
[fltsim.0]
title=PSS Boeing 777-300ER ONYX Swiss
sim=PSSB773ER-GE
model=novc
panel=
sound=
texture=SWISS
atc_id=HB-XXX
atc_airline=Onyx Swiss
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=FeelThere/ONYX TEST
ui_type="777-300ER No VC Model"
ui_variation=KLM
description=THE PSS 777 TEAM ARE:\n--------------------------------------------------------\nPanel Programming: Alex Baskatov\nPanel Art: Lena Bashkatov \nModel: Graham Waterfield\nTextures: Ben Jones\nVirtual Cockpit: Anthony Waterfield\nFDE: Eugene "Schtirlitz" Schneider\nSounds: Mike Hambly\nResearch: Robert Kirkland\nSupport - Web: Norman Blackburn, Alex Greenland\nWeather Radar: Florian "AOG" Praxmarer\n\nSpecial Thanks Goes Out To:\nAdam Gaweda, Cyrille DeLattre, Michael Benson, Richard Green, Lee Holland, Steve Cullen, Terry Scanlan, Mark Richards, Joe Park, Chris File, Bob Scott.\n\nCopyright Phoenix Simulation Software (C) 2005" www.phoenix-simulation.co.uk\n\nSEE MANUAL FOR DETAILED INSTRUCTIONS. "
atc_airline=Onyx siwss
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_parking_types=RAMP,GATE
atc_parking_codes=ONY

////////////////////////////////////////////////////////////////////
//JFDVD


[General]
atc_type=BOEING 
atc_model=B773 
editable=0 
performance="Cruise Speed        \nMach 0.84         555 mph         893 kmh\n\nEngine options        \nP&W 4000\nRR Trent 800\nGE 90 series\n\nMaximum Range              \n5,960 nm          6,859 sm        11,038 km\n\nService Ceiling    \n42,000 ft           12,800 m\n\nFuel Capacity       \n45,220 U.S. gal        171,160 L \n\nMaximum Takeoff Weight     \n660,000 lb        299,370 kg\n\nLength    \n242 ft, 4 in         73.9 m\n\nWingspan      \n199 ft, 11 in          60.9 m\n\nHeight        \n60 ft, 8 in           18.5 m\n\nSeating       \nSeats 386 to 550 \n\nCargo Capacity        \n7,552 ft              213.8 m\n" 

[weight_and_balance]

// ACM V2.5
max_gross_weight = 777000
empty_weight = 370000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 26443208
empty_weight_roll_MOI = 8710758
empty_weight_yaw_MOI = 24371969
empty_weight_coupled_MOI = 0
max_number_of_stations = 14

station_load.0 = 360, 112.7, 0, 4.12, 	Cockpit Crew
station_load.1 = 1080, 0, 0, 0,		Cabin Crew

station_load.2 = 3960, 85, 0, 0,	First Class
station_load.3 = 12600, 40, 0, 0,	Business Class
station_load.4 = 19440, 0, 0, 0,	Coach Y1
station_load.5 = 19440, -20, 0, 0,	Coach Y2

station_load.6 = 2316, 40, 0, 0, 	Containers P. 1
station_load.7 = 6952, 10, 0, 0,	Containers P. 2
station_load.8 = 6952, -30, 0, 0, 	Containers P. 3
station_load.9 = 11027, -60, 0, 0,	Containers P. 4
station_load.10 = 1325, -70, 0, 0,	Bulk Cargo P. 5


station_load.11 = 474, 0, 0, 0, 	Meals
station_load.12 = 139, 0, 0, 0,		Potable Water
station_load.13 = 20, 0, 0, 0,		Lav Service


[GeneralEngineData]
//JFDVD
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.0401
min_throttle_limit = -0.25
engine.0 = 32.75, -32.03, -7.41,
engine.1 = 32.75, 32.03, -7.41,

[smokesystem]
smoke.0 = 5.90, -27.40, 77.13, fx_pss_fuel_jett
smoke.1 = 5.9, -27.4, -77.13, fx_pss_fuel_jett

[effects]
wake = fx_wake
water = fx_spray
waterspeed = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
startup = fx_pss_startup
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 4
electric_pump = 1

Center1 = 5, 0, -4, 20550, 3
LeftMain = 5, -35, 0, 9300, 3
LeftAux = -10, -60, 3, 4370, 0
RightMain = 5, 35, 0, 9300, 3
RightAux = -10, 60, 3, 4370, 0


