[fltsim.0]
title=Gulfstream_v sp pro INTER
sim=Gulfstream_v
model=
panel=
sound=
texture=
checklists=
kb_checklists=Gulfstream_V_CHECK
kb_reference=Gulfstream_V_REF 
atc_type=Gulf
atc_id_enable=1
atc_id=C9-TOZ
editable=0
atc_heavy=0
atc_airline=Hawaiian
atc_flight_number=105
visual_damage=20
description=Gulfstream V INTER\n\Paint by Mario Coelho www.bluestarsim.cjb.net  
ui_manufacturer=Gulfstream
ui_type=Gulfstream V
ui_variation=INTER

[General]
performance=Engines (2)BMW Rolls-Royce BR710\n\nMaximum Range (Mach 0.80, 8 passengers, 4 crew, NBAA IFR reserves)6,500 nm12,046 km\n\nLong Range Cruise SpeedMach 0.80459 ktas851 km\/h\n\nMmo (Maximum Allowable Mach Number)Mach 0.885  \n\nInitial Cruise Altitude41,000 ft12,497 m \nMaximum Cruise Altitude51,000 ft15,545 m\nMaximum Takeoff Weight90,500 lb41,051 kg\nPassengers (Maximum)19\nLength96 ft 5 in29.4 m\nHeight25 ft 10 in7.9 m\nWingspan93 ft 6 in28.5 \n\nby:OMC'99         08\/2000.\nAirfile rew. by Roy Hahmann
atc_type=GULFSTREAM
atc_model=V5

[SMOKESYSTEM]
//smoke.0=7.00,-73.00,8.70,fx_engsmoke.fx  ,//right engine;
//smoke.1=7.00,-73.00,8.70,fx_steam1.fx    ,//right engine;
//smoke.2=7.00,-73.00,8.70,fx_oilleak_m.fx ,//right engine;
//smoke.3=7.00,-73.00,8.70,fx_smkpuff_m.fx ,//right engine;
//smoke.4=7.00,-73.00,8.70,fx_launch2.fx    ,//right engine;

smoke.0=7.00,-73.00,-8.70,fx_smoke_rx.fx  ,//left engine;
smoke.1=7.00,-73.00, 8.70,fx_smoke_rx.fx  ,//right engine;

smoke.2=0.00,-63.50,-47.30, fx_contrail_s.fx
smoke.3=0.00,-63.50, 47.30, fx_contrail_s.fx

[LIGHTS]
//Types:1=beacon, 2=strobe, 3=navigation, 4=cockpit,(FRT & BCK),(L & R),(up&dn)
//5=landing 
light.0=3, -62.20, -47.30,  3.30, fx_navred,100
light.1=3, -62.20,  47.30,  3.30, fx_navgre,100
light.2=3, -83.30,   0.00,  8.00, fx_navwhi,100
light.3=2, -40.00,   0.00, -1.00, fx_strobe,100
light.4=1, -20.00,   0.00, 10.00, fx_beacon,100
light.5=1, -89.50,   0.00, 23.50, fx_beacon,100
//light.6=1, -40.00,   0.00, -1.00, fx_beacon,100
light.7=4,   7.00,   0.00,  9.00, fx_vclight,100
light.8=5, -26.50, -5.00,   1.00, fx_landing,100
light.9=5, -26.50,  5.00,   1.00, fx_landing,100
light.10=5, -26.50, -6.00,  1.00, fx_landing,100
light.11=5, -26.50,  6.00,  1.00, fx_landing,100
light.12=5,  7.00, -0.75,  -2.00, fx_landing,100
light.13=5,  7.00,  0.75,  -2.00, fx_landing,100
                                                    
[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

[WEIGHT_AND_BALANCE]
empty_weight=21700.0				// (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)
empty_weight_roll_MOI=892622.000000
empty_weight_pitch_MOI=1602999.000000
empty_weight_yaw_MOI=2003017.000000
empty_weight_coupled_MOI=1300.000000

[jet_engine]
thrust_scalar=1.0

[fuel]
Center1=-34.500000,0.000000,0.000000,1803.000000,0.000000
LeftMain=-34.500000,-33.333333,0.000000,2149.000000,0.000000
RightMain=-34.500000,33.333333,0.000000,2149.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=540.000000
wing_span=94.750000
wing_root_chord=12.000000
wing_dihedral=5.998535
wing_incidence=0.000000
wing_twist=-1.999512
oswald_efficiency_factor=4.356853
wing_winglets_flag=65535
wing_sweep=0.000000
wing_pos_apex_lon=-34.500000
wing_pos_apex_vert=0.000000
htail_area=408.000000
htail_span=41.666667
htail_pos_lon=-99.083333
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=305.000000
vtail_span=19.912308
vtail_sweep=0.000000
vtail_pos_lon=-95.583333
vtail_pos_vert=5.833333
elevator_area=102.000000
aileron_area=45.440000
rudder_area=51.850000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0=1.000000,-12.166667,0.000000,-6.000000,1574.803150,0.000000,0.946632,46.080000,0.191211,2.500000,1.621459,6.000000,6.000000,0.000000,0.000000,0.000000
point.1=1.000000,-38.666667,-5.583333,-6.416667,1574.803150,1.000000,0.946632,0.000000,0.942142,2.500000,0.584379,7.000000,7.000000,2.000000,0.000000,0.000000
point.2=1.000000,-38.666667,5.583333,-6.416667,1574.803150,2.000000,0.946632,0.000000,0.942142,2.500000,0.584379,7.500000,7.500000,3.000000,0.000000,0.000000
point.3=2.000000,-59.500000,-33.333333,-1.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-59.500000,33.333333,-1.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-59.500000,0.000000,2.500000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,5.500000,0.000000,2.083333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.000000
static_cg_height=6.007489

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=20.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=4.999057,0.000000
flaps-position.2=9.998114,0.000000
flaps-position.3=14.997170,0.000000
flaps-position.4=19.996227,0.000000
flaps-position.5=24.995284,0.000000
flaps-position.6=29.994341,0.000000
flaps-position.7=34.993397,0.000000
flaps-position.8=39.992454,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=-51.166667,-5.416667,-0.416667
Engine.1=-51.166667,5.416667,-0.416667
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=13.234200
rated_N2_rpm=29920.000000
static_thrust=12028.500000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=138.000000
full_flaps_stall_speed=110.400000
cruise_speed=557.252642

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=5.485236,-1.832657,6.997416

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_bank=1 
use_no_default_pitch=0 

[direction_indicators]
direction_indicator.0=3,0

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 10, 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 20, 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 17.0
light_nav          = 0, 5 , 17.0
light_beacon       = 0, 5 , 17.0
light_landing      = 0, 5 , 17.0
light_taxi         = 0, 5 , 17.0
light_strobe       = 0, 5 , 17.0
light_panel        = 0, 5 , 17.0

[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

[EFFECTS]
wake=fx_wake_m
water=fx_waterland
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
contrail=fx_contrail_l,100

[exits]
number_of_exits=2
exit_rate.0=0.4
exit_rate.1=0.4