[fltsim.0]
title=Gulfstream_IV (Paint 1)
sim=GulfIV_04
model=
panel=
sound=
texture=white
atc_id=G-AXZX
ui_manufacturer=Gulfstream
ui_type=Gulf_IV
ui_variation=Private Livery (White)
atc_heavy=0
atc_airline=
atc_flight_number=
description=Gulfstream IV. Original model by Rick Sasala, update for FS2004 and new FDE files by Roger Mole, August 2004.
[fltsim.1]
title=Gulfstream_IV (Paint 2)
sim=GulfIV_04
model=
panel=
sound=
texture=grey
atc_id=G-AXZX
ui_manufacturer=Gulfstream
ui_type=Gulf_IV
ui_variation=Private Livery (Grey)
atc_heavy=0
atc_airline=
atc_flight_number=
description=Gulfstream IV. Original model by Rick Sasala, update for FS2004 and new FDE files by Roger Mole, August 2004.
[fltsim.2]
title=Gulfstream_IV (Paint 3)
sim=GulfIV_04
model=
panel=
sound=
texture=brown
atc_id=G-AXZX
ui_manufacturer=Gulfstream
ui_type=Gulf_IV
ui_variation=Private Livery (Brown)
atc_heavy=0
atc_airline=
atc_flight_number=
description=Gulfstream IV. Original model by Rick Sasala, update for FS2004 and new FDE files by Roger Mole, August 2004.
[fltsim.3]
title=Gulfstream_IV (Paint 4)
sim=GulfIV_04
model=
panel=
sound=
texture=blue
atc_id=G-AXZX
ui_manufacturer=Gulfstream
ui_type=Gulf_IV
ui_variation=Private Livery (Blue)
atc_heavy=0
atc_airline=
atc_flight_number=
description=Gulfstream IV. Original model by Rick Sasala, update for FS2004 and new FDE files by Roger Mole, August 2004.
[General]
atc_type=GULFSTREAM
atc_model=
editable=0
performance=Cruise Speed\tMach .81\nMaximum Range\t2,200 nm\nService Ceiling\t51,000 ft\nMax Gross Weight\t20,450 lb\nSeating\t\tUp to 9\nUseful Load\t2,650 lb\n
Category=airplane
[pitot_static]
vertical_speed_time_constant=2 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[WEIGHT_AND_BALANCE]
max_gross_weight = 20450.0 // (pounds)
empty_weight = 11700.0 // (pounds)
reference_datum_position = 34.5, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -35.79, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, -17.0, -1.2, 0.0 //Pilot Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -17.0, 1.2, 0.0 //Co-Pilot Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 170, -22.5, -1.2, 0.0 //Pssngr 1 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 170, -22.5, 1.2, 0.0 //Pssngr 2 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 170, -26.7, -1.2, 0.0 //Pssngr 3 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 170, -26.7, 1.2, 0.0 //Pssngr 4 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 170, -30.9, -1.2, 0.0 //Pssngr 5 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = 170, -30.9, 1.2, 0.0 //Pssngr 6 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = 170, -35.1, -1.2, 0.0 //Pssngr 7 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = 170, -35.1, 1.2, 0.0 //Pssngr 8 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = 100, -42.0, 0.0, 0.0 //Baggage1 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = 50, -45.0, 0.0, 0.0 //Baggage2 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 320000
empty_weight_roll_MOI = 125000
empty_weight_yaw_MOI = 190000
empty_weight_coupled_MOI = 0.0
[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
[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 ,
[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 = 1.3
roll_stability = 1.0
yaw_stability = 1.3
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 = -42.8, -4.8, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -42.8, 4.8, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit=-0.250000
[TurbineEngineData]
fuel_flow_gain = 0.0025 //Gain on fuel flow
inlet_area = 4.2895 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 3500 //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
//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, -11.17, 0.00, -4.44, 1181.1, 0, 0.6349, 46.8, 0.4197, 2.5, 0.5878, 10.0, 10.0, 0, 0.0, 0.0
point.1=1, -37.25, -4.75, -4.92, 1574.8, 1, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 0.0, 0.0
point.2=1, -37.25, 4.75, -4.92, 1574.8, 2, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 0.0, 0.0
point.3=2, -37.83, -23.92, -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, -37.83, 23.92, -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, -57.17, 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, -11.47, 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 = -0.75
static_cg_height = 4.41
gear_system_type=0
[Views]
eyepoint = 4.51, -1.31, 6.14
[flaps.0]
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 = 8 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[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]
Center1 = -41.4, 0.0, -1.5, 359.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -36.3, -10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -36.3, 10.0, -1.5, 268.5, 0.0 //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 = 312.0 //Square feet
wing_span = 45.8 //Feet
wing_root_chord = 7.3 //Feet
wing_dihedral = 2.5 //Degrees
wing_incidence = 0.5 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.8 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 35.0 //Degrees, wing leading edge
wing_pos_apex_lon = -28.0 //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 = 67.0 //Square feet
htail_span = 17.2 //Feet
htail_pos_lon = -59.1 //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 = 2.0 //Degrees
htail_sweep = 25.0 //Degrees, horizontal tail leading edge
vtail_area = 42.0 //Square feet
vtail_span = 7.4 //Feet, tip to body
vtail_sweep = 30.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -55.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 4.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 17.0 //Square feet
aileron_area = 13.5 //Square feet
rudder_area = 7.3 //Square feet
elevator_up_limit = 17.0 //Degrees
elevator_down_limit = 15.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 4.6 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 5 //Degrees
min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
[Reference Speeds]
flaps_up_stall_speed = 112.0 //Knots True (KTAS)
full_flaps_stall_speed = 102.0 //Knots True (KTAS)
cruise_speed = 464.0 //Knots True (KTAS)
max_indicated_speed=530.000000
max_mach=0.810010
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
default_pitch_mode=0
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
[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
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[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
