[fltsim.0] title = AW Spitfire MK XIV RAAF sim=SpitfireMk14E model= panel= sound= texture= checklists=Spitfire_CHECK atc_id=NI visual_damage=1 description=Supermarine Spitfire FR. XIVe - 451st Squadron, Royal Australian Air Force, Germany, 1945 Photoreconniassance variant with Griffon engine and bubble canopy. ui_manufacturer=Supermarine ui_type=Spitfire XIV ui_variation=1. 451 Squadron, RAAF atc_airline=warbird editable=0 [fltsim.1] title = AW Spitfire MK XIV RAF sim=SpitfireMk14E model= panel= sound= texture=1 checklists=Spitfire_CHECK atc_id=MV349 visual_damage=1 description=Supermarine Spitfire FR. XIVe - 28th Squadron S.E.A.C., Malaya, Early 1945 ui_manufacturer=Supermarine ui_type=Spitfire XIV ui_variation=2. 28 Squadron RAF atc_airline=Air Force editable=0 [fltsim.2] title = AW Spitfire MK XIV RAF (GREY) sim=SpitfireMk14E model= panel= sound= texture=2 checklists=Spitfire_CHECK atc_id=MV320 visual_damage=1 description=Supermarine Spitfire FR. XIVe - 28th Squadron S.E.A.C., Kuala Lumpur, Malaya, 1945 ui_manufacturer=Supermarine ui_type=Spitfire XIV ui_variation=3. 28 Squadron RAF atc_airline=Air Force editable=0 [WEIGHT_AND_BALANCE] empty_weight = 7056 reference_datum_position=0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.135, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, -5.1, 0.0, 2.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 7791 empty_weight_roll_MOI = 5489 empty_weight_yaw_MOI = 12000 empty_weight_coupled_MOI=0.000000 CG_forward_limit=1.000 CG_aft_limit=1.0 [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 [piston_engine] power_scalar=1.0 cylinder_displacement=186.666667 compression_ratio=6.000000 number_of_cylinders=12 max_rated_rpm=2750.000000 max_rated_hp=1540.000000 fuel_metering_type=2 cooling_type=1 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=53.999999 min_design_mp=9.000000 critical_altitude=25400.000000 emergency_boost_type=3 emergency_boost_mp_offset=11.900000 emergency_boost_gain_offset=1.111739 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [propeller] thrust_scalar=1.0 rotation=-1 propeller_type=0 propeller_diameter=10.416700 propeller_blades=4 propeller_moi=35.005465 beta_max=65.000000 beta_min=15.000000 min_gov_rpm=412.500000 prop_tc=0.010000 gear_reduction_ratio=1.961000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=70.000000 beta_feather=88.500000 power_absorbed_cf=0.900000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=1.000000 minimum_reverse_beta=-14.000000 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [contact_points] //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) point.0=1.0,-18.25, 0.00, -2.36, 2165, 0, 0.54, 46.0, 0.46, 2.50,0.49, 3.0, 3.00, 0, 0, 135 point.1=1.0, 1.91,-4.00, -6.65, 2165, 1, 0.54, 0.0, 0.53, 2.50,0.87, 6.0, 6.00, 2, 0, 135 point.2=1.0, 1.91, 4.00, -6.65, 2165, 2, 0.54, 0.0, 0.53, 2.50,0.87, 7.0, 7.00, 3, 0, 135 point.3=2.0, 0.00,-18.4, 0.00, 1181, 0, 0.00, 0.0, 0.00, 0.00,0.00, 0.0, 0.00, 5 point.4=2.0, 0.00, 18.4, 0.00, 1181, 0, 0.00, 0.0, 0.00, 0.00,0.00, 0.0, 0.00, 6 point.5=2.0,-19.98, 0.0, 0.00, 1181, 0, 0.00, 0.0, 0.00, 0.00,0.00, 0.0, 0.00, 9 point.6=2.0, 9.32, 0.0, 0.00, 1181, 0, 0.00, 0.0, 0.00, 0.00,0.00, 0.0, 0.00, 4 static_pitch=12.722168 static_cg_height=5.4 [Views] eyepoint=-4.95,0.0,2.28 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.125 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=14 // degrees, KIAS flaps-position.2=28 // degrees, KIAS flaps-position.3=42 // degrees, KIAS flaps-position.4=55 // degrees, KIAS damaging-speed=175 // KIAS blowout-speed=265 // KIAS [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [SMOKESYSTEM] SMOKE.0=1.00, -4.00, -1.64, FX_HB_FS2002_ENG_SMOKE, // (feet) vertical, longitudinal, lateral, SMOKE.1=1.00, -4.00, 1.64, FX_HB_FS2002_ENG_SMOKE, SMOKE.2=0.20, -1.00, -18.50, FX_HB_CONTRAIL_s, SMOKE.3=0.20, -1.00, 18.50, FX_HB_CONTRAIL_s, [LIGHTS] light.0=4, -4.00, 0.00, 0.60, fx_vclight [General] performance=Weight: 7256 lbs\nPower: 1540 hp\n7.5g Corner speed: 242 mph\nMax speed @ SL: 363 mph\nMax speed: 446 mph @ 25400 ft\nClimb rate: 5040 ft\/min @ 141 mph\nFlight Model By: Jerry Beckwith\n8\/25\/02 05:23 PM\nFlight Model Workbook V2.80.53 [fuel] Center1=0.400000,0.000000,1.000000,48.000000,0.000000 Center2=0.400000,0.000000,-1.000000,36.000000,0.000000 LeftMain=0.000000,-6.000000,-1.000000,12.750000,0.000000 RightMain=0.000000,6.000000,-1.000000,12.750000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=242.000000 wing_span=36.833333 wing_root_chord=6.583333 wing_dihedral=4.998779 wing_incidence=1.999512 wing_twist=0.000000 oswald_efficiency_factor=0.979993 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=28.000000 htail_span=14.750000 htail_pos_lon=-18.000000 htail_pos_vert=0.000000 htail_incidence=0.999756 htail_sweep=0.000000 vtail_area=13.000000 vtail_span=4.110961 vtail_sweep=0.000000 vtail_pos_lon=-18.000000 vtail_pos_vert=5.500000 elevator_area=18.700000 aileron_area=22.600000 rudder_area=10.100000 elevator_up_limit=28.000000 elevator_down_limit=23.000000 aileron_up_limit=20.000000 aileron_down_limit=25.000000 rudder_limit=28.500000 elevator_trim_limit=15.000000 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [GeneralEngineData] engine_type=0 Engine.0=8.416667,0.000000,0.000000 fuel_flow_scalar=1.000000 [Reference Speeds] flaps_up_stall_speed=94.000000 full_flaps_stall_speed=75.200000 cruise_speed=286.382224 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0
