[fltsim.0]
title = A380-800
sim = airbus
model=
panel =
sound =
texture =
atc_id =
atc_airline = "Airbus"
atc_heavy = 1
atc_flight_number =
ui_manufacturer = "Airbus"
ui_type = "A380 British Airways"
ui_variation = "livery"
ui_typerole = "Commercial Airliner"
ui_createdby = "Dunken Avionics"
description = The Airbus A380-800 is the largest most advanced passenger airliner built to date."Cruise Speed\n0.85 Mach/565 mph910 km\/h\n\nEngine options\nPratt & Whitney PW4062\nRolls-Royce RB211-524H\nGeneral Electric CF6-80C2B5F\n\nMaximum Range\n9,325 nm currently only a dozen of the A380-800s are flying. The wait list is sure to keep airbus profiting from this giant for years to come.
[CameraDefinition.0]
Title = "Right Side Window"
Guid = {54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC}
Description = View of the right wing from the passenger cabin economy
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 5.5, 5, 5
InitialPbh = 0, 0, 95
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Left Side Window"
Guid = {0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description = View of the left wing from the passenger cabin economy
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -5.5, 5, 5
InitialPbh = 0, 0, 265
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.2]
Title = "Landing Gear"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the landing gear and left wing inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .32
ShowWeather = Yes
InitialXyz = 0, -5, -15
InitialPbh = 0, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.3]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0, 9.0, -25.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.4]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 40.8, 1.4, 4.0
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.5]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -40.8, 1.4, 4.0
InitialPbh = 6, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
[CameraDefinition.001]
Title = "Right Seat"
Guid = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.25, 0.0, 0.0
InitialPbh=0, 0, 0
[CameraDefinition.002]
Title = "Radio Stack"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.6, 0.30, -0.05
InitialPbh=85, 0, 0
[CameraDefinition.003]
Title = "Overhead Panel"
Guid = {4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.8
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.635, -0.58, -0.2
InitialPbh=-55.0, 0, 0
[CameraDefinition.004]
Title = "Engine Controls"
Guid = {195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.6, 0.3, 0
InitialPbh=59.5, 0, 0
[General]
atc_type = "Airbus"
atc_model = "A380 British Airways"
editable = 1
performance = "Cruise Speed\n0.85 Mach 650 mph 1215 km\/h\n\nEngine options\nPratt & Whitney PW4062\nRolls-Royce RB328-585H\nGeneral Electric CF6-83C2B5F\n\nMaximum Range\n8,685 nm
Category = Airplane
[pitot_static]
vertical_speed_time_constant = 5 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.00 //Scalar on heat effectiveness, 0 = not available
[WEIGHT_AND_BALANCE]
max_gross_weight = 1235000 // (pounds)
empty_weight = 610700 // (pounds)
reference_datum_position = 0.0, 0, 0 // 40.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -4, 0, 0 //-43.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170.0, 77.0, -2.0, 16.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170.0, 77.0, 2.0, 16.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 =1700.0, -83.5, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 2000, 40.0, 0.0, 8.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 33068, 35.0, 0.0, 6.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 45469, -6.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 74647, 30.0, 0.0, -6.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = 54012, -25.0, 0.0, -6.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = 15000, 0.0, 0.0, -6.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_name.1 = "Co-Pilot"
