[fltsim.0] title=HE 17 sim=HE-17 model= panel= sound= texture= kb_checklists= atc_id= ui_manufacturer=HE ui_type=HE 17 ui_variation=Default [General] atc_type= atc_model= editable=0 performance="Cruise speed\n185 mph 161 kts 298 km/hr\n\nEngines\nTwo Pratt & Whitney R-1830s\n\nMaximum range\n1,845 nm 2,125 mi 3,420 km\n\nService ceiling\n23,200 ft 7,071 m\n\nFuel capacity\n604 gal 2,286 L\n\nEmpty weight\n16,145 lb 7,323 kg\n\nMaximum gross weight\n26,200 lb 11,884 kg\n\nLength\n65.5 ft 20 m\n\nWingspan\n95 ft 29 m\n\nHeight\n17 ft 5.18 m\n\nMaximum seating\n21 to 28\n\nUseful load\n10,055 lb 4,560 kg" [WEIGHT_AND_BALANCE] max_gross_weight = 36200 // (pounds) empty_weight = 26145 // (pounds) reference_datum_position = 19.25, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -20.90, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations =50 //station_load.0 = "170.0, -5.4, -2.0, 0.0, Pilot" //Weight, Lat, Lon, Vert Position //station_load.1 = "170.0, -5.4, 2.0, 0.0, Co-Pilot" //Weight, Lat, Lon, Vert Position //station_load.2 = "680.0, -14.2, 0.0, 0.0, Passenger Row 1" //Weight, Lat, Lon, Vert Position //station_load.3 = "680.0, -17.4, 0.0, 0.0, Passenger Row 2" //Weight, Lat, Lon, Vert Position //station_load.4 = "680.0, -20.7, 0.0, 0.0, Passenger Row 3" //Weight, Lat, Lon, Vert Position //station_load.5 = "680.0, -23.9, 0.0, 0.0, Passenger Row 4" //Weight, Lat, Lon, Vert Position //station_load.6 = "510.0, -27.2, 0.0, 0.0, Passenger Row 5" //Weight, Lat, Lon, Vert Position //station_load.7 = "510.0, -30.4, 0.0, 0.0, Passenger Row 6" //Weight, Lat, Lon, Vert Position //station_load.8 = "340.0, -33.7, 0.0, 0.0, Passenger Row 7" //Weight, Lat, Lon, Vert Position //station_load.9 = "340.0, -36.9, 0.0, 0.0, Passenger Row 8" //Weight, Lat, Lon, Vert Position //station_load.10 = "500.0, -23.8, 0.0, 0.0, Forward Baggage" //Weight, Lat, Lon, Vert Position //station_load.11 = "100.0, -45.5, 0.0, 0.0, Rear Cargo" //Weight, Lat, Lon, Vert Position ;Moments of Inertia empty_weight_pitch_MOI = 69699.03 empty_weight_roll_MOI = 61179.10 empty_weight_yaw_MOI = 131797.97 empty_weight_coupled_MOI = 0.0 [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 = 7 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 11 // degrees flaps-position.2 = 23 // degrees flaps-position.3 = 34 // degrees flaps-position.4 = 45.0 // degrees damaging-speed = 140 // KIAS blowout-speed = 175 // KIAS lift_scalar = 1.0 drag_scalar = 1.5 pitch_scalar= 1.0 system_type = 1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -9.75, -10.1, -1.8 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -9.75, 9.1, -1.8 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.2 = -9.75, -9.1, -1.8 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.3 = -9.75, 10.1, -1.8 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 1.0 //Fuel flow scalar min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser master_ignition_switch = 1 //Master Ignition Switch [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 130.71 //Cubic inches per cylinder compression_ratio= 6.7 //Compression ratio number_of_cylinders=14 //Number of cylinders max_rated_rpm= 2700 //Max rated RPM max_rated_hp= 1200 //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 [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 11.53 //Propeller Diameter, (feet) propeller_blades= 3 //Number of propeller blades propeller_moi= 40.2 //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= 1.778 //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 //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=1, -46.64, 0.0, -4.74, 1200.0, 0, 0.60, 90.0, 0.200, 2.3, 0.995, 0.0, 0.0, 0.0, 0.0, 0.0 point.1=1, -7.18, -11.5, -7.65, 1600.0, 1, 1.35, 0.0, 0.704, 2.3, 0.986, 7.0, 9.0, 7.0, 166.0, 166.0 point.2=1, -7.18, 