[fltsim.0] title=Gulfstream V sim=ldgv model= panel= sound= texture= kb_checklists=GV_check kb_reference=GV_ref atc_id_enable=1 atc_id=PH-FVL ui_manufacturer=Gulfstream ui_type=Ultra long range large corporate transport ui_variation=Gulfstream G550 description=The Gulfstream G550 is the largest and latest development of the Gulfstream line of corporate transports, designed to fly intercontinental distances. It competes with Bombardier's Global Express, the Boeing Business Jet and Airbus A319CJ.\n\nModel, Sounds & Textures By:\nPeter Brun (peter@liderdesigns.com)\nFlight Dynamics and Data By:\nDouglas E. Trapp (KC6ZOF@Yahoo.com)\nFS Flight Dynamics Engineer\nArlington, Texas\nAugust 2009\n atc_airline= atc_flight_number= atc_heavy=0 visual_damage=1 atc_parking_types=GATE atc_parking_codes=INT atc_id_color=0xff000000 [General] atc_type=GULFSTREAM editable=1 performance=Note: Data below reflects this aircraft model with real-world specifications.\n\nPowerplants: Two Rolls-Royce BR710-48 @ 15,385 lbf ea\nLength: 96ft 5in\nHeight @ tail: 25ft 10in\nCabin length: 50ft 1in\nCabin height: 6ft 2in\nCabin width: 7ft 4in n\nWingspan: 93ft 5in\nWing area: 1,137 ft/sq\nEmpty weight: 48,300 lb\nMTOW: 91,000 lb\nRamp weight: 91,400 lb\nMLW: 75,300 lb\nFuel capacity: 6,164 US gal\nClimb rate: 2,000 ft/min to FL370\nMmo: .885\nLong distance cruise speeds:\nmach .80-.84 @ FL370 to FL450\nmach .83-.87 @ FL450 to FL510\nCertified service ceiling: FL510\nMax Range: 8,700 nm @ FL510E, mach .80\nCrew: 2\nPassengers: 6\nLuggage: 442 lb\n atc_model=G550 Category=airplane [contact_points] //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 point.0=1, 38.83, 0.00, -6.70, 981.1, 0, 0.8500, 70.0, 0.25, 2.5, 0.8878, 9.0, 10.0, 0, 180.0, 200.0 point.1=1, -2.19, -5.39, -8.10, 1174.8, 1, 1.5000, 0.0, 1.0, 2.5, 0.8456, 13.0, 15.0, 2, 180.0, 200.0 point.2=1, -2.19, 5.39, -8.10, 1174.8, 2, 1.5000, 0.0, 1.0, 2.5, 0.8456, 13.0, 15.0, 3, 180.0, 200.0 point.3=2, -5.83, -33.32, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -5.83, 33.32, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -36.29, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 46.47, 0.00, -1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch = -0.750 static_cg_height = 6.410 gear_system_type=0 [Views] eyepoint = 36.48, -1.15, 4.15 [electrical] // ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 flap_motor = 1, 0 , 1.0 gear_motor = 0, 5 , 17.0 avionics_bus = 0, 0 , 1.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 0 , 1.0 additional_system = 0, 0 , 1.0 marker_beacon = 1, 2 , 17.0 gear_warning = 7, 0 , 99.0 gear_motor = 4, 0 , 1.0 fuel_pump = 0, 0 , 1.0 fuel_transfer_pump = 0, 0 , 1.0 starter1 = 0, 20, 17.0 starter2 = 0, 0 , 1.0 light_nav = 0, 0 , 1.0 light_beacon = 0, 0 , 1.0 light_landing = 0, 0 , 1.0 light_taxi = 0, 0 , 1.0 light_strobe = 0, 0 , 1.0 light_panel = 0, 7 , 99.0 light_recognition = 0, 0 , 1.0 light_wing = 0, 0 , 1.0 marker_beacon = 0, 0 , 1.0 standby_vacuum = 0, 0 , 1.0 auto_brakes = 0, 0 , 1.0 hydraulic_pump = 0, 0 , 1.0 propeller_device = 0, 0 , 1.0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 0.8 induced_drag_scalar = 0.8 elevator_effectiveness = 1.0 aileron_effectiveness = 1.5 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 [airplane_geometry] wing_area=1137.000 wing_span=93.5 wing_root_chord=18.480 wing_dihedral=2.330 wing_incidence=0.000 wing_twist=1.000 oswald_efficiency_factor=2.500 wing_winglets_flag=1 wing_sweep=28.000 wing_aspect_ratio=7.7 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=244.870 htail_span=35.160 htail_pos_lon=-49.167 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=30.000 vtail_area=140.160 vtail_span=11.720 vtail_sweep=37.000 vtail_pos_lon=-47.917 vtail_pos_vert=5.833 elevator_area=57.500 aileron_area=25.000 rudder_area=32.300 elevator_up_limit=27.502 elevator_down_limit=20.626 aileron_up_limit=25.000 aileron_down_limit=25.000 rudder_limit=23.491 elevator_trim_limit=19.481 spoiler_limit=50.000 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 auto_spoiler_available=1 