[fltsim.0] title=2UFOGA sim=Boeing737-400 model= panel= sound= texture=2UFOGA kb_checklists=Boeing737-400_check kb_reference=Boeing737-400_ref atc_id=U102 atc_airline=UFO atc_flight_number=102 ui_manufacturer=1GUZMAN_ARTES ui_type=FLYING SAUCER ui_variation=FLYABLE description=FLYABLE MODEL - UFO - BY LIBARDO GUZMAN - GUZMAN_ARTES [General] atc_type=UFO atc_model=FLYING SAUCER editable=0 performance="Velocidad de crucero UNKNOWN / Motores UNKNOWN / Alcance máximo UNKNOWN / Techo de servicio UNKNOWN / [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight = 2 // (pounds) empty_weight = 2 // (pounds) reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "170.0, 41.0, -1.5, 0.0, Piloto" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "170.0, 41.0, 1.5, 0.0, Copiloto" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "510.0, 0.0, 0.0, 0.0, Tripulación" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "1360.0, 25.5, 0.0, 0.0, Primera clase" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "8160.0, 11.0, 0.0, 0.0, Turista 3-10" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = "8160.0, -10.0, 0.0, 0.0, Turista 11-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = "7140.0, -30.5, 0.0, 0.0, Turista 19-25" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = "10000.0, 20.5, 0.0, 0.0, Equipaje anterior" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8 = "4000.0, -27.5, 0.0, 0.0, Equipaje posterior" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 13172439 empty_weight_roll_MOI = 12262183 empty_weight_yaw_MOI = 1337024 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 2.0 parasite_drag_scalar = 9.0 induced_drag_scalar = 0.5 elevator_effectiveness = 20.0 aileron_effectiveness = 19.0 rudder_effectiveness = 59.0 pitch_stability = 9.0 roll_stability = 9.0 yaw_stability = 3.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 9.0 rudder_trim_effectiveness = 1.0 [GeneralEngineData] engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 4.75, -16.1, -4.5 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = 4.75, 16.1, -4.5 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 1 //Scalar for fuel flow efficiency min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear [TurbineEngineData] fuel_flow_gain = 0.002 //Gain on fuel flow inlet_area = 19.6 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 23500 //Lbs, max rated static thrust at Sea Level afterburner_available = 0 //Afterburner available? reverser_available = 1 //Thrust reverser available? [jet_engine] thrust_scalar = 8.0 [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, 5, 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 2, 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, 40.00, 0.00, -8.40, 1181.1, 0, 1.442, 55.92, 0.6, 2.5, 0.9, 4.0, 4.0, 0, 220.0, 250.0 point.1=1, -7.75, -8.58, -8.60, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0 point.2=1, -7.75, 8.58, -8.60, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.9, 7.1, 7.1, 3, 220.0, 250.0 max_number_of_points = 21 static_pitch=0.04 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=7.67 //feet, altitude of CG when at rest on the ground gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 5.0 //Flap angle that activates warning at idle flap_limit_power = 25.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 2.885 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=43.7, -1.31, 3.7 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] //Trailing Edge Flaps type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 0.1 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 1 // degrees flaps-position.2 = 2 // degrees flaps-position.3 = 5 // degrees flaps-position.4 = 10 // degrees flaps-position.5 = 15 // degrees flaps-position.6 = 25 // degrees flaps-position.7 = 30 // degrees flaps-position.8 = 40 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 9.0 drag_scalar = 9.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.1] //Inboard Leading Edge Flaps type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 0.1 // seconds flaps-position.0 = 0 // flaps-position.1 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 9.0 drag_scalar = 9.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.2] //Outboard Leading Edge Slat type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 0.1 // seconds flaps-position.0 = 0 // flaps-position.1 = 0.5 // flaps-position.4 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 9.0 drag_scalar = 3.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -0.0, -48.0, -0.5, fx_navgrem , light.1 = 3, -0.0, 48.0, -0.5, fx_navgrem , light.2 = 2, -0.0, -48.0, -0.5, fx_strobeh , light.3 = 2, -0.0, 48.0, -0.5, fx_strobeh , light.4 = 2, 0.0, 0.00, -4.60, fx_beaconb , light.5 = 1, 0.00, 0.00, 10.00, fx_beaconh , light.6 = 3, 48.0, 0.0, -0.5, fx_navgrem , light.7 = 3, -48.0, 0.0, -0.5, fx_navgrem , light.8 = 2, 48.0, 0.0, -0.5, fx_strobeh , light.9 = 2, -48.0, 0.0, -0.5, fx_strobeh , light.10 = 3, -34.0, -34.0, -0.5, fx_navredm , light.11 = 3, 34.0, -34.0, -0.5, fx_navredm , light.12 = 3, -34.0, 34.0, -0.5, fx_navredm , light.13 = 3, 34.0, 34.0, -0.5, fx_navredm , light.14 = 3, -34.0, -34.0, -0.5, fx_strobeh , light.15 = 3, 34.0, -34.0, -0.5, fx_strobeh , light.16 = 3, -34.0, 34.0, -0.5, fx_strobeh , light.17 = 3, 34.0, 34.0, -0.5, fx_strobeh , [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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga=1 pitch_takeoff_ga = 8; max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=12.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=25.0 gs_integrator_control=0.53 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [fuel] Center1 = 0, 0, 0, 2313, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -3, -59, 0, 1500, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -3, 59, 0, 1500, 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 electric_pump=0 [airplane_geometry] wing_area = 1137.0 //Square feet wing_span = 94.75 //Feet wing_root_chord = 18.0 //Feet wing_dihedral = 6.2 //Degrees wing_incidence = 1.0 //Degrees wing_twist = -0.5 //Degrees oswald_efficiency_factor= 0.75 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 25.0 //Degrees, wing leading edge wing_pos_apex_lon = 8.0 //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 = 338.0 //Square feet htail_span = 41.7 //Feet htail_pos_lon = -35.0 //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 = 0.0 //Degrees htail_sweep = 30.0 //Degrees, horizontal tail leading edge vtail_area = 424.0 //Square feet vtail_span = 20.0 //Feet, tip to body vtail_sweep = 35.0 //Degrees, vertical tail leading edge vtail_pos_lon = -35.8 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 5.8 //Feet, vertical distance from reference point, positive going up elevator_area = 70.5 //Square feet aileron_area = 26.9 //Square feet rudder_area = 56.2 //Square feet elevator_up_limit = 22.5 //Degrees elevator_down_limit = 19.5 //Degrees aileron_up_limit = 20.0 //Degrees aileron_down_limit = 20.0 //Degrees rudder_limit = 26.0 //Degrees elevator_trim_limit = 20.0 //Degrees spoiler_limit = 60.0 //Degrees spoilerons_available = 1 //Spoilerons Available? aileron_to_spoileron_gain = 3 //Aileron to spoileron gain min_ailerons_for_spoilerons = 10 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed = 0.1 //Knots True (KTAS) full_flaps_stall_speed = 0.1 //Knots True (KTAS) cruise_speed = 4477.0 //Knots True (KTAS) max_mach = 4.82 max_indicated_speed = 4340 //Red line (KIAS) [forcefeedback] 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=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 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 [stall_warning] type=2