[fltsim.0] title= sim=FeelThere_A330-200 ui_manufacturer=Simmer's Sky ui_type=Airbus A330-200 PW ui_variation= description=Overland Co.,Ltd. Products --- Airbus A330-200\n\nL1 Cabin Door [Shift+E] then [1]\nCargo Door Operate with Door Display Gauge\nL2 Cabin Door Operate with Door Display Gauge [General] visual_damage=1 // 0=off, 1=on atc_type=AIRBUS atc_model=A330 editable=0 performance=Cruise Speed\tMach .83\nMaximum Range\t6,400 nm\nService Ceiling\t33,000 ft\nMax Takeoff Weight\t507,050 lb\nSeating\t\t256 to 293\nCargo Capacity\t32 standard LD3 containers \n [WEIGHT_AND_BALANCE] max_gross_weight=509050 // (pounds) empty_weight=264875 // (pounds) reference_datum_position = 0.0, 0.0,-6.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0.0, 0.0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0 = "170.0, 80.4, -2.0, 0.0, Pilot" //Weight (lbs), station_load.1 = "170.0, 80.4, 2.0, 0.0, Co-Pilot" //Weight (lbs), station_load.2 = "850.0, 3.0, 0.0, 0.0, Crew" //Weight (lbs), station_load.3 = "1200.0, 65.0, 0.0, 0.0, First Class" //Weight (lbs), station_load.4 = "2720.0, 34.0, 0.0, 0.0, Business" //Weight (lbs), station_load.5 = "4960.0, -7.0, 0.0, 0.0, Coach 1-8" //Weight (lbs), station_load.6 = "7800.0, -49.5, 0.0, 0.0, Coach 9-18" //Weight (lbs), station_load.6 = "1600.0, -75.5, 0.0, 0.0, Coach 19-23" //Weight (lbs), station_load.7 = "1400.0, 44.0, 0.0, -6.0, Forward Cargo" //Weight (lbs), station_load.8 = "500.0, -39.0, 0.0, -6.0, Aft Cargo" //Weight (lbs), ;Moments of Inertia empty_weight_roll_MOI=21100000 empty_weight_pitch_MOI=21400000 empty_weight_yaw_MOI=15800000 empty_weight_coupled_MOI=0.0 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [pitot_static] vertical_speed_time_constant=999 [GROUND_REACTION] MAX_STEERING_ANGLE=75 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.0001 induced_drag_scalar =1.1 elevator_effectiveness =1.0 aileron_effectiveness =1.0 rudder_effectiveness =1.0 pitch_stability =1.000 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =0.6 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0= 12.60, -29.90, -6.10 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1= 12.60, 29.90, -6.10 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=0.70225 min_throttle_limit=-0.7 [TurbineEngineData] fuel_flow_gain=0.001 //Gain on fuel flow inlet_area= 68.3 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=70000 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=0.96 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 200 electric_always_available = 1 flap_motor = 0, 0 , 17.0 gear_motor = 0, 0 , 17.0 autopilot = 0, 0 , 17.0 avionics_bus = 0, 0 , 17.0 avionics = 0, 0 , 17.0 pitot_heat = 0, 0 , 17.0 additional_system = 0, 0 , 17.0 marker_beacon = 0, 0 , 17.0 gear_warning = 0, 0 , 17.0 fuel_pump = 0, 0 , 17.0 starter1 = 0, 0 , 17.0 starter2 = 0, 0 , 17.0 light_nav = 0, 0 , 17.0 light_beacon = 0, 0 , 17.0 light_landing = 0, 0 , 17.0 light_taxi = 0, 0 , 17.0 light_strobe = 0, 0 , 17.0 light_panel = 0, 0 , 17.0 light_cabin = 0, 0 , 17.0 auto_brakes = 0, 0 , 17.0 standby_vacuum = 0, 0 , 17.0 hydraulic_pump = 0, 0 , 17.0 fuel_transfer_pump = 0, 0 , 17.0 light_recognition = 0, 0 , 17.0 light_wing = 0, 0 , 17.0 light_logo = 0, 0 , 17.0 directional_gyro = 0, 0 , 17.0 directional_gyro_slaving = 0, 0 , 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, 73.42, 0.00, -14.42, 1181.1, 0, 4.521, 75.0, 0.50, 2.1, 0.8135,11.0, 13.2, 0, 0.0, 0.0 //nose point.1=1, -5.00, -15.80, -17.12, 1574.8, 1, 4.737, 0.0, 1.51, 2.0, 0.7470, 9.7, 14.1, 2, 0.0, 0.0 //left main 1.1 was 2.0 point.2=1, -5.00, 15.80, -17.12, 1574.8, 2, 4.737, 0.0, 1.51, 2.0, 0.7470, 9.7, 14.1, 3, 0.0, 0.0 //right main point.3=1, -8.20, -15.90, -16.04, 1574.8, 1, 4.737, 0.0, 1.51, 2.0, 0.7470, 9.7, 14.1, 2, 0.0, 0.0 //left point.4=1, -8.20, 15.90, -16.04, 1574.8, 2, 4.737, 0.0, 1.51, 2.0, 0.7470, 9.7, 14.1, 3, 0.0, 0.0 //right point.5=2, -10.17, -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.6=2, -10.17, 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.7=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.8=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 point.9=2, 73.47, 0.00, -9.70, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 static_pitch=-0.00830 static_cg_height=20.670 gear_system_type=0 [smokesystem] smoke.0= -13.60, -29.90, -14.90 ,fx_wetrnwyspray smoke.1= -13.60, 29.90, -14.90 ,fx_wetrnwyspray [Views] eyepoint=88.74, -1.80, 5.85 