[fltsim.0]
title=Gulf_IV
sim=Gulf_IV
model=
panel=
sound=
texture=
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
atc_id=N422ML
ui_manufacturer=Gulfstream
ui_type=Gulf_IV
ui_variation=EIB Rush's Plane
description=GIV is the plane chosen by my buddy Rush Hudson Limbaugh III. Therefore it must be the best.
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=GULFSTREAM
atc_model=GIV
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=1.402
parasite_drag_scalar=1.302
induced_drag_scalar=1.302
elevator_effectiveness=1.000
aileron_effectiveness=0.702
rudder_effectiveness=0.800
pitch_stability=1.202
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
min_throttle_limit=-0.549927
[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
gear_system_type=0
[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
electric_pump=0
[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
max_indicated_speed=564.000000
max_mach=0.879980
[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
default_bank_mode=0
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]
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
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=1
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
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
