[fltsim.0] title=Visage Turbo Prop sim=Pilatus6SeaterPrototypeVisage95 model= panel= sound= texture= atc_id=N773LH ui_manufacturer=Lionheart Aerospace ui_type=Visage Turbo Prop ui_variation=White kb_checklists= description=This is the Pilatus Visage 6 passenger turbo prop concept plane created by William Ortis of Lionheart Creations Ltd. The is a project to show conceptual possibilities in the use of modern day composite technologies and newer aerodynamic research developments by way of wing foil profiles, interior arangements, etc. This design was originally done in 2000. [General] atc_type=Pilatus atc_model= editable=1 ui_manufacturer=Pilatus ui_type=Visage 6 Seater ui_variation=White performance=Cruise Speed\t\n315 kts 363 mph 583 km\/h\n\nEngine\t\nPratt & Whitney PT6A-60A 1,050 shp\n\nMaximum Range\t\n1,765 nm 2,031 m\t 3,269 km\n\nService Ceiling\t\n35,000 ft 10,668 m\n\nFuel Capacity\t\n539 U.S. gal 2,040 L\n\nMaximum Takeoff Weight \n5,000 lb\t 6,818 kg\n\nLength\t\n46.7 ft\t 14.23 m\n\nWingspan\t\n32.9 ft\t 17.65 m\n\nHeight\t\n14.3 ft\t 4.36 m\n\nSeating\t\nUp to 5\n\nUseful Load\t\n5,810 lb\t 2,635 kg [WEIGHT_AND_BALANCE] max_gross_weight = 4250 // (pounds) empty_weight = 2250 // (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 = 1.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 170, 5.0, -2.0, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 170, 5.0, 2.0, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = 170, -2.1, -2.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = 170, -2.1, 2.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight= 2560.000 empty_weight_roll_MOI= 10400.000 empty_weight_pitch_MOI= 10300.000 empty_weight_yaw_MOI= 17300.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 4500.000 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar =0.3 induced_drag_scalar = 1.0 elevator_effectiveness = 1.4 aileron_effectiveness = 1.4 rudder_effectiveness = 1.4 pitch_stability = 1.4 roll_stability = 1.4 yaw_stability = 1.4 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.2 [GeneralEngineData] engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 2.1, 0.0, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 0.4 //Scalar for fuel flow efficiency min_throttle_limit=-0.250000 [propeller] thrust_scalar = 0.60 //Propeller thrust scalar propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter = 8.8 //Propeller Diameter, (feet) propellor_anim_ration = -1.75 rotation = 1,1 propeller_blades = 4 //Number of propeller blades propeller_moi = 24 //Propeller moment of inertia beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min = 15.2 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm = 25520 //Miminum governed RPM prop_tc = 0.004 //Prop time-constant gear_reduction_ratio = 17.6 //Propeller gear reduction ratio fixed_pitch_beta = 0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit = 80 //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= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather = 700 //Minimum RPM for prop feathering beta_feather = 79.3 //Feathering pitch angle (degrees) power_absorbed_cf = 0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta = 1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta = -14.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain = 0.035 //Gain on fuel flow inlet_area = 0.0 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust =15 //Lbs, max rated static thrust at Sea Level [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [turboprop_engine] power_scalar = 1.40 //Scalar on Turboprop power maximum_torque = 4200 //Maximum torque available (ft-lbs) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor = 0, 5 , 17.0 gear_motor = 0, 5 , 17.0 autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 20, 17.0 marker_beacon = 1, 2 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 17.0 starter1 = 0, 20, 17.0 light_nav = 0, 5 , 17.0 light_beacon = 0, 5 , 17.0 light_landing = 0, 5 , 17.0 light_taxi = 0, 5 , 17.0 light_strobe = 0, 5 , 17.0 light_panel = 0, 5 , 17.0 //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, 