[General] atc_type=Airbus atc_model=A300 editable=0 performance=Cruise Speed \nMach 0.84 555 mph 893 kmh\n\nEngine options \nP&W 4000\nRR Trent 800\nGE 90 series\n\nMaximum Range \n5,960 nm 6,859 sm 11,038 km\n\nService Ceiling \n42,000 ft 12,800 m\n\nFuel Capacity \n45,220 U.S. gal 171,160 L \n\nMaximum Takeoff Weight \n660,000 lb 299,370 kg\n\nLength \n242 ft, 4 in 73.9 m\n\nWingspan \n199 ft, 11 in 60.9 m\n\nHeight \n60 ft, 8 in 18.5 m\n\nSeating \nSeats 386 to 550 \n\nCargo Capacity \n7,552 ft 213.8 m\n [WEIGHT_AND_BALANCE] max_gross_weight = 760000 // (pounds) empty_weight = 381680 // (pounds) reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations =50 station_load.0 =0.000000,0.000000,0.000000,0.000000 ;Moments of Inertia empty_weight_pitch_MOI = 18000000 empty_weight_roll_MOI = 5500000 empty_weight_yaw_MOI = 16300000 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 [GeneralEngineData] engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 20.5, -75.5, -6.9 Engine.1 = 10.5, -38.6, -8.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.2 = 10.5, 38.6, -8.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.3 = 20.5, 75.5, -6.9 fuel_flow_scalar = 1 //Scalar for fuel flow efficiency min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain = 0.002 //Gain on fuel flow inlet_area = 18.0 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 45000 //Lbs, max rated static thrust at Sea Level afterburner_available = 0 //Afterburner available? reverser_available = 1 //Thrust reverser available? [jet_engine] thrust_scalar = 1.0 [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, 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, 87.42, 0.00, -16.10, 1581.1, 0, 4.521, 50.0, 0.63, 2.5, 0.7235, 4.0, 4.0, 0, 0.0, 0.0 point.1=1, -19.50, -12.00, -16.70, 2574.8, 1, 4.521, 0.0, 1.21, 2.5, 0.5470, 6.9, 6.9, 2, 0.0, 0.0 point.2=1, -19.50, 12.00, -16.70, 2574.8, 2, 4.521, 0.0, 1.21, 2.5, 0.5470, 7.1, 7.1, 3, 0.0, 0.0 point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -83.33, 0.00, 2.50, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch = -0.60 static_cg_height = 16.56 gear_system_type=0 [Views] eyepoint = 90.0, -2.65, 8.6 [flaps.0] //Inboard Trailing Edge type = 1 // 1 - tail, 2 - lead span-outboard = 0.2 // 0.0 .. 1.0 extending-time = 25 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 0 // degrees flaps-position.2 = 5 // degrees flaps-position.3 = 15 // degrees flaps-position.4 = 20 // degrees flaps-position.5 = 25 // degrees flaps-position.6 = 30 // degrees damaging-speed = 260 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.55 drag_scalar = 0.55 pitch_scalar= 0.55 system_type = 1 //Hydraulic [flaps.1] //Outboard Trailing Edge type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 23 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 0 // degrees flaps-position.2 = 5 // degrees flaps-position.3 = 15 // degrees flaps-position.4 = 20 // degrees flaps-position.5 = 25 // degrees flaps-position.6 = 30 // degrees damaging-speed = 260 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.35 drag_scalar = 0.35 pitch_scalar= 0.35 system_type = 1 //Hydraulic [flaps.2] //Inboard Leading Edge Slats type = 2 // 1 - tail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 4 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 0.5 // degrees flaps-position.2 = 0.5 // degrees flaps-position.3 = 0.5 // degrees flaps-position.4 = 0.5 // degrees flaps-position.5 = 1.0 // degrees flaps-position.6 = 1.0 // degrees damaging-speed = 260 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.05 drag_scalar = 0.05 pitch_scalar= 0.05 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 [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.1 = 1, 3.00, 0.00, -9.95, fx_beaconb , light.2 = 1, 49.00, 0.00, 9.90, fx_beaconh , light.3 = 2, 45.50, 9.29, -0.90, fx_navwhih light.4 = 2, 45.50, -9.29, -0.90, fx_navwhih light.5 = 3, -17.02,-75.12, 1.8, fx_navredh , light.6 = 3, -17.02, 75.12, 1.8, fx_navgreh , light.7 = 2, -17.60,-75.60, 2.0, fx_strobeh , light.8 = 2, -17.60, 75.60, 2.0, fx_strobeh , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [fuel] Center1 = 0.0, 0.0, -4.0, 12400.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -7.0, -35.0, 0.0, 16400.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -7.0, 35.0, 0.0, 16400.0, 3.0 //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 = 4605.0 //Square feet wing_span = 200.0 //Feet wing_root_chord = 23.0 //Feet wing_dihedral = 6.2 //Degrees wing_incidence = 1.0 //Degrees wing_twist = -0.5 //Degrees oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 32.0 //Degrees, wing leading edge wing_pos_apex_lon = 25.0 //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 = 1090.0 //Square feet htail_span = 70.7 //Feet htail_pos_lon = -100.0 //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 = 40.0 //Degrees, horizontal tail leading edge vtail_area = 573.0 //Square feet vtail_span = 27.3 //Feet, tip to body vtail_sweep = 35.0 //Degrees, vertical tail leading edge vtail_pos_lon = -108.3 //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 = 137.0 //Square feet aileron_area = 68.0 //Square feet rudder_area = 232.0 //Square feet elevator_up_limit = 15.0 //Degrees elevator_down_limit = 15.0 //Degrees aileron_up_limit = 30.0 //Degrees aileron_down_limit = 15.0 //Degrees rudder_limit = 25.0 //Degrees elevator_trim_limit = 20.0 //Degrees spoiler_limit = 60.0 //Degrees spoilerons_available = 0 //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 = 150.0 //Knots True (KTAS) full_flaps_stall_speed = 120.0 //Knots True (KTAS) cruise_speed = 400.0 //Knots True (KTAS) max_indicated_speed=430.000000 max_mach=0.900000 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1800.0 autothrottle_available= 1 autothrottle_arming_required= 1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga= 1 pitch_takeoff_ga = 8; 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] 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 [brakes] toe_brakes_scale=0.274667 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [fltsim.0] title=FSP A300B4 Philippines Airlines sim=A300 model= panel= sound= texture=Philippine atc_id= atc_airline=Philippine atc_flight_number=345 atc_heavy=1 ui_manufacturer=FS Painter ui_type=Airbus A300B2/B4 ui_variation=Philippines Airlines description=For AI aircraft