[fltsim.0]
title=Project Opensky -- Boeing 777-200ER VARIG PP-VRF
sim=777-200ER-PW4090
model=
panel=
sound=
texture=
checklists=
atc_airline=varig
atc_id=PP-VRF
atc_flight_number=860
atc_heavy=0
atc_parking_types=GATE, RAMP, CARGO
atc_parking_code=varig
ui_manufacturer=Project Opensky
ui_type=777-200ER
ui_variation=Varig
visual_damage=0
description=
[General]
performance=
atc_type=BOEING
atc_model=B772
editable=1
[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 5.000, 0.000, 0.000
max_number_of_stations =50
max_number_of_stations = 6
// New FS2004 Numbers
// Max Structural Payload Per Boeing - 96,557 lbs
// Max Structural Payload Opensky - 55,500 lbs
// Actual Total PAX - 43,050 lbs
station_load.0= "900, 0.0, 0.0, 0.0, 1st Class - 06 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1= "7350, 0.0, 0.0, 0.0, Bus Class - 49 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="34800, 0.0, 0.0, 0.0, Econ Class-232 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
// Total Opensky Cargo - 10,500 lbs
station_load.3 = "4500, 0.0, 0.0, 0.0, Lwr Dk Cgo Fwd" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "4500, 0.0, 0.0, 0.0, Lwr Dk Cgo Aft" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "1500, 0.0, 0.0, 0.0, Lwr Dk Cgo Bulk" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight= 299000.000
max_gross_weight= 649000.000
empty_weight_roll_MOI = 20500000.000
empty_weight_pitch_MOI= 33901309.500
empty_weight_yaw_MOI = 40000000.000
empty_weight_coupled_MOI= 1000.000
[flight_tuning]
cruise_lift_scalar = 1.00
parasite_drag_scalar = 0.75
induced_drag_scalar = 0.75
elevator_effectiveness = 1.00
aileron_effectiveness = 1.75
rudder_effectiveness = 1.50
pitch_stability = 1.00
roll_stability = 1.00
yaw_stability = 1.00
elevator_trim_effectiveness = 0.50
aileron_trim_effectiveness = 0.50
rudder_trim_effectiveness = 0.50
[pitot_static]
vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI
[fuel]
Center1= 0.0, 0.0, -4.0, 26620.0, 1.0
LeftMain= 4.000, -35.000, 0.000, 9300.000, 0.000
RightMain= 4.000, 35.000, 0.000, 9300.000, 0.000
fuel_type= 2.000
number_of_tank_selectors= 1
electric_pump=0
[airplane_geometry]
wing_area= 4605.000
wing_span= 199.917
wing_root_chord= 23.000
wing_dihedral= 6.218
wing_incidence= 1.000
wing_twist= -0.500
oswald_efficiency_factor= 0.600
wing_winglets_flag= 0
wing_sweep= 31.5
wing_pos_apex_lon= 35.000
wing_pos_apex_vert= 0.000
htail_area= 1090.000
htail_span= 70.700
htail_pos_lon= -84.5
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 40.000
vtail_area= 573.000
vtail_span= 27.300
vtail_sweep= 35.000
vtail_pos_lon= -92.583
vtail_pos_vert= 5.800
elevator_area= 137.000
aileron_area= 68.000
rudder_area= 232.000
elevator_up_limit= 24.000
elevator_down_limit= 18.000
aileron_up_limit= 24.000
aileron_down_limit= 18.000
rudder_limit= 32.000
elevator_trim_limit= 16.000
spoiler_limit= 45.000
spoilerons_available= 1
aileron_to_spoileron_gain = 1.000
min_ailerons_for_spoilerons = 7.000
min_flaps_for_spoilerons = 0
[GeneralEngineData]
engine_type= 1
Engine.0= 10.000, -32.583, -10.500
Engine.1= 10.000, 32.583, -10.500
fuel_flow_scalar= 0.6299348
min_throttle_limit= -0.38
[TurbineEngineData]
fuel_flow_gain = 0.002 //Gain on fuel flow
inlet_area = 92.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 90200 //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
[Reference Speeds]
flaps_up_stall_speed= 138.000
full_flaps_stall_speed= 110.400
cruise_speed= 485.00
max_indicated_speed=350.000000
max_mach=0.870020
[keyboard_response]
elevator= 100.000, 200.000
aileron= 100.000, 200.000
rudder= 100.000, 200.000
[Views]
eyepoint= 98.502, -1.756, 1.628