11.5, -7.65, 1600.0, 2, 1.35, 0.0, 0.704, 2.3, 0.986, 3.0, 5.0, 7.0, 166.0, 166.0 point.3=2, -27.00, -46.3, -0.1, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 point.4=2, -27.00, 46.3, -0.1, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0 point.5=2, -61.00, 0.0, 14.0, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0 point.6=2, 0.40, 0.0, -1.2, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4.0, 0.0, 0.0 static_pitch = 12.76 static_cg_height = 7.65 gear_system_type=1 //Hydraulic tailwheel_lock = 1 [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 = 0.3 //Brake scalar differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected [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 = -6.495, -1.512, 3.217 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //light.0 = 3, -27.20, -46.3, 0.65, fx_navredm , //light.1 = 3, -27.20, 46.3, 0.65, fx_navgrem , //light.2 = 3, -64.00, 0.00, 2.72, fx_navwhi , //light.3 = 1, -36.80, 0.00, 6.25, fx_beaconh , //light.4 = 4, -6.00, 0.00, 1.80, fx_vclight, light.5 = 4, -33.00, 0.00, 4.20, fx_vclighth, [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 [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 =200, 1000 aileron =200, 1000 rudder =200, 1000 [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 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=2,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks startup=fx_engstrt_jenny touchdown=fx_tchdwn_s, 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 25 max_generator_alternator_amps = 100 [fuel] LeftMain = -22.55, -6.7, -3.0, 202.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain= -22.55, 6.7, -3.0, 202.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center1 = -22.55, 0.0, -2.7, 200.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 2 electric_pump=1 [airplane_geometry] wing_area = 987.0 //Square feet wing_span = 95.0 //Feet wing_root_chord = 12.85 //Feet wing_dihedral = 5.0 //Degrees wing_incidence = 2.0 //Degrees wing_twist = -1.0 //Degrees oswald_efficiency_factor= 0.65 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 14.5 //Degrees, wing leading edge wing_pos_apex_lon = -13.00 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = -2.7 //Feet, vertical distance from reference point, positive going up htail_area = 95.8 //Square feet htail_span = 28.25 //Feet htail_pos_lon = -52.7 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = -52.7 //Feet, vertical distance from reference point, positive going up htail_incidence = -1.0 //Degrees htail_sweep = 27.0 //Degrees, horizontal tail leading edge vtail_area = 37.9 //Square feet vtail_span = 11.49 //Feet, tip to body vtail_sweep = 50.4 //Degrees, vertical tail leading edge vtail_pos_lon = -51.4 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 6.7 //Feet, vertical distance from reference point, positive going up elevator_area = 83.4 //Square feet aileron_area = 102.8 //Square feet rudder_area = 46.7 //Square feet elevator_up_limit = 30.0 //Degrees elevator_down_limit = 20.0 //Degrees aileron_up_limit = 27.0 //Degrees aileron_down_limit = 18.0 //Degrees rudder_limit = 30.0 //Degrees elevator_trim_limit = 12.0 //Degrees spoiler_limit = 0.0 //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 = 67.5 //Knots True (KTAS) full_flaps_stall_speed = 61.5 //Knots True (KTAS) cruise_speed = 95.0 //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 [forcefeedback] ground_bumps_magnitude1=2600 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.6 ground_bumps_magnitude2=1200 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.085 ground_bumps_slope2=0.65 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=3500000 ; in microseconds [stall_warning] type=1 [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second