[fltsim.0] title=Found_Floats sim=Found_Floats model= panel= sound= texture= kb_checklists=Found kb_reference=Found atc_id=C-GDWS editable=0 ui_manufacturer=Found ui_type=Bush Hawk XP w/Floats ui_variation=C-GDWS description=The Bush Hawk-XP is a rugged, all-metal, high cantilever wing, single-engine airplane. Available with tail wheel landing gear or floats and designed for general utility purposes. atc_heavy=0 [General] atc_type=Found atc_model= performance=-Dimensions \nSpan : 36'0 ft \nLength : 26'6 ft \nHeight : 8'3 ft \n-Weight \nempty : 1,900 lb \nmax : 3,500 lb \n-Power Plant \n300hp LycomingIO-540-L1C5 \n-Performance \ncruise speed : 150kts \nceiling : 18.000ft\nrange : 880nm \n\nAircraft by: Steven Grant - April 2003 [WEIGHT_AND_BALANCE] max_gross_weight=3500 // (pounds) empty_weight=1960 // (pounds) reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0= 0.653, -0.849, 1.535, 200.00 //Pilot Weight(lbs), longitudinal, lateral, vertical positions(feet) station_load.1= 0.653, 0.849, 1.535, 000.00 //Front Passenger Weight(lbs), longitudinal, lateral, vertical positions(feet) station_load.2= -2.416, 0.849, 1.535, 000.00 //Rear Passenger1 Weight(lbs), longitudinal, lateral, vertical positions(feet) station_load.3= -2.416, 0.000, 1.535, 000.00 //Rear Passenger2 Weight(lbs), longitudinal, lateral, vertical positions(feet) station_load.3= -2.416, -0.849, 1.535, 000.00 //Rear Passenger3 Weight(lbs), longitudinal, lateral, vertical positions(feet) empty_weight_roll_MOI=1137.000000 empty_weight_pitch_MOI=1400.000000 empty_weight_yaw_MOI=2360.000000 empty_weight_coupled_MOI=0.000000 [flight_tuning] cruise_lift_scalar=0.4 parasite_drag_scalar=1.3 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=2.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [fuel] LeftMain=-0.250000,-2.100000,2.500000,50.000000,0.000000 RightMain=-0.250000,2.100000,2.500000,50.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=176.000000 wing_span=36.000000 wing_root_chord=4.916670 wing_dihedral=1.735840 wing_incidence=1.499634 wing_twist=2.00 oswald_efficiency_factor=0.719935 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=1.229000 wing_pos_apex_vert=0.000000 htail_area=39.000000 htail_span=11.666667 htail_pos_lon=-14.666667 htail_pos_vert=0.000000 htail_incidence=3.246460 htail_sweep=0.000000 vtail_area=18.000000 vtail_span=4.837355 vtail_sweep=0.000000 vtail_pos_lon=-12.583333 vtail_pos_vert=1.500000 elevator_area=16.610000 aileron_area=18.300000 rudder_area=6.650000 elevator_up_limit=29.50 elevator_down_limit=21.50 aileron_up_limit=18.00 aileron_down_limit=12.00 rudder_limit=30.00 elevator_trim_limit=6.00 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 //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] point.0=4, -9.33, -4.09, -3.30, 3500, 0, 0.5, 0.0, 0.50, 1.50, 0.78, 0.00, 0.00, 0.00 point.1=4, -9.33, 4.09, -3.30, 3500, 0, 0.5, 0.0, 0.50, 1.50, 0.78, 0.00, 0.00, 0.00 point.2=4, 4.00, -4.09, -3.80, 3500, 0, 0.5, 0.0, 0.50, 1.50, 0.78, 0.00, 0.00, 2.00 point.3=4, 4.00, 4.09, -3.80, 3500, 0, 0.5, 0.0, 0.50, 1.50, 0.78, 0.00, 0.00, 3.00 point.4=2, 0.00, 17.96, 4.12, 1800, 0, 0.0, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00 point.5=2, 0.00, -17.96, 4.12, 1800, 0, 0.0, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00 point.6=2, 1.50, -1.23, -1.07, 1800, 0, 0.0, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00 point.7=2, 1.50, 1.23, -1.07, 1800, 0, 0.0, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00 point.8=2, -14.17, 0.00, 0.93, 1800, 0, 0.0, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00 point.9=2, 5.65, 0.00, -0.15, 1800, 0, 0.0, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00 point.10=5,-12.00, -5.08, -4.60, 1600, 0, 0.0, 45.0, 0.00, 0.00, 1.00, 2.00, 2.20, 0.00 point.11=5,-12.00, 5.08, -4.60, 1600, 0, 0.0, 45.0, 0.00, 0.00, 1.00, 2.00, 2.20, 0.00 static_pitch= 1.20 //degrees (pitch when loaded on ground) static_cg_height=2.80 //feet, altitude of CG when at rest on the ground [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=0.00 // degrees flaps-position.1=8.00 // degrees flaps-position.2=15.00 // degrees flaps-position.3=22.00 // degrees flaps-position.4=32.00 // degrees damaging-speed=120 // KIAS blowout-speed=150 // KIAS lift_scalar=1.5 drag_scalar=1.2 pitch_scalar=1.0 system_type=0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.40, -18.10, 4.08, fx_navred light.1=3, 0.40, 18.10, 4.08, fx_navgre light.2=2, 0.38, -18.10, 4.08, fx_strobe light.3=2, 0.38, 18.10, 4.08, fx_strobe light.4=1,-14.08, 0.00, 7.93, fx_beacon light.5=4, 1.50, 0.00, 3.20, fx_vclight [SMOKESYSTEM] smoke.0=0.0, -6.0, -5.0, fx_FoundWater smoke.1=0.0, -6.0, 5.0, fx_FoundWater [GeneralEngineData] engine_type=0 Engine.0=6.000000,0.000000,0.000000 fuel_flow_scalar=1.000000 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=90.0 //Cubic inches per cylinder compression_ratio=8.7 //Compression ratio number_of_cylinders=6 //Number of cylinders max_rated_rpm=2700 //Max rated RPM max_rated_hp=300 //Max rated HP fuel_metering_type=0 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque=0.3 //Starter torque factor turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp=32.00 //Max design manifold pressure, (inHg) min_design_mp=8.00 //Min design manifold pressure, (inHg) critical_altitude=0 //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 [propeller] thrust_scalar=1.5 //Propeller thrust scalar propeller_type=0 propeller_diameter=7.00 propeller_blades=3 propeller_moi=5.700000 beta_max=31.100000 beta_min=11.200000 min_gov_rpm=1400.000000 prop_tc=0.100000 gear_reduction_ratio=1.00 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=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Reference Speeds] flaps_up_stall_speed=57.000000 full_flaps_stall_speed=52.000000 cruise_speed=150.000000 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.12,0.11 ;Percent per second [exits] number_of_exits=2 exit_rate.0=0.5 ;Percent per second exit_rate.1=0.5 ;Percent per second [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint= 0.37, -0.86, 3.20 //(feet) longitudinal, lateral, vertical distance from reference datum [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0
