[General]
atc_type=Airbus
atc_model=A340
editable=0
performance=Cruise Speed        \nMach 0.83         555 mph         883 kmh\n\nEngine options        \nP&W 4000\nRR Trent 800\nGE 90 series\n\nMaximum Range              \n8,500 nm          6,859 sm        15,742 km\n\nService Ceiling    \n42,000 ft           12,800 m\n\nFuel Capacity       \n45,220 U.S. gal        171,160 L \n\nMaximum Takeoff Weight     \n804,675 lb        365,000 kg\n\nLength    \n247 ft, 0 in         73.9 m\n\nWingspan      \n208 ft, 11 in          63.7 m\n\nHeight        \n58 ft, 5 in           17.8 m\n\nSeating       \nSeats 316 \n\n
[WEIGHT_AND_BALANCE]
max_gross_weight=804675                       // (pounds)
empty_weight=390220                           // (pounds)
reference_datum_position=0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
;Moments of Inertia
empty_weight_pitch_MOI   = 24223159
empty_weight_roll_MOI    = 13352310
empty_weight_yaw_MOI     = 39531785
empty_weight_coupled_MOI=0.0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=0.6
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=2.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=0.8
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=20.5, -75.5, -6.9
Engine.1=10.5, -38.6, -8.4                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2=10.5,  38.6, -8.4                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3=20.5,  75.5, -6.9
fuel_flow_scalar=1                            //Scalar for fuel flow efficiency
min_throttle_limit=-0.250000
[TurbineEngineData]
fuel_flow_gain=0.002                          //Gain on fuel flow
inlet_area=138.0                              //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                            //RPM, second stage compressor rated value
static_thrust=56000                           //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,  87.42,   0.00, -16.10, 1581.1, 0, 4.521, 50.0, 0.63, 2.5, 0.7235, 4.0, 4.0, 0, 0.0, 0.0
point.1=1, -19.50, -12.00, -16.70, 2574.8, 1, 4.521,  0.0, 1.21, 2.5, 0.5470, 6.9, 6.9, 2, 0.0, 0.0
point.2=1, -19.50,  12.00, -16.70, 2574.8, 2, 4.521,  0.0, 1.21, 2.5, 0.5470, 7.1, 7.1, 3, 0.0, 0.0
point.3=2, -14.17, -47.33,   0.00,  787.4, 0, 0.000,  0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -14.17,  47.33,   0.00,  787.4, 0, 0.000,  0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -83.33,   0.00,   2.50,  787.4, 0, 0.000,  0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2,  42.67,   0.00,  -3.75,  787.4, 0, 0.000,  0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch=-0.10
static_cg_height=15.56
gear_system_type=0
[Views]
eyepoint=90.0, -2.65, 8.6
[flaps.0]      //Inboard Trailing Edge
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.2                                  // 0.0 .. 1.0
extending-time=25                                   // 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=0.55
drag_scalar=0.55
pitch_scalar=0.55
system_type=1                                         //Hydraulic
[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
[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
[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
[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
[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.8=1,  3.00,   0.00, -10.40, fx_beaconb ,
light.11=1,  63.00,   0.00, 9.90, fx_beaconh ,
light.9=1,  3.00,   0.00, -10.40, fx_beaconb ,
light.10=1,  63.00,   0.00, 9.90, fx_beaconh ,
[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=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second
[fuel]
Center1=0.0,   0.0, -4.0, 12400.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=-7.0, -35.0,  0.0, 16400.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-7.0,  35.0,  0.0, 16400.0, 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                    
electric_pump=0
[airplane_geometry]
wing_area=4704.0                //Square feet
wing_span=208.1                 //Feet
wing_root_chord=43.0                  //Feet
wing_dihedral=6.2                   //Degrees
wing_incidence=1.0                   //Degrees
wing_twist=-0.5                  //Degrees
oswald_efficiency_factor=0.65                  //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=32.0                  //Degrees, wing leading edge
wing_pos_apex_lon=25.0                  //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=1090.0                //Square feet
htail_span=70.7                  //Feet
htail_pos_lon=-100.0                //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=40.0                  //Degrees, horizontal tail leading edge
vtail_area=573.0                 //Square feet
vtail_span=27.3                  //Feet, tip to body
vtail_sweep=35.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-108.3                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=5.8                   //Feet, vertical distance from reference point, positive going up
elevator_area=137.0                 //Square feet
aileron_area=68.0                  //Square feet
rudder_area=232.0                 //Square feet
elevator_up_limit=20.0                  //Degrees
elevator_down_limit=25.0                  //Degrees
aileron_up_limit=30.0                  //Degrees
aileron_down_limit=15.0                  //Degrees
rudder_limit=25.0                  //Degrees
elevator_trim_limit=20.0                  //Degrees
spoiler_limit=60.0                  //Degrees
spoilerons_available=0                     //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=150.0                 //Knots True (KTAS)
full_flaps_stall_speed=120.0                 //Knots True (KTAS)
cruise_speed=400.0                 //Knots True (KTAS)
max_indicated_speed=430.000000
max_mach=0.900000
[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=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
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=0.000000
[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
[brakes]
toe_brakes_scale=0.466222
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0


[fltsim.0]
title=South African Airways Airbus A340-600
sim=A340-600
model=
sound=
texture=5
atc_airline=South African
atc_flight_number=346
atc_heavy=1
ui_manufacturer=Active Korea FS Traffic
ui_type="Airbus 346"
ui_variation=South African Airways
description=AI Aircraft FSP Airbus A340-600 for FS2004