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cabin light.1 = 1, 30.25, 0.00, -7.90, fx_shockwave_beaconb , light.2 = 1, 17.60, 0.00, 12.00, fx_shockwave_beaconh , light.3 = 2, -97.42, 0.00, 9.00, fx_shockwave_strobe_l , light.4 = 3, -97.42, 0.00, 9.00, fx_shockwave_navwhi_l_nl , light.5 = 5, 31.500, 10.500, -2.00, fx_shockwave_landing_light_narrow light.6 = 5, 31.500, -10.500, -2.000, fx_shockwave_landing_light_narrow light.7 = 4, 99.02, 0, 5.3, Fx_shockwave_vclight light.8 = 6, 76.000, 0.0, -7.3, fx_shockwave_landing_light_a321_nose light.9 = 4, 99.02, 0, 5.3, fx_vclight_l light.10 = 8, 56.635, -9.4, 2.30, fx_shockwave_navwhi , // Left wing light light.11 = 8, 54.635, -9.4, 2.30, fx_shockwave_navwhi , // Left wing light light.12 = 8, 56.635, 9.4, 2.30, fx_shockwave_navwhi , // Right wing light light.13 = 8, 54.635, 9.4, 2.30, fx_shockwave_navwhi , // Right wing light [Flaps.0] type=1 span-outboard=0.500000 extending-time=20.000000 system_type=1 flaps-position.0=0.000000,0.000000 flaps-position.1=0.0 flaps-position.2=15.0 //nominal value should be10 but we need big effect RY flaps-position.3=20.0 //ditto to accomodate flap 2 flaps-position.4=26.0 //ditto to accomodate flap 2 flaps-position.5=35.0 //ditto to accomodate flap 2 [Flaps.1] type=2 span-outboard=0.800 extending-time=20.000 system_type=1 damaging-speed=232.000 blowout-speed=250.000 lift_scalar=0.3 drag_scalar=0.2 pitch_scalar=0.0 flaps-position.0=0 flaps-position.1=18.0 flaps-position.2=18.0 flaps-position.3=22.0 flaps-position.4=22.0 flaps-position.5=27.0 [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 [EFFECTS] wake=fx_wake_l water=fx_nicks_tchwater dirt=fx_nicks_tchdirt_m concrete=fx_sparks touchdown=fx_tchdwn windshield_rain_effect_available=1 SnowTrack = fx_snowtrack WheelSnowSpray = fx_wtrspray_l WheelWetSpray = fx_wtrspray_l [fuel] // Max Fuel Capacity 51,379.0 (54,023.2) USg Center1 = 1.0, 0.0, -4.0, 10980.0, 21.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2 =-11.0, 0.0, -4.0, 1646.0, 6.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = 0.0, -25.0, 0.0, 11095.0, 32.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = 0.0, 25.0, 0.0, 11095.0, 32.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux= -1.0, -38.0, 0.0, 964.0, 0.0 RightAux= -1.0, 38.0, 0.0, 964.0, 0.0 fuel_type=2.000000 number_of_tank_selectors=2 electric_pump=1 [airplane_geometry] wing_area=3908.4 //Square feet wing_span=197.10 //Feet wing_root_chord=24.0 //Feet wing_dihedral=5.8 //Degrees wing_incidence=0.0 //Degrees wing_twist=-0.0 //Degrees oswald_efficiency_factor=0.773 //Measure of lift effeciency of wing 8723 wing_winglets_flag=1 //Are winglets available? wing_sweep=32.0 //Degrees, wing leading edge wing_pos_apex_lon=34.90 //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=767.0 //Square feet htail_span=63.6 //Feet htail_pos_lon=-78.50 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=8.0 //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=493.0 //Square feet vtail_span=27.3 //Feet, tip to body vtail_sweep=29.0 //Degrees, vertical tail leading edge vtail_pos_lon=-62.70 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=12.0 //Feet, vertical distance from reference point, positive going up elevator_area=97.0 //Square feet aileron_area=38.0 //Square feet rudder_area=62.0 //Square feet elevator_up_limit=30.0 //Degrees elevator_down_limit=20.0 //Degrees aileron_up_limit=25.0 //Degrees aileron_down_limit=15.0 //Degrees rudder_limit=29.0 //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=180.000000 // at MTW full_flaps_stall_speed=132.000000// at MTW cruise_speed=320 max_indicated_speed=475.000000 max_mach=0.86 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1200.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 max_pitch=10.000000 max_pitch_acceleration=0.8 max_pitch_velocity_lo_alt=1.0 max_pitch_velocity_hi_alt=1.0 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=29.000000 max_bank_acceleration=3.0 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=0.86000000 parking_brake=1 differential_braking_scale = 1.0 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=10.04 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=100,100 ;Percent per second [TailHook] tailhook_length=4 ;(feet) tailhook_position=0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0.0 [exits] number_of_exits = 3 exit_rate.0 = 100 ;Percent per second exit_rate.1 = 100 ;Percent per second exit_rate.2 = 100 ;Percent per second