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1500.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=105.000000
pitch_takeoff_ga=8.000000
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=0.300000
max_pitch_velocity_lo_alt_breakpoint= 7000.000000
max_pitch_velocity_hi_alt_breakpoint=24000.000000
max_bank=30.000000
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=1.000000
[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
[flaps.0] //Inboard Trailing Edge
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.2 // 0.0 .. 1.0
extending-time = 30 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0 // degrees
flaps-position.2 = 5 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
//lift_scalar = 1.00
//drag_scalar = 1.00
//pitch_scalar= 1.00
//system_type = 1 //Hydraulic
lift_scalar = 0.55
drag_scalar = 0.55
pitch_scalar= 0.55
system_type = 1
[flaps.1] //Outboard Trailing Edge
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 30 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 5 // degrees
flaps-position.2 = 10 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
//lift_scalar = 0.50
//drag_scalar = 0.50
//pitch_scalar= 0.50
//system_type = 1 //Hydraulic
lift_scalar = 0.35
drag_scalar = 0.35
pitch_scalar= 0.35
system_type = 1
[flaps.2] //Inboard Leading Edge Slats
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 35 // seconds
//flaps-position.0 = 0 // degrees
//flaps-position.1 = 5 // degrees
//flaps-position.2 = 10 // degrees
//flaps-position.3 = 15 // degrees
//flaps-position.4 = 5 // degrees
//flaps-position.5 = 20 // degrees
//flaps-position.6 = 20 // degrees
flaps-position.0 = 0 // degrees
flaps-position.1 = 5 // degrees
flaps-position.2 = 10 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.50
drag_scalar = 0.50
pitch_scalar= 0.50
system_type = 1 //Hydraulic
[direction_indicators]
direction_indicator.0=3,0
[contact_points]
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
point.0=1.0, 82.250, 0.000, -16.433, 1181.102, 0.000, 5.505, 90.0, 1.80, 1.800, 1.0, 8.000, 9.000, 0.000, 0.000, 0.000
point.1=1.0, -6.667, -18.000, -17.417, 1574.803, 1.000, 5.505, 8.0, 0.980, 1.250, 1.0, 9.900, 11.900, 2.000, 0.000, 0.000
point.2=1.0, -6.667, 18.000, -17.417, 1574.803, 2.000, 5.505, 8.0, 0.980, 1.250, 1.0, 10.100, 13.100, 3.000, 0.000, 0.000
static_pitch=-0.104370
static_cg_height=16.620275
gear_system_type=0
[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
[brakes]
toe_brakes_scale=0.580
parking_brake=1
[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
[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
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
//light_panel = 0, 5 , 17.0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=Opensky_sparks, 1
touchdown=fx_tchdwn, 1
[TailHook] // For opening cargo door.
tailhook_length=1 ;(feet)
tailhook_position = 0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum
[folding_wings] // For opening main deck cargo door.
wing_fold_system_type = 4 ;0=None
fold_rates = 0.05,1.00 ;Percent per second
[exits]
number_of_exits = 4
exit_rate.0 = 0.18 ;Percent per second
exit_rate.1 = 0.05 ;Percent per second
exit_rate.2 = 0.18 ;Percent per second
exit_rate.3 = 0.18 ;Percent per second
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo
light.0 = 1, 28.600, 0.000, 12.700, Opensky_beacon ,
light.1 = 1, 4.800, 0.000, -8.700, Opensky_beacon ,
light.2 = 3, -112.000, 0.000, 4.500, fx_strobe.fx ,
light.3 = 3, -112.000, 0.000, 8.100, fx_navwhi ,
light.4 = 5, 32.700, -15.000, -2.000, Opensky_wing_light ,
light.5 = 5, 32.700, 15.000, -2.000, Opensky_wing_light ,
light.6 = 5, 20.700, -13.500, -2.000, Opensky_nav_yellow ,
light.7 = 5, 20.700, 13.500, -2.000, Opensky_nav_yellow ,
