[fltsim.0]
title=Project Opensky - Airbus A340-313E1 SAS VC
sim=A340-313E-GE-CFM56-5C4
model=VC
panel=
sound=
texture=SAS
checklists=

atc_airline=SCANDINAVIAN
atc_id=LN-RKF
atc_flight_number=1
atc_heavy=1
atc_parking_types=GATE, RAMP, CARGO
atc_parking_code=SAS

ui_manufacturer=Аэробус
ui_type=A340-300
ui_variation=Скандинавиан
visual_damage=1
description=Дальнемагистральный пассажирский самолет, разработанный западноевропейским консорциумом Airbus. Самолет принадлежит семейству дальнемагистральных самолетов А330/340. А340-300 четырехдвигательный пассажирский самолет большой дальности, оборудованный турбовентиляторными двигателями CFM International CFM56-5C. Самолет является дальнейшим развитием А340-200, с увеличенной пасажировместимостью. Самолет может перевозить 295 человек в трехклассной конфигурации на расстояние 7300 морских миль (13520 километров). 


[CameraDefinition.0]
Title=Окно справа
Guid={54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC}
Description=Вид на правое крыло из пассажирской кабины
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.0
ShowWeather=Yes
InitialXyz=5.5, 0.75, -13
InitialPbh=0, 0, 95
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000

max_number_of_stations= 8

station_load.0 =  "210.0,  60.0,  0.0,	 4.0, First Class     (12 pax)"       //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.1 =  "73.0,  40.0,  0.0,	 4.0, Business Class  (42 pax)"       //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2 = "421.0,   0.0,  0.0,	 4.0, Tourist Class   (241 pax)"      //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3 =  "109.0,  70.0,  0.0,	 4.0, Fwd Galley"                     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.4 =  "200.0,  20.0,  0.0,	 4.0, Center  Galley"                 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.5 =  "172.0,   0.0,  0.0,	 4.0, Aft Galley"                     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.6 = "3150.0,  40.0,  0.0, -3.0, Fwd Cargo Compt (2844 cu ft)"   //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.7 = "2450.0,   0.0,  0.0, -3.0, Aft Cargo Compt (2212 cu ft)"   //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

empty_weight= 298311.000
max_gross_weight= 618750.000

// Total A340-300 High Gross Max Structural Payload per Airbus = 112,436 lb
// Opensky Total A340-300 Total Possible Payload               = 112,436 lb

empty_weight_roll_MOI= 9146509.000
empty_weight_pitch_MOI= 16143375.000
empty_weight_yaw_MOI= 26494495.000
empty_weight_coupled_MOI= 0.000

CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar     =1.000
parasite_drag_scalar   =1.000
induced_drag_scalar    =1.000
elevator_effectiveness =1.200
aileron_effectiveness  =1.500
rudder_effectiveness   =2.500
pitch_stability        =1.500
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[pitot_static]
vertical_speed_time_constant=999		//Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[fuel]
Center1=    0.000,   0.000, -4.000, 11210.000, 3.000
Center2=  -83.676,   0.000,  0.000,  1650.000, 3.000
Center3=    3.000,   0.000, -4.000,  1814.500, 3.000
LeftMain=  -7.000, -37.983,  0.000, 11303.000, 3.000
RightMain= -7.000,  37.983,  0.000, 11303.000, 3.000
LeftAux=  -13.000, -70.269,  0.000,   970.000, 3.000
RightAux= -13.000,  70.269,  0.000,   970.000, 3.000
fuel_type= 2.000                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors= 1
electric_pump=1

[airplane_geometry]
wing_area= 3892.000
wing_span= 197.833
wing_root_chord= 25.000
wing_dihedral= 6.218
wing_incidence= 0.750
wing_twist= -0.500
oswald_efficiency_factor= 0.600
wing_winglets_flag= 1
wing_sweep= 30.000
wing_pos_apex_lon= 30.000
wing_pos_apex_vert= 0.000
htail_area= 1050.000
htail_span= 69.700
htail_pos_lon= -85.100
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 40.000
vtail_area= 690.000
vtail_span= 27.300
vtail_sweep= 35.000
vtail_pos_lon= -79.576
vtail_pos_vert= 5.800
elevator_area= 137.000
aileron_area= 68.000
rudder_area= 232.000
elevator_up_limit= 15.000
elevator_down_limit= 30.000
aileron_up_limit= 25.000
aileron_down_limit= 25.000
rudder_limit= 31.350
elevator_trim_limit= 15.000
spoiler_limit= 35.000
spoilerons_available= 0
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 9.969
min_flaps_for_spoilerons= 0.000
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000

