[fltsim.2]
title=ARYUS BJ-III
sim=BJ-III_Goldenbird
model=
panel=
sound=
texture=ARYUS
kb_checklists=
kb_reference=
atc_id=N440AY
ui_manufacturer=Aryus Company
ui_type="BJ-III Goldenbird"
ui_variation="Aryus House 2"
description="Aryus BJ-III created by Alex Guedes. Aryus Company is an subdivision of Fullguns Military Industry"
[fltsim.0]
title=ARYUS BJ-III Luigi Maffei
sim=BJ-III_Goldenbird
model=
panel=
sound=
texture=Maffei
kb_checklists=
kb_reference=
atc_id=PP-MAF
ui_manufacturer=Aryus Company
ui_type="BJ-III Goldenbird"
ui_variation="Luigi Maffei"
description="Aryus BJ-III created by Alex Guedes. Aryus Company is an subdivision of Fullguns Military Industry"
[fltsim.1]
title=ARYUS BJ-III Blue
sim=BJ-III_Goldenbird
model=
panel=
sound=
texture=Aryus_Blue
kb_checklists=
kb_reference=
atc_id=PP-MFA
ui_manufacturer=Aryus Company
ui_type="BJ-III Goldenbird"
ui_variation="N729BJ"
description="Aryus BJ-III created by Alex Guedes. Aryus Company is an subdivision of Fullguns Military Industry"
[General]
atc_type=experimental
atc_model=experimental
editable=0
performance="Cruise Speed\n0.82 Mach 475 kts 880 km\/h\n\nEngine options\nBMW Rolls & Royce BR710 14750lbs\n\nMaximum Range\n7,000 nm 13,000 km\n\nMaximum Certified Operating Altitude 51,100 ft 15,544 m\n\nFuel Capacity\n5,720 gal 21,650 L\n\nBasic Empty Weight\n41,150 lb 18,665 kg\n\nMax Gross Weight 82,230 lb 37,300kg\n\nLength\n92 ft, 48 in 28.19 m\n\nWingspan\n78 ft, 74 in 24.00 m\n\nHeight\n23 ft, 29 in 7.1 m\n\nSeating Typical Long Range configuration - 6+4 crew\nTypical configuration - 14+2 crew
[WEIGHT_AND_BALANCE]
max_gross_weight = 82230 // (pounds)
empty_weight = 41150 // (pounds)
reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "1970, 0.0, 0.0, 0.0, Max 2180kg" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 221967
empty_weight_roll_MOI = 41681
empty_weight_yaw_MOI = 157094
empty_weight_coupled_MOI = 0
[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
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -24.6, -6.6, 2.5 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -24.6, 6.6, 2.5 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.3567 //Scalar for fuel flow efficiency
min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.002 //Gain on fuel flow
inlet_area = 16.81 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 14000 //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
[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, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 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
//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)
[contact_points]
point.0=1, 34.00, 0.00, -8.36, 1181.1, 0, 0.942, 78.92, 0.3000, 2.5, 0.3100, 10.0, 10.0, 0, 260.0, 260.0
point.1=1, -3.9, -5.9, -9.72, 1574.8, 1, 1.342, 0.00, 0.7798, 2.5, 0.5456, 9.0, 9.0, 2, 260.0, 260.0
point.2=1, -3.9, 5.9, -9.72, 1574.8, 2, 1.342, 0.00, 0.7798, 2.5, 0.5456, 9.0, 9.0, 3, 260.0, 260.0
point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -44.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
max_number_of_points = 21
static_pitch = -0.9 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height = 9.0 //feet, altitude of CG when at rest on the ground
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 1 //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 = 25.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.67 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint= 34.3, -1.41, 2.0 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.7 // 0.0 .. 1.0
extending-time = 10 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 8 // degrees
flaps-position.2 = 20 // degrees // KIAS
flaps-position.3 = 40 // degrees
blowout-speed = 300 // KIAS
lift_scalar = 0.67
drag_scalar = 0.97
pitch_scalar= 0.67
system_type = 1 //Hydraulic
[flaps.1] //Outboard Leading Edge Slat
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.4 // 0.0 .. 1.0
extending-time = 6 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 1.5 // //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.67
drag_scalar = 0.97
pitch_scalar= 0.67
system_type = 1 //Hydraulic
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
Center1 = 0, 0, 0, 1480, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -3, -19, 0, 2120, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3, 19, 0, 2120, 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 = 930.0 //Square feet
wing_span = 78.74 //Feet
wing_root_chord = 11.87 //Feet
wing_dihedral = 3.0 //Degrees
wing_incidence = 2.0 //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 = 32.1 //Degrees, wing leading edge
wing_pos_apex_lon = 13.88 //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 = 210.0 //Square feet
htail_span = 28.4 //Feet
htail_pos_lon = -41.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 12.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 30.0 //Degrees, horizontal tail leading edge
vtail_area = 118.0 //Square feet
vtail_span = 11.8 //Feet, tip to body
vtail_sweep = 45.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -35.8 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 3.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 78.0 //Square feet
aileron_area = 38.0 //Square feet
rudder_area = 45.3 //Square feet
elevator_up_limit = 26.0 //Degrees
elevator_down_limit = 26.0 //Degrees
aileron_up_limit = 22.0 //Degrees
aileron_down_limit = 20.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 20.0 //Degrees
spoiler_limit = 60.0 //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
[Reference Speeds]
flaps_up_stall_speed = 132.0 //Knots True (KTAS)
full_flaps_stall_speed = 103.6 //Knots True (KTAS)
cruise_speed = 467.7 //Knots True (KTAS)
max_mach = 0.90
max_indicated_speed = 370 //Red line (KIAS)
[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= 150.0, 250.0
aileron= 150.0, 250.0
rudder= 150.0, 250.0
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 1
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
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=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[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
[stall_warning]
type=2
[direction_indicators]
direction_indicator.0=3,0