7.550, 0.000, -4.960, 1181.102, 0.000, 0.522, 40.000, 0.150, 2.500, 0.500, 7.000, 7.000, 0.000, 0.000, 0.000 point.1= 1, -1.417, -4.500, -5.350, 1574.803, 1.000, 0.522, 0.000, 0.260, 2.500, 0.841, 9.000, 9.000, 2.000, 0.000, 0.000 point.2= 1, -1.417, 4.500, -5.350, 1574.803, 2.000, 0.522, 0.000, 0.260, 2.500, 0.841, 9.000, 9.000, 3.000, 0.000, 0.000 point.3 = 2, 2.512, -20.672, 0.398, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.4 = 2, 2.768, 20.552, 0.343, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.5 = 2, -25.400, -0.032, 1.130, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.6 = -0.27, -4.60, -5.24, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.7 = -0.24, 4.76, -5.27, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.8 = 12.04, -0.15, -4.81, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.9 = -0.27, -4.60, -5.24, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.10 = -0.24, 4.76, -5.27, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.11 = 12.11, -0.15, -4.98, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 static_pitch = -1.1804 //degrees (pitch when loaded on ground) static_cg_height=5.110 //feet, altitude of CG when at rest on the ground gear_system_type=0 [Views] eyepoint= 3.19, -0.96, 1.69 //(feet) longitudinal, lateral, vertical distance from reference datum [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 = 324 // KIAS blowout-speed = 348 // KIAS [GEAR_DOWN] filename=kmgeardn [GEAR_UP] filename=kmgearup [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 Transponder.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, 5=landing light.0 = 3, 2.350, -21.225, .802, fx_navred , light.1 = 3, 2.700, 21.225, .802, fx_navgre , light.2 = 2, 2.450, -21.225, .802, fx_strobe , light.3 = 2, 2.800, 21.225, .802, fx_strobe , light.4 = 2, -30.200, 0.00, 8.70, fx_beacon , light.5 = 2, 0.375, 0.00, -1.602, fx_beacon , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain = 0.0, -14.5, -1.0, 40.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = 0.0, 14.5, -1.0, 40.0, 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 wing_fold =1 electric_pump=0 [airplane_geometry] wing_area = 310.0 //Square feet wing_span = 57.2 //Feet wing_root_chord = 5.4 //Feet wing_dihedral = 6.0 //Degrees wing_incidence = 1.0 //Degrees wing_twist = -1.5 //Degrees oswald_efficiency_factor= 0.7 //Measure of lift effeciency of wing wing_winglets_flag = 1 //Are winglets available? wing_sweep = 1.0 //Degrees, wing leading edge wing_pos_apex_lon = 2.1 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_area = 67.0 //Square feet htail_span = 17.2 //Feet htail_pos_lon = -22.6 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_incidence = 0.5 //Degrees htail_sweep = 20.0 //Degrees, horizontal tail leading edge vtail_area = 42.0 //Square feet vtail_span = 7.4 //Feet, tip to body vtail_sweep = 40.0 //Degrees, vertical tail leading edge vtail_pos_lon = -20.5 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 4.1 //Feet, vertical distance from reference point, positive going up elevator_area = 17.0 //Square feet aileron_area = 13.5 //Square feet rudder_area = 7.3 //Square feet elevator_up_limit = 17.0 //Degrees elevator_down_limit = 15.5 //Degrees aileron_up_limit = 18.0 //Degrees aileron_down_limit = 18.0 //Degrees rudder_limit = 30.0 //Degrees elevator_trim_limit = 15.0 //Degrees spoiler_limit = 60.0 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 0 //Aileron to spoileron gain min_ailerons_for_spoilerons = 0 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed = 96.0 //Knots True (KTAS) full_flaps_stall_speed = 76.8 //Knots True (KTAS) cruise_speed = 315.0 //Knots True (KTAS) max_indicated_speed=259.000000 max_mach=0.579980 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1800.0 autothrottle_available= 0 pitch_takeoff_ga=8.000000 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 [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=1.000000 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=1,0,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0