station_name.2 = "Crew"
station_name.3 = "First Class"
station_name.4 = "Business Class"
station_name.5 = "Upper Deck"
station_name.6 = "Coach 1-7"
station_name.7 = "Forward Baggage"
station_name.8 = "Aft Baggage"
;Moments of Inertia
empty_weight_roll_MOI = 13352310
empty_weight_pitch_MOI = 23123159
empty_weight_yaw_MOI = 38531785
empty_weight_coupled_MOI = 0
[fuel]
LeftMain = 1.0,-14.0, 0.0, 14000.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 1.0, 14.0, 0.0, 14000.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = -8.0,-26.0, 0.0, 9000.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = -8.0, 26.0, 0.0, 9000.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 = 3.0, 0.0, 0.0, 33500.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = -5.0, 0.0, 0.0, 13000.0, 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 = 3
fuel_dump_rate = 0.65 //Percent of max quantity per second, i.e. about 1 minute for full fuel
electric_pump = 1
[airplane_geometry]
wing_area = 9100.0 //Square feet
wing_span = 261.8 //Feet
wing_root_chord = 58.8 //Feet
wing_dihedral = 5.0 //Degrees
wing_incidence = 2.0 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 0.68 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 33.5 //Degrees, wing leading edge
wing_pos_apex_lon = 37 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0 //Feet, vertical distance from reference point, positive going up
htail_area = 1470 //Square feet
htail_span = 72.8 //Feet
htail_pos_lon = -210.0 //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 = 0.0 //Degrees
htail_sweep = 37.5 //Degrees, horizontal tail leading edge
vtail_area = 1060 //Square feet
vtail_span = 37.1 //Feet, tip to body
vtail_sweep = 45.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -198.5 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 26.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 327 //Square feet
aileron_area = 225 //Square feet
rudder_area = 230 //Square feet
elevator_up_limit = 30 //Degrees
elevator_down_limit = 20 //Degrees
aileron_up_limit = 25 //Degrees
aileron_down_limit = 19 //Degrees
rudder_limit = 45.0 //Degrees
elevator_trim_limit = 20 //Degrees
spoiler_limit = 45 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 3 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=8.000000
positive_g_limit_flaps_down=8.000000
negative_g_limit_flaps_up=-8.000000
negative_g_limit_flaps_down=-8.000000
[Reference Speeds]
flaps_up_stall_speed = 165.0 //Knots True (KTAS)
full_flaps_stall_speed = 138.0 //Knots True (KTAS)
cruise_speed =1955.0 //Knots True (KTAS)
max_mach = 3.88
max_indicated_speed =2960.0 //Red line (KIAS)
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 28 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0 // degrees
flaps-position.2 = 10 // degrees
flaps-position.3 = 20 // degrees
flaps-position.4 = 30 // degrees
flaps-position.5 = 40 // degrees
damaging-speed = 350 // KIAS
blowout-speed = 400 // KIAS
lift_scalar = 0.3
drag_scalar = 1.0
pitch_scalar= 0
system_type = 1 //Hydraulic
[flaps.1]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 8 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 2.0 // degrees
flaps-position.2 = 2.0 // degrees
flaps-position.3 = 3.5 // degrees
flaps-position.4 = 3.5 // degrees
flaps-position.5 = 5.0 // degrees
damaging-speed = 350 // KIAS
blowout-speed = 400 // KIAS
lift_scalar = 2.0
drag_scalar = 0.1
pitch_scalar= 0
system_type = 1 //Hydraulic
[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
[flight_tuning]
cruise_lift_scalar = 3.0
parasite_drag_scalar = 0.5
induced_drag_scalar = 0.5
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
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 =-24.0, -83.0, -2.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 0.0, -43.0, -2.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = 0.0, 43.0, -2.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3 =-24.0, 83.0, -2.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.28; //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature = -40 //Temp at which contrail is formed outside
