 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5.0 ground_bumps_slope1 = 0.6 ground_bumps_magnitude2 = 1200 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.085 ground_bumps_slope2 = 0.65 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 3500000 [airplane_geometry] wing_area = 4285 wing_span = 212.0 wing_root_chord = 32.33 wing_dihedral = 5 wing_incidence = 2.0 wing_twist = -1.0 oswald_efficiency_factor = 0.80 wing_winglets_flag = 0 wing_sweep = 13 wing_pos_apex_lon = 13.06 wing_pos_apex_vert = -2.70 htail_area = 206 htail_span = 62.18 htail_pos_lon = -49.24 htail_pos_vert = -52.68 htail_incidence = -1.0 htail_sweep = 13 vtail_area = 85 vtail_span = 24.68 vtail_sweep = 25 vtail_pos_lon = -61.45 vtail_pos_vert = 5.12 elevator_area = 83.4 aileron_area = 102.8 rudder_area = 46.7 elevator_up_limit = 30.0 elevator_down_limit = 30.0 aileron_up_limit = 25.0 aileron_down_limit = 25.0 rudder_limit = 30.0 elevator_trim_limit = 12.0 spoiler_limit = 45 aileron_to_spoileron_gain = 0 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 0 auto_spoiler_available=0 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-1.500000 negative_g_limit_flaps_down=-1.500000 spoiler_extension_time=0.000000 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 25 max_generator_alternator_amps = 100 engine_generator_map = 1,1,1,1 electric_always_available = 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 p_factor_on_yaw = 0.5 torque_on_roll = 1.0 gyro_precession_on_yaw = 1.0 gyro_precession_on_pitch = 1.0 [flaps.0] //Trailing Edge Flaps 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 = 11 // degrees flaps-position.2 = 23 // degrees flaps-position.3 = 34 // degrees flaps-position.4 = 40.0 // degrees damaging-speed = 140 // KIAS blowout-speed = 175 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [piston_engine] power_scalar=1.2 //Piston power scalar cylinder_displacement=186.1 //Cubic inches per cylinder compression_ratio=6.7 //Compression ratio number_of_cylinders=18 //Number of cylinders max_rated_rpm=2800 //Max rated RPM max_rated_hp=3350 //Max rated HP fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque=0.3 //Starter torque factor turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp=47 //Max design manifold pressure, (inHg) min_design_mp=10 //Min design manifold pressure, (inHg) critical_altitude=7000 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction magneto_order_left_right_both = 1 //sets the order of the magneto switch direction [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=17.0 //Propeller Diameter, (feet) propeller_blades=3 //Number of propeller blades propeller_moi=60.2 //Propeller moment of inertia beta_max=30.0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=18.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=1400 //Miminum governed RPM prop_tc=0.1 //Prop time-constant gear_reduction_ratio=1.9 //Propeller gear reduction ratio fixed_pitch_beta=0.0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80.0 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=700.0 //Minimum RPM for prop feathering beta_feather=89.5 //Feathering pitch angle (degrees) power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller in feather defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=0.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=0.0 //Minimum pitch angle in reverse, (degrees) feathering_switches=1 //Switches which invoke feathering [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 0.0 //Flap angle that activates warning at idle flap_limit_power = 16.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.8 //Brake scalar differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected auto_brakes = 0 [hydraulic_system] normal_pressure = 732.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=31.7, -2.45, 3.6 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Adf.2 = 1 Transponder.1=0 Marker.1=1 [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=1,0 direction_indicator.1=2,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 attitude_indicator.1 = 2 [altimeters] altimeter.0=1 altimeter.1=1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=2,0 [vacuum_system] max_pressure=5.0 //PSI vacuum_type=1 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi engine_map=1,1 [pneumatic_system] max_pressure=0.000000 [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available [Reference Speeds] flaps_up_stall_speed=67.5 //Knots True (KTAS) full_flaps_stall_speed=61.5 //Knots True (KTAS) cruise_speed=135.0 //Knots True (KTAS) max_indicated_speed = 224 //Red line (KIAS) [autopilot] autopilot_available=1 flight_director_available=0 pitch_takeoff_ga=0.0 default_vertical_speed=700.000000 autothrottle_available=0 direction_indicator=1 attitude_indicator =1 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 = 0.0 default_bank_mode=2 //Default to Heading Hold [stall_warning] type=1 stick_shaker=0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [deice_system] structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots [Spoilers.0] type= 1 span-outboard= 0.5 extending-time= 3 spoilers-position.0= 0.0, 0.0 //spoilers-position.1= 70, 0.0 spoilers-position.1= 25, 0.0 [TailHook] tailhook_length=4 ;(feet) tailhook_position = -23.6, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust = 1.0