[fltsim.0] title=Gulf_IV sim=Gulf_IV model= panel= sound= texture= kb_checklists=Gulf_IV_check kb_reference=Gulf_IV_ref atc_id=G02CF ui_manufacturer=Gulfstream ui_type=Gulf_IV ui_variation=Ferrari F1 Team description=The Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine of the top ten Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream IV has a range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as high as 45,000 feet, enabling it to fly above commercial airline traffic and adverse weather. atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=GULFSTREAM atc_model= editable=1 performance=Cruise Speed Mach 0.81 464 kts 859kmh\nEngines\tRolls Royce TAY611-8 13,850 lb thrust\nMaximum Range 4,480 nm\nService Ceiling 45,000 ft 15,545 m\n\nFuel Capacity\t\n29,500lb \n\nMaximum Gross Weight\t\n74,500 lb \n\nUseful Load\t\n31,750 lb [WEIGHT_AND_BALANCE] max_gross_weight= 74500.000 empty_weight= 49000.000 reference_datum_position= 34.500, 0.000, 0.000 empty_weight_CG_position= -35.790, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, -17.000, -1.200, 0.000 station_load.1= 170.000, -17.000, 1.200, 0.000 station_load.2= 170.000, -22.500, -1.200, 0.000 station_load.3= 170.000, -22.500, 1.200, 0.000 station_load.4= 170.000, -26.700, -1.200, 0.000 station_load.5= 170.000, -26.700, 1.200, 0.000 station_load.6= 170.000, -30.900, -1.200, 0.000 station_load.7= 170.000, -30.900, 1.200, 0.000 station_load.8= 170.000, -35.100, -1.200, 0.000 station_load.9= 170.000, -35.100, 1.200, 0.000 station_load.10= 100.000, -42.000, 0.000, 0.000 station_load.11= 50.000, -45.000, 0.000, 0.000 ;Moments of Inertia empty_weight_pitch_MOI= 350048.000 empty_weight_roll_MOI= 177442.000 empty_weight_yaw_MOI= 543541.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [electrical] max_battery_voltage=12.0 generator_alternator_voltage=13.8 max_generator_alternator_amps=40.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=0, 10, 9.5 avionics=1, 5 , 9.5 additional_system=0, 20, 9.5 marker_beacon=1, 2 , 9.0 fuel_pump=0, 5 , 9.0 [flight_tuning] cruise_lift_scalar=1.401 parasite_drag_scalar=1.301 induced_drag_scalar=1.301 elevator_effectiveness=1.000 aileron_effectiveness=0.701 rudder_effectiveness=0.800 pitch_stability=1.201 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type= 1 Engine.0= -42.800, -4.800, 0.800 Engine.1= -42.800, 4.800, 0.800 fuel_flow_scalar= 0.900 [TurbineEngineData] fuel_flow_gain= 0.003 inlet_area= 8.290 rated_N2_rpm= 29920.000 static_thrust= 13850.000 afterburner_available= 0 reverser_available= 1 [jet_engine] thrust_scalar=1.000 [SMOKESYSTEM] smoke.0=0.8,-48.4,-4.8, fx_smoke_rxS3 smoke.1=0.8,-48.4, 4.8, fx_smoke_rxS3 //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= 1.000, -11.170, 0.000, -4.120, 3200.100, 0.000, 0.635, 45.000, 0.120, 2.500, 0.850, 10.000, 10.000, 0.000, 0.000, 0.000 point.1= 1.000, -37.250, -6.750, -5.520, 3200.800, 1.000, 0.635, 0.000, 1.000, 2.500, 0.946, 9.000, 9.000, 2.000, 0.000, 0.000 point.2= 1.000, -37.250, 6.750, -5.520, 3200.800, 2.000, 0.635, 0.000, 1.000, 2.500, 0.946, 9.000, 9.000, 3.000, 0.000, 0.000 point.3= 2.000, -37.830, -23.920, -3.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -37.830, 23.920, -3.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -57.170, 0.000, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, -11.470, 0.000, -1.500, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= -0.750 static_cg_height= 4.410 [Views] eyepoint=4.31, -1.31, 6.44 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=1, -18.223, 0.00, 8.595, fx_beaconbGulf , light.1=1, -36.572, 0.00, 0.30, fx_beaconbGulf , light.2=3, -41.75, -39.00, 2.80, fx_navredm , light.3=3, -41.75, 39.00, 2.80, fx_navgrem , light.4=2, -41.75, -39.00, 2.80, fx_strobe , light.5=2, -41.75, 39.00, 2.80, fx_strobe , light.6=2, -67.10, 0.00, 5.73, fx_strobe , light.7=3, -67.10, 0.00, 5.73, fx_navwhi , light.8=4, 4.90, 0.00, 5.44, fx_vclight , light.9=4, -0.50, 0.00, 5.44, fx_vclight , light.10=4, -10.00, 0.00, 5.44, fx_vclighth , light.11=4, -20.00, 0.00, 5.44, fx_vclighth , light.12=4, -33.00, 0.00, 5.44, fx_vclighth , light.13=6, 17.0, 0.00, -5.0, RNLE2 , light.14=5, -10.0, -4.00, -5.0, RNLE2 , light.15=5, -10.0, 4.00, -5.0, RNLE2 , [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 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 water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [fuel] LeftMain= -36.300, -10.000, -1.500, 2202.200, 0.000 RightMain= -36.300, 10.000, -1.500, 2202.200, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [exits] number_of_exits=2 exit_rate.0=0.05 exit_rate.1=0.1 [airplane_geometry] wing_area= 950.390 wing_span= 77.100 wing_root_chord= 12.320 wing_dihedral= 2.500 wing_incidence= 0.000 wing_twist= -4.000 oswald_efficiency_factor= 0.860 wing_winglets_flag= 1 wing_sweep= 35.000 wing_pos_apex_lon= -28.000 wing_pos_apex_vert= 0.000 htail_area= 220.000 htail_span= 32.000 htail_pos_lon= -59.100 htail_pos_vert= 0.000 htail_incidence= 2.000 htail_sweep= 30.000 vtail_area= 82.000 vtail_span= 12.400 vtail_sweep= 35.000 vtail_pos_lon= -55.000 vtail_pos_vert= 4.100 elevator_area= 57.000 aileron_area= 23.500 rudder_area= 47.300 elevator_up_limit= 17.000 elevator_down_limit= 15.500 aileron_up_limit= 18.000 aileron_down_limit= 18.000 rudder_limit= 30.000 elevator_trim_limit= 15.000 spoiler_limit= 55.000 spoilerons_available= 1 aileron_to_spoileron_gain= 2.200 min_ailerons_for_spoilerons= 5.000 min_flaps_for_spoilerons= 0.000 [Reference Speeds] flaps_up_stall_speed= 112.000 full_flaps_stall_speed= 102.000 cruise_speed= 464.000 [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=8.00000 use_no_default_bank=1 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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 [Flaps.0] type= 1 span-outboard= 0.800 extending-time= 5.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.500 drag_scalar= 1.200 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 39.000, 0.000