[TurbineEngineData]
fuel_flow_gain = 0.006 //Gain on fuel flow
inlet_area = 61.1 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29950.50 //RPM, second stage compressor rated value
static_thrust = 71250.75 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
ThrustSpecificFuelConsumption = 0.40
[jet_engine]
thrust_scalar = 1.0
[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 1500.0
autothrottle_available = 1
autothrottle_arming_required = 1
autothrottle_max_rpm = 125.0
autothrottle_takeoff_ga = 1
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=0.13
max_pitch_velocity_hi_alt=0.12
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=125.05
nav_proportional_control=16.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control = 18.0
gs_integrator_control = 0.33
gs_derivative_control = 0.00
gs_integrator_boundary = 0.70
gs_derivative_boundary = 0.00
yaw_damper_gain = 1.0
[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, -25.0, 0.0, -17.2, 3200, 0, 2.0, 70.0, 0.5, 3.5, 0.900, 9.0, 8.0, 0, 225, 250
;point.1 = 1, -114.0, -18.0, -20.0, 3200, 1, 2.0, 13.0, 3.0, 2.5, 0.900, 11.0, 9.0, 2, 225, 250
;point.2 = 1, -114.0, 18.0, -20.0, 3200, 2, 2.0, 13.0, 3.0, 2.5, 0.900, 11.0, 9.0, 3, 225, 250
;point.3 = 2, -152.6, -103.5, 3.0, 3200, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 225, 250
;point.4 = 2, -152.6, 103.5, 3.0, 3200, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 225, 250
;point.5 = 2, 3.0, 0.0, 0.0, 3200, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 225, 250
;point.6 = 2, -222.7, 0.0, 4.0, 3200, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 225, 250
point.0= 1, 71.0, 0.00, -11.30, 8200.0, 0, 1.96, 66, 0.84, 3.4, 0.4, 7.00, 8.00, 0, 225.0, 250.0 //Nosewheel
point.1= 1, -13.00, -19.10, -11.30, 8200.0, 2, 1.94, 0.0, 3.00, 2.2, 0.8, 7.70, 7.40, 2, 225.0, 250.0 //Forward Outer Left Main
point.2= 1, -13.00, 19.50, -11.30, 8200.0, 2, 1.94, 0.0, 3.00, 2.2, 0.8, 7.40, 7.80, 2, 225.0, 250.0 //Forward Outer Right Main
point.3= 1, -25.00, -8.50, -11.60, 8200.0, 2, 1.94, 0.0, 2.30, 1.7, 0.8, 7.70, 7.40, 2, 225.0, 250.0 //Rear Inner Left Main
point.4= 1, -25.00, 8.70, -11.60, 8200.0, 2, 1.94, 0.0, 2.30, 1.7, 0.8, 7.40, 7.80, 2, 225.0, 250.0 //Rear Inner Right Main
;point.0= 1, 62.0, -10.00, -35.40, 8200.0, 0, 1.96, 60.0, 0.80, 2.5, 0.7, 7.00, 8.00, 0, 225.0, 250.0 //contact_cgear
;point.1= 1, -24.30, -24.56, -36.80, 8200.0, 1, 1.94, 0.0, 1.00, 2.5, 0.8, 7.70, 7.40, 2, 225.0, 250.0 //contact_lgear01
;point.2= 1, -24.30, 24.56, -36.80, 8200.0, 2, 1.94, 0.0, 1.00, 2.5, 0.8, 7.40, 7.80, 2, 225.0, 250.0 //contact_rgear01
;point.3= 1, -58.30, -15.56, -36.80, 3200.0, 1, 1.94, 0.0, 1.00, 1.5, 0.8, 8.00, 8.00, 2, 225.0, 250.0 //contact_lgear02
;point.4= 1, -58.30, 15.56, -36.80, 3200.0, 2, 1.94, 20.0, 1.00, 1.5, 0.8, 7.60, 7.50, 2, 225.0, 250.0 //contact_rgear02
;point.5= 1, -33.30, 0.00, -36.80, 3200.0, 0, 1.94, 20.0, 1.00, 1.5, 0.8, 7.60, 7.50, 2, 225.0, 250.0 //contact_midgear
;point.6= 2, -128.0, -5.59, 8.67, 3200.0, 0, 2.27, 0.0, 0.82, 2.5, 0.8, 0.0, 0.0, 4, 225.0, 250.0 //contact_scrape_tail
;point.7= 2, -66.2, -119.9, 3.27, 3200.0, 0, 4.89, 0.0, 0.82, 2.5, 0.8, 0.0, 0.0, 5, 225.0, 250.0 //contact_scrape_leftwing
;point.8= 2, -66.2, 118.0, 3.27, 3200.0, 0, 4.82, 0.0, 0.82, 2.5, 0.8, 0.0, 0.0, 6, 225.0, 250.0 //contact_scrape_rightwing
static_pitch = 0.2
gear_system_type=1 //Hydraulic
static_cg_height = 11.81
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 20.0 //Flap angle that activates warning at idle
flap_limit_power = 25.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.24 //Brake scalar
differential_braking_scale= 1.45 //Differential Brake scalar
auto_brakes = 4
hydraulic_system_scalar = 1 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,1,1 //pumps on Eng1,2,3,4
