[fltsim.0] title=Bald Eagle sim=Bald Eagle model= panel= sound= texture= kb_checklists= ui_manufacturer=Sea ANIMALS [General] atc_type=Curtiss atc_model=Jenny editable=0 performance="Maximum Speed\n75 mph 65 kts 121 km/hr\n\nEngine\n90-hp Curtiss OX-5\n\nPropeller\nWood\n\nMaximum Range\n160 mi 257 km\n\nService Ceiling\n11,000 ft 3,353 m\n\nFuel Capacity\n21 gal 79 L\n\nEmpty Weight\n1,460 lb 662.25 kg\n\nMaximum Gross Weight\n1,920 lb 871 kg\n\nLength\n27 ft, 4 in 8.3 m\n\nWingspan\n43 ft, 7 in 13.35 m\n\nHeight\n9 ft, 10-5/8 in 4.7 m\n\nSeating\n2\n\nUseful Load\n460 lb 208 kg" [WEIGHT_AND_BALANCE] max_gross_weight = 1920 // (pounds) empty_weight = 1460 // (pounds) reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -1.52, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations =50 station_load.0 = "165.000, -4.8, 0.0, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "0.000, -1.4, 0.0, 0.0, Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 1005.8 empty_weight_roll_MOI = 1034.6 empty_weight_yaw_MOI = 2093.7 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 [Flaps.0] type= 0 [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 5.6, 0.0, 0.0 //(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 starter_type = 1 //1=Manual Starter [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 62.83 //Cubic inches per cylinder compression_ratio= 5.4 //Compression ratio number_of_cylinders=8 //Number of cylinders number_of_magnetos = 1 //Number of magnetos max_rated_rpm= 1400 //Max rated RPM max_rated_hp= 90 //Max rated HP fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 1 //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= 0 //Max design manifold pressure, (inHg) min_design_mp= 0 //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 = 1.0 //Propeller thrust scalar propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 8.28 //Propeller Diameter, (feet) propeller_blades= 2 //Number of propeller blades propeller_moi= 9.93 //Propeller moment of inertia beta_max= 0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 0 //Miminum governed RPM prop_tc= 0 //Prop time-constant gear_reduction_ratio= 1.0 //Propeller gear reduction ratio fixed_pitch_beta= 19 //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= 0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available= 0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 0 //Minimum RPM for prop feathering beta_feather= 0 //Feathering pitch angle (degrees) power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller 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 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees) //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=3, -17.50, 0.0, -2.20, 1200.0, 0, 0.00, 0.0, 0.400, 2.5, 0.495, 0.0, 0.0, 7.0, 0.0, 0.0 point.1=1, 0.70, -2.6, -5.18, 1600.0, 0, 1.10, 0.0, 0.400, 2.5, 0.486, 0.0, 0.0, 2.0, 0.0, 0.0 point.2=1, 0.70, 2.6, -5.18, 1600.0, 0, 1.10, 0.0, 0.400, 2.5, 0.482, 0.0, 0.0, 3.0, 0.0, 0.0 point.3=2, 0.00, -20.9, 3.10, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 point.4=2, 0.00, 20.9, 3.10, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0 point.5=2, 0.00, -16.6, -2.10, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 point.6=2, 0.00, 16.6, -2.10, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0 point.7=2, -20.00, 0.0, 4.30, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0 point.8=2, 4.40, 0.0, -3.00, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4.0, 0.0, 0.0 static_pitch = 9.44 static_cg_height = 4.64 [brakes] parking_brake = 0 //Parking brake available toe_brakes_scale = 0.0 //Brake scalar [hydraulic_system] normal_pressure = 0.0 //PSI [Views] eyepoint = -5.216, 0.0, 2.44 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, -4.0, 0.00, 1.80, fx_vclight, [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 0 Com.1 = 1, 0 Nav.1 = 0, 0, 0 Adf.1 = 0 Transponder.1 = 0 Marker.1 = 0 [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=0,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 0 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=0,0 [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 = 0 //Do not draw rain on this windshield [electrical] max_battery_voltage = 0 generator_alternator_voltage = 0 [fuel] Center1 = 0.7, 0.0, 0.0, 21.0, 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 = 1 electric_pump=0 [airplane_geometry] wing_area = 317.36 //Square feet wing_span = 43.608 //Feet wing_root_chord = 4.86 //Feet wing_dihedral = 1.0 //Degrees wing_incidence = 2.0 //Degrees wing_twist = 0.0 //Degrees oswald_efficiency_factor= 1.0 //Measure of lift effeciency of wing (Artificially high for biplanes) wing_winglets_flag = 0 //Are winglets available? wing_sweep = 0.0 //Degrees, wing leading edge wing_pos_apex_lon = 0.85 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 1.4 //Feet, vertical distance from reference point, positive going up htail_area = 56.0 //Square feet htail_span = 9.6 //Feet htail_pos_lon = -16.6 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = -1.1 //Feet, vertical distance from reference point, positive going up htail_incidence = 0.0 //Degrees htail_sweep = 0.0 //Degrees, horizontal tail leading edge vtail_area = 15.0 //Square feet vtail_span = 6.0 //Feet, tip to body vtail_sweep = 39.0 //Degrees, vertical tail leading edge vtail_pos_lon = -18.9 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 1.4 //Feet, vertical distance from reference point, positive going up elevator_area = 20.0 //Square feet aileron_area = 37.3 //Square feet rudder_area = 11.8 //Square feet elevator_up_limit = 30.0 //Degrees elevator_down_limit = 20.0 //Degrees aileron_up_limit = 20.0 //Degrees aileron_down_limit = 20.0 //Degrees rudder_limit = 25.0 //Degrees elevator_trim_limit = 0.0 //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 = 39.0 //Knots True (KTAS) full_flaps_stall_speed = 39.0 //Knots True (KTAS) cruise_speed = 54.7 //Knots True (KTAS) max_indicated_speed = 180 //Red line (KIAS) [autopilot] autopilot_available= 0 flight_director_available= 0 [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=0 [exits] number_of_exits = 1 exit_rate.0=0.09 ;Percent per second