[GeneralEngineData]
engine_type= 1
Engine.0= -10.000, -64.300, -2.413
Engine.1=  10.000, -30.900, -5.583
Engine.2=  10.000,  30.900, -5.583
Engine.3= -10.000,  64.300, -2.413
fuel_flow_scalar= 0.750
min_throttle_limit=-0.229907

// Basic engine information - thrust/Bypass ratio
// CFM56-5C2 - 31,200 lbs/6.6
// CFM56-5C3 - 32,500 lbs/6.5
// CFM56-5C4 - 34,000 lbs/6.4

[TurbineEngineData]
bypass_ratio=6.4
fuel_flow_gain= 0.001
inlet_area= 28.496
rated_N2_rpm= 29920.000
static_thrust= 34000.000
afterburner_available= 0
reverser_available= 1

[jet_engine]
thrust_scalar=1.070

[Reference Speeds]
flaps_up_stall_speed= 132.000
full_flaps_stall_speed= 124.000
cruise_speed= 460.000
max_indicated_speed=330.000000
max_mach=0.860010

[keyboard_response]
elevator= 100.000, 200.000
aileron=  100.000, 200.000
rudder=   100.000, 200.000

[Views]
eyepoint= 78.9, -1.756, 8.1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
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=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=1.0


[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

[direction_indicators]
direction_indicator.0=3,0

[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)

//Nose Gear
point.0= 1.000,  74.443,   0.000, -11.500, 1181.102, 0.000, 4.845, 72.000, 1.000, 1.400, 0.510,  7.000,  9.000, 0.000, 280.000, 300.000
point.1= 1.000, -13.500, -17.750, -12.300, 1574.803, 2.000, 2.450, -8.000, 0.700, 0.800, 0.550, 10.600, 11.800, 2.000, 280.000, 300.000  
point.2= 1.000, -13.500,  17.750, -12.300, 1574.803, 1.000, 2.450, -8.000, 0.700, 0.800, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000 
//point.3= 1.000, -11.067,   0.000, -12.500, 1574.803, 0.000, 4.845, -8.000, 1.000, 1.400, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000
point.4= 2.000, -14.167, -84.717,   0.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 5.000,   0.000,   0.000
point.5= 2.000, -14.167,  91.817,   0.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 6.000,   0.000,   0.000
point.6= 2.000, -120.667,  0.000,   6.500,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000,   0.000,   0.000
point.7= 2.000,  78.417,   0.000,  -3.750,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 4.000,   0.000,   0.000
point.8= 2.000,  14.167, -99.917,   0.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 7.000,   0.000,   0.000
point.9= 2.000,  0.000,   44.750,   0.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 8.000,   0.000,   0.000

static_pitch= -2.000
static_cg_height= 10.560
gear_system_type=0

//Nose Gear
//point.0= 1.000, 74.443, -2.000, -11.500, 1181.102, 0.000, 4.845, 72.000, 1.000, 2.400, 0.510, 7.000, 9.000, 0.000, 280.000, 300.000
//point.1= 1.000, 74.443,  2.000, -11.500, 1181.102, 0.000, 4.845, 72.000, 1.000, 2.400, 0.510, 7.000, 9.000, 0.000, 280.000, 300.000
//
//Main Gear (Left)
//point.2= 1.000, -11.067, -20.500, -13.500, 1574.803, 1.000, 4.845, -8.000, 2.200, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//point.3= 1.000, -11.067, -15.000, -13.500, 1574.803, 1.000, 4.845, -8.000, 2.200, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//point.4= 1.000,  -6.667, -20.500, -13.200, 1574.803, 1.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//point.5= 1.000,  -6.667, -15.000, -13.200, 1574.803, 1.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//
//Main Gear (Right)
//point.6= 1.000, -11.067,  20.500, -13.500, 1574.803, 2.000, 4.845, -8.000, 2.200, 2.400, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000
//point.7= 1.000, -11.067,  15.000, -13.500, 1574.803, 2.000, 4.845, -8.000, 2.200, 2.400, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000
//point.8= 1.000,  -6.667,  20.500, -13.200, 1574.803, 2.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000
//point.9= 1.000,  -6.667,  15.500, -13.200, 1574.803, 2.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000
//
// Main Gear (Center)
//point.10= 1.000, -11.067,  2.200, -13.200, 1574.803, 0.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000
//point.11= 1.000, -11.067, -2.200, -13.200, 1574.803, 0.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//
//
//Scrape Points
//point.12= 2.000, -14.167, -84.717, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
//point.13= 2.000, -14.167, 91.817, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
//point.14= 2.000, -120.667, 0.000, 6.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
//point.15= 2.000, 88.417, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
//point.16= 2.000, 14.167, -99.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
//point.17= 2.000, 0.000, 44.750, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
//
//static_pitch= -2.000
//static_cg_height= 11.560
//gear_system_type=0

[LIGHTS]        
Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =  1,    0.000,   0.000,  14.800, Opensky_beacon, 
light.1 =  1,    8.225,   0.000,  -4.800, Opensky_beacon, 
light.2  = 4,   86.000,   0.000,   1.000, fx_vclight  ,
light.3  = 5,   18.000,  27.000,  -4.000, Opensky_wing_light,
light.4  = 5,   19.933,   8.826,  -4.368, Opensky_wing_light,
light.5  = 5,   18.000, -27.000,  -4.000, Opensky_wing_light,
light.6  = 5,   19.933,  -8.826,  -5.368, Opensky_wing_light,
light.7  = 5,   17.700,  19.000,  -1.000, Opensky_nacelle_refl,
light.8 = 5,   17.700, -19.000,  -1.000, Opensky_nacelle_refl,
light.9 = 3, -116.500,   0.000,  11.200, Opensky_nav_yellow , 
light.10 = 2, -116.500,   0.200,  11.200, fx_strobeh ,
;light.11 = 5,   46.250,   9.350,   4.900, Opensky_nav_yellow ,
;light.12 = 5,   46.250,  -9.350,   4.900, Opensky_nav_yellow ,
;light.13 = 5,   47.850,   9.350,   4.900, Opensky_nav_yellow ,
;light.14 = 5,   47.850,  -9.350,   4.900, Opensky_nav_yellow ,


[General]
performance=Модификация:А340-300\n\nРазмах крыла:60,30м.\n\nДлинна:63,60м.\n\nВысота:16,70м.\n\nПлощадь крыла,м2:361,60.\n\nМаксимальная взлетная масса:275000,пустого самолета:130200\n\nТяга,кгс:4х15422\n\nМаксимальная скорость,км/ч:976.\n\nКрейсерская скорость,км/ч:937.\n\nПрактический потолок,м:11800.\n\nПрактическая дальность,км:12520.\n\nЭкипаж:2 чел.\n\nПолезная нагрузка:295 пассажиров в трехклассной конфигурации или 41000 кг груза.
atc_type=AIRBUS
atc_model=A340
Category=airplane

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=Opensky_sparks, 1
touchdown=fx_tchdwn, 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

[electrical]
//                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot          = 0, 5 , 17.0
flap_motor         = 1, 0 ,  1.0
gear_motor         = 0, 5 , 17.0
avionics_bus       = 0, 0 ,  1.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 0 ,  1.0
additional_system  = 0, 0 ,  1.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 7, 0 , 99.0
gear_motor         = 4, 0 ,  1.0
fuel_pump          = 0, 0 ,  1.0
fuel_transfer_pump = 0, 0 ,  1.0
starter1           = 0, 20, 17.0
starter2           = 0, 0 ,  1.0
light_nav          = 0, 0 ,  1.0
light_beacon       = 0, 0 ,  1.0
light_landing      = 0, 0 ,  1.0
light_taxi         = 0, 0 ,  1.0
light_strobe       = 0, 0 ,  1.0
light_panel        = 0, 7 , 99.0
light_recognition  = 0, 0 ,  1.0
light_wing         = 0, 0 ,  1.0
marker_beacon      = 0, 0 ,  1.0
standby_vacuum     = 0, 0 ,  1.0
auto_brakes        = 0, 0 ,  1.0
hydraulic_pump     = 0, 0 