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=2.465812 negative_g_limit_flaps_up=-2.600427 negative_g_limit_flaps_down=-1.698718 [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 //Payload = 1,800 lb //Pax weight = 1,360 lb //Luggage weight = 442 lb @ 55 lb/pax station_load.0=170.000000,25.000000,2.5000000,1.800000//Pilot station_load.1=170.000000,25.000000,-2.5000000,1.800000//Co-Pilot station_load.2=170.000000,10.000000,3.500000,2.000000//Pax station_load.3=170.000000,10.000000,-3.500000,2.000000//Pax station_load.4=170.000000,5.000000,3.500000,2.000000//Pax station_load.5=170.000000,5.000000,-3.500000,2.000000//Pax station_load.6=170.000000,0.000000,3.500000,2.000000//Pax station_load.7=170.000000,0.000000,-3.500000,2.000000//Pax station_load.8=442.000000,-18.000000,0.000000,-2.000000//Luggage empty_weight= 48300.000 empty_weight_roll_MOI= 150774.000 empty_weight_pitch_MOI= 242040.000 empty_weight_yaw_MOI= 416940.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 91000.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] //6,164 US gal = 41,300 lb Center1= 1.800, 0.000, -3.000, 1380.000, 0.000 LeftMain= -1.800, -9.360, -1.500, 2392.000, 0.000 RightMain= -1.800, 9.360, -1.500, 2392.000, 0.000 fuel_type= 2.000 number_of_tank_selectors= 1 electric_pump=0 [GeneralEngineData] engine_type= 1 Engine.0= -18.667, -7.500, 5.750 Engine.1= -18.667, 7.500, 5.750 fuel_flow_scalar= 1.000000 min_throttle_limit=-0.250000 [smokesystem] smoke.0 = -28.667, -7.500, 5.750, fx_smoke_f6 smoke.1 = -28.667, 7.500, 5.750, fx_smoke_f6 [TurbineEngineData] //Rolls Royce BR710-48 bypass_ratio=3.3 fuel_flow_gain= 0.002 inlet_area= 5.91 rated_N1_rpm= 3854.000 rated_N2_rpm= 11055.000 static_thrust= 15385.000 afterburner_available= 0 reverser_available= 1 [jet_engine] thrust_scalar =1.000 [flaps.0] type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 8 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 20 // degrees flaps-position.2 = 20 // degrees flaps-position.3 = 25 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS [flaps.1] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 5 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 0 // degrees flaps-position.2 = 8 // degrees flaps-position.3 = 20 // degrees flaps-position.4 = 30 // degrees flaps-position.5 = 45 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS [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 = 100, 200 aileron = 100, 200 rudder = 100, 200 [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 [exits] number_of_exits = 1 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 [Reference Speeds] flaps_up_stall_speed = 112.0 //Knots True (KTAS) full_flaps_stall_speed = 102.0 //Knots True (KTAS) cruise_speed = 488.0 //Knots True (KTAS) max_indicated_speed=410.0 max_mach=0.885 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 2000.000 autothrottle_available= 1 autothrottle_arming_required= 1 autothrottle_takeoff_ga= 1 autothrottle_max_rpm= 110.000 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=30,15 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=11.00 nav_integrator_control=0.20 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [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=35999 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=35999 ; 0 - 35999 degrees crash_period2=75000000 ; in microseconds crash_duration2=25000000 ; in microseconds [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -13.25, -45.50, 0.55, fx_navredm , light.1=3, -13.25, 45.50, 0.55, fx_navgrem , light.2=3, -38.95, 0.00, 4.35, fx_navwhi ,100 light.3=2, -13.35, -45.75, 0.55, fx_strobe , light.4=2, -13.35, 45.75, 0.55, fx_strobe , light.5=1, 13.55, 0.00, 7.08, fx_beaconh , light.6=1, -2.55, 0.00,-2.50, fx_beaconb , light.7=4, 34.30, -1.50, 3.30, fx_vclight, light.8=4, 34.30, 1.50, 3.30, fx_vclight, light.9=1, 34.10, -1.00, 3.4, fx_vclighth , light.10=1, 34.10, 1.00, 3.4, fx_vclighth , [brakes] toe_brakes_scale=1.000000 parking_brake=1 auto_brakes=4 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0