[contact_points]
static_pitch = 0.1
static_cg_height = 17.56
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 17

point.0 = 1, 100.6083, 0, -17.5803, 1181.1, 0, 4.521, 65, 1, 2.5, 0.7235, 13, 14, 0, 270, 270
point.1 = 1, -6.76, -20, -18.5905, 1574.8, 1, 4.521, 8, 1.91, 2.5, 0.747, 13, 14, 2, 270, 270
point.2 = 2, 30.8612, -31.5494, -14.1458, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.3 = 2, 30.8612, 31.5494, -14.1458, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.4 = 1, -6.76, 20, -18.5905, 1574.8, 2, 4.521, 8, 1.91, 2.5, 0.747, 12.9, 13.9, 3, 270, 270
point.5 = 2, -115, -36, 9, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.6 = 2, -38.4, -105, 12.5, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.7 = 2, -115, 36, 9, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.8 = 2, -38.4, 105, 12.5, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.9 = 2, -116.5152, 0, 44.1266, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.10 = 2, -115.5083, 0, 3.1359, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.11 = 2, -85.5589, 0, -4.8617, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.12 = 2, -56.4399, 0, -8.5634, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.13 = 2, -116.3871, 0, 3.9812, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.14 = 2, 50.4709, 0, 13.0267, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.15 = 2, 120.1817, 0, 0.4276, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.16 = 5, 0.0, 0.0, -10.0, 1600, 0.0, 0.0, 50.0, 0.0, 0.0, 1.00, 1.0, 1.0, 0, 0.0, 0.0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[airplane_geometry]

wing_area = 4604.801
wing_span = 212.58
wing_root_chord = 21.65
wing_dihedral = 3.90
wing_incidence = 1.0
wing_twist = -2
oswald_efficiency_factor = 0.88667
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 5.40
wing_pos_apex_vert = -4.46
htail_area = 1089.954
htail_span = 70.04
htail_pos_lon = -100.23
htail_pos_vert = 5.78
htail_incidence = 0.0
htail_sweep = 40
vtail_area = 572.963
vtail_span = 33.23
vtail_sweep = 35
vtail_pos_lon = -94.60
vtail_pos_vert = 10.63
elevator_area = 137.0
aileron_area = 76.5
rudder_area = 232.0
elevator_up_limit = 30.0
elevator_down_limit = 30.0
aileron_up_limit = 30.0
aileron_down_limit = 15.0
rudder_limit = 25.0
elevator_trim_limit = 20.0
spoiler_limit = 60.0
aileron_to_spoileron_gain = 3
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 10
min_flaps_for_spoilerons = 0
spoilerons_available = 1

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[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=1.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 

[TurbineEngineData]
fuel_flow_gain=0.0010                          //Gain on fuel flow
inlet_area=93.840195                           //Square Feet, engine nacelle inlet area
rated_N2_rpm=11292                            //RPM, second stage compressor rated value
static_thrust=115540                        //GE90-115B 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 

[gear_warning_system]
gear_warning_available = 0    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  5.0     //Flap angle that activates warning at idle
flap_limit_power   = 25.5     //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.7  //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 1         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[Views]
eyepoint=111, -1.30, 4.25 

[Flaps.0]	//Inboard Krueger
type= 2
span-outboard= 0.100
extending-time= 15.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 275.000
lift_scalar= 0.0
drag_scalar= 0.0000
pitch_scalar= 0.0
flaps-position.0= 0.000, 0.000
flaps-position.1= 30.000, 265.000

[Flaps.1]	//Slat
type= 2
span-outboard= 0.800
extending-time= 15.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 275.000
lift_scalar= 0.02100
drag_scalar= 0.300
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.500, 265.000
flaps-position.2= 15.500, 245.000
flaps-position.3= 15.500, 230.000
flaps-position.4= 15.500, 225.000
flaps-position.5= 30.000, 200.000
flaps-position.6= 30.000, 180.000 

[Flaps.2]	//Inboard Flap
type= 1
span-outboard= 0.200
extending-time= 25.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 275.000
lift_scalar= 0.4750
drag_scalar= 0.250
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.1000, 265.000
flaps-position.2= 5.000, 245.000
flaps-position.3= 15.000, 230.000
flaps-position.4= 20.000, 225.000
flaps-position.5= 25.000, 200.000
flaps-position.6= 30.000, 180.000

[Flaps.3]	//Outboard Flap
type= 1
span-outboard= 0.600
extending-time= 25.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 275.000
lift_scalar= 0.4750
drag_scalar= 0.300
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.10, 265.000
flaps-position.2= 5.000, 245.000
flaps-position.3= 15.000, 230.000
flaps-position.4= 20.000, 225.000
flaps-position.5= 25.000, 200.000
flaps-position.6= 30.000, 180.000

[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, 1 
Adf.1=1,1 
Adf.2=1,1
Transponder.1=1 
Marker.1=1 

[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 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.1                               ;Percent per second

[Reference Speeds]
flaps_up_stall_speed=150.0                 //Knots True (KTAS)
full_flaps_stall_speed=120.0                 //Knots True (KTAS)
cruise_speed=482.0                 //Knots True (KTAS)
max_mach                = 0.90
max_indicated_speed     = 330                   //Red line (KIAS)

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800.0 
autothrottle_available=1 
autothrottle_arming_required= 1
autothrottle_max_rpm = 108.5
autothrottle_takeoff_ga= 1
pitch_takeoff_ga=8.000000
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=0.7
max_pitch_velocity_hi_alt=0.4
max_pitch_velocity_lo_alt_breakpoint=11000.0
max_pitch_velocity_hi_alt_breakpoint=25000.0
max_bank=25.0
max_bank_acceleration=1.4
max_bank_velocity=2.8
max_throttle_rate=0.08
nav_proportional_control=11.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=19.0
gs_integrator_control=0.530
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
