[fltsim.0]
title=MST A381 KAL
sim=a380
model=
panel=
sound=
texture=kal
kb_checklists=
kb_reference=
atc_id=HL9001
atc_airline=KOREAN AIR
atc_flight_number=003
atc_heavy=1
ui_manufacturer=Airbus
ui_type=A380-100 (Mike Stone)
ui_variation=Korean Air
description=Airbus A380
[General]
atc_type=AIRBUS
atc_model=A380
editable=1
performance=x
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
max_gross_weight = 1235000.000
empty_weight = 608400.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations = 50
;Moments of Inertia
empty_weight_roll_MOI = 33000000.000
empty_weight_pitch_MOI = 150000000.000
empty_weight_yaw_MOI = 99000000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[fuel]
LeftMain = 0.000, -30.000, -3.000, 24000.000, 0.000
RightMain = 0.000, 30.000, -3.000, 24000.000, 0.000
Center1 = 0.000, 0.000, -5.000, 34000.000, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 9100.000
wing_span = 261.000
wing_root_chord = 54.000
wing_dihedral = 5.000
wing_incidence = 1.000
wing_twist = -1.000
oswald_efficiency_factor= 0.700
wing_winglets_flag = 1
wing_sweep = 33.500
wing_pos_apex_lon = 40.000
wing_pos_apex_vert = 0.000
htail_area = 1974.000
htail_span = 104.000
htail_pos_lon = -120.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 33.500
vtail_area = 1350.000
vtail_span = 35.000
vtail_sweep = 45.000
vtail_pos_lon = -110.000
vtail_pos_vert = 20.000
elevator_area = 300.000
aileron_area = 200.000
rudder_area = 350.000
elevator_up_limit = 25.000
elevator_down_limit = 15.000
aileron_up_limit = 25.000
aileron_down_limit = 15.000
rudder_limit = 30.000
elevator_trim_limit = 20.000
spoiler_limit = 45.000
spoilerons_available = 1
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 140.000
full_flaps_stall_speed = 110.000
cruise_speed = 550.000
max_mach = 0.89
max_indicated_speed = 450.0 //Red line (KIAS)
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.508
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 1
Engine.0 = -10.000, -83.000, 0.000
Engine.1 = 17.000, -49.000, 0.000
Engine.2 = 17.000, 49.000, 0.000
Engine.3 = -10.000, 83.000, 0.000
fuel_flow_scalar = 1.000
min_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 80.000
rated_N2_rpm = 29920.000
static_thrust = 77770.000
afterburner_available = 0
reverser_available = 1.000
[jet_engine]
thrust_scalar =1.000
[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=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 = 1.000, 75.000, 0.000, -16.400, 1000.000, 0.000, 2.000, 70.000, 0.500, 3.500, 0.900, 7.000, 7.000, 0.000, 220.000, 250.000
point.1 = 1.000, -10.000, -20.000, -19.200, 2000.000, 1.000, 2.000, 13.000, 3.000, 2.500, 0.900, 8.000, 8.000, 2.000, 220.000, 250.000
point.2 = 1.000, -10.000, 20.000, -19.200, 2000.000, 2.000, 2.000, 13.000, 3.000, 2.500, 0.900, 8.200, 8.200, 3.000, 220.000, 250.000
point.3 = 2.000, -69.100, -103.500, 3.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4 = 2.000, -69.100, 103.500, 3.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5 = 2.000, 86.500, 0.000, 0.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6 = 2.000, -139.200, 0.000, 4.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 0.000
static_cg_height = 18.000
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 = 25.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.24 //Brake scalar
[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
[Views]
eyepoint = 87.43, -2.03, 5.75 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 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
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -65.92, -131.01, 8.47, fx_navredh ,
light.1 = 3, -65.92, 131.01, 8.47, fx_navgreh ,
light.2 = 3, -143.90, 0.00, 13.39, fx_navwhih ,
light.3 = 2, -65.82, -131.01, 8.47, fx_strobeh ,
light.4 = 2, -65.82, 131.01, 8.47, fx_strobeh ,
light.5 = 2, -143.90, 0.00, 13.49, fx_strobeh ,
light.6 = 1, 27.87, 0.00, 19.62, fx_beaconh ,
light.7 = 1, 1.65, 0.00, -10.57, fx_beaconh ,
light.8 = 4, 87.09, 0.00, 6.57, fx_vclighth,
[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=0,0
[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, 250
aileron = 150, 250
rudder = 150, 250
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[exits]
number_of_exits=2
exit_rate.0=0.8 //opens using shift+e and part name passenger_door
exit_rate.1=0.4 //opens using shift+e+2 and part name cargo_door
[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
[Flaps.0]
type= 1
span-outboard= 0.700
extending-time= 10.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 250.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 20.000, 0.000
flaps-position.4= 30.000, 0.000
flaps-position.5= 40.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 2.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.300
drag_scalar= 0.100
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