[electrical]
max_battery_voltage = 28.5
generator_alternator_voltage = 28.5
max_generator_alternator_amps = 850.0
engine_generator_map = 1,1,1,1
electric_always_available = 0
flap_motor = 0, 300, 21
gear_motor = 0, 610, 21
autopilot = 1, 6, 21
avionics_bus = 0, 75, 21
avionics = 1, 65, 21
pitot_heat = 0, 20, 21
additional_system = 0, 110, 3
marker_beacon = 0, 10, 21
gear_warning = 0, 10, 21
fuel_pump = 0, 20, 20
starter1 = 0, 150, 21
starter2 = 0, 150, 21
starter3 = 0, 150, 21
starter4 = 0, 150, 21
light_nav = 0, 10, 19
light_beacon = 0, 10, 19
light_landing = 0, 20, 19
light_taxi = 0, 20, 19
light_strobe = 0, 20, 21
light_panel = 2, 15, 21
standby_vacuum = 0, 15, 21
hydraulic_pump = 0, 110, 21
fuel_transfer_pump = 0, 30, 21
light_recognition = 0, 20, 19
light_wing = 0, 20, 19
light_logo = 0, 20, 19
light_cabin = 0, 30, 19
[Auxiliary Power Unit]
available = 1
[forcefeedback]
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 = 35500 ; 0 - 35999 degrees
gear_bump_left_duration = 250000 ; in microseconds
gear_bump_right_magnitude = 2700 ; 0 - 10000
gear_bump_right_direction = 00500 ; 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
[LIGHTS]
light.0 = 2, -1.0, 0.0, 26.0, fx_f20_strobe //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1 = 1, -1.0, 0.0, 26.0, fx_f20_beacon //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.2 = 2, -30.0, 0.0, -3.8, fx_f20_strobe //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.3 = 1, -30.0, 0.0, -3.8, fx_f20_beacon //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.4 = 4, 66.0, 1.7, 10.0, fx_f20_vclight_red //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.5 = 4, 66.0, -1.7, 10.0, fx_f20_vclight_red //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.6 = 4, 62.0, 0, 11.0, fx_f20_vclight_red //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.7 = 8, 18.5, 48.6, 0, fx_vclighth //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.8 = 8, 18.5, -48.0, 0, fx_vclighth //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.9 = 8, -7.0, 82.0, 1, fx_vclighth //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.10= 8, -7.0, -82.0, 1, fx_vclighth //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
[Views]
eyepoint = 65.0, -2.0, 10.5 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
[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
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[Pressurization]
design_cabin_pressure = 10.9 ;PSI (~8000 feet)
max_pressure_differential = 4.96 ;PSI
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[vacuum_system]
//Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
max_pressure=5.150000
vacuum_type=2
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[keyboard_response]
elevator = 150, 250 //Breakpoint speeds (knots) on the keyboard increments of control surfaces.
aileron = 150, 250 //Breakpoint speeds (knots) on the keyboard increments of control surfaces.
rudder = 150, 250 //Breakpoint speeds (knots) on the keyboard increments of control surfaces.
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_dsb_heat
touchdown=fx_tchdwn, 1
windshield_rain_effect_available = 1
[GPWS]
max_warning_height = 0
sink_rate_fpm = -99999.0
excessive_sink_rate_fpm = -99999.0
climbout_sink_rate_fpm = -99999.0
flap_and_gear_sink_rate_fpm= -99999.0
[VoiceAlerts]
LowFuelPct = 0.1, -1, 5 //Low Fuel limit (percent), Check BELOW, Check every 60 seconds
OverGLimit = 6.0, 1, 1 //High G limit, Check ABOVE, Check every 1 seconds
[exits]
number_of_exits = 3
exit.0 = 0.4, 75, -9.5, 16, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1 = 0.4, 70, 8.0, -7, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.2 = 0.4, -42.30, 9.0, -7, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
[stall_warning]
type=2
stick_shaker=1
[deice_system]
structural_deice_type=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots