[fltsim.0]
title=A320 LanChile
sim=fsp_a320
model=V25
panel=
sound=
texture=LAN
kb_checklists=
kb_reference=
atc_id=CC-COF
atc_id_color=0xffffffff
atc_airline=LAN CHILE
atc_flight_number=421
ui_manufacturer=LAN CHILE
ui_type=Airbus A320
ui_variation=Lan Chile
description=For AI aircraft
TBAirCraftUId=297
[General]
atc_type=Airbus
atc_model=A321
editable=1
performance=Cruise Speed\t.74 Mach\nMaximum Range\t2,059 nm\nService Ceiling\t36,089 ft\nMax Takeoff Weight\t138,500 lb\nSeating\t\t147 to 168\nCargo Capacity\t1,373 CU ft\n
TBAirCraftFolderUId=58
[WEIGHT_AND_BALANCE]
max_gross_weight = 160000 // (pounds)
empty_weight = 79686 // (pounds)
reference_datum_position = 77.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -74.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 33000, -69.5, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 1651967
empty_weight_roll_MOI = 465681
empty_weight_yaw_MOI = 1447094
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 = -103.6, -8.5, 0.6 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -103.6, 8.5, 0.6 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
[TurbineEngineData]
fuel_flow_gain = 0.002 //Gain on fuel flow
inlet_area = 10.4 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 21000 //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, 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
//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, -9.20, 0.00, -8.3, 1500, 0, 1.08, 25.0, 1.00, 2.5, 0.9, 7.0, 5.0, 0
point.1 = 1, -83.10, -8.33, -9.8, 3000, 1, 1.85, 0.0, 1.50, 2.5, 0.8, 7.0, 7.0, 2
point.2 = 1, -83.10, 8.33, -9.8, 3000, 2, 1.85, 0.0, 1.50, 2.5, 0.8, 7.0, 7.0, 3
point.3 = 2, -95.75, -53.92, -1.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -98.75, 53.92, -1.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6
point.5 = 2, -139.00, 0.00, 3.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9
point.6 = 2, -3.00, 0.00, 0.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4
max_number_of_points = 21
static_pitch = -0.3 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height = 8.0 //feet, altitude of CG when at rest on the ground
[Views]
eyepoint= -13.3, -1.82, 5.0 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.1] //Outboard Trailing Edge
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 23 // 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 = 0.35
drag_scalar = 0.35
pitch_scalar= 0.35
system_type = 1 //Hydraulic
[flaps.2] //Inboard Leading Edge Slats
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 4 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0.5 // degrees
flaps-position.2 = 0.5 // degrees
flaps-position.3 = 0.5 // degrees
flaps-position.4 = 0.5 // degrees
flaps-position.5 = 1.0 // degrees
flaps-position.6 = 1.0 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.05
drag_scalar = 0.05
pitch_scalar= 0.05
system_type = 1 //Hydraulic
[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
light.0 = 3, -86.00, 55.0, 6.10, fx_navgrem ,
light.1 = 3, -86.00, -55.0, 6.10, fx_navredm ,
light.2 = 2, -86.50, -56.0, 6.10, fx_strobeh ,
light.3 = 2, -86.50, 56.0, 6.10, fx_strobeh ,
light.4 = 1, -38.00, 0.00, 12.0, fx_beaconb ,
light.5 = 1, -72.00, 0.00, -2.60, fx_beaconb
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
Center1 = -76.2, 0.0, -6.0, 580.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = -78.2, 0.0, -6.0, 580.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -78.7, -12.1, -4.0, 2920.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -78.7, 12.1, -4.0, 2920.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[airplane_geometry]
wing_area = 1209.0 //Square feet
wing_span = 107.8 //Feet
wing_root_chord = 23.1 //Feet
wing_dihedral = 3.0 //Degrees
wing_incidence = 1.3 //Degrees
wing_twist = 0.0 //Degrees
oswald_efficiency_factor= 0.8 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 24.5 //Degrees, wing leading edge
wing_pos_apex_lon = -61.0 //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 = 341.0 //Square feet
htail_span = 40.0 //Feet
htail_pos_lon = -134.0 //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 = 30.0 //Degrees, horizontal tail leading edge
vtail_area = 168.0 //Square feet
vtail_span = 14.8 //Feet, tip to body
vtail_sweep = 25.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -131.8 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 10.9 //Feet, vertical distance from reference point, positive going up
elevator_area = 145.0 //Square feet
aileron_area = 38.0 //Square feet
rudder_area = 65.3 //Square feet
elevator_up_limit = 26.0 //Degrees
elevator_down_limit = 26.0 //Degrees
aileron_up_limit = 30.0 //Degrees
aileron_down_limit = 30.0 //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 = 142.0 //Knots True (KTAS)
full_flaps_stall_speed = 113.6 //Knots True (KTAS)
cruise_speed = 437.7 //Knots True (KTAS)
[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
use_no_default_pitch=1
use_no_default_bank=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
[direction_indicators]
direction_indicator.0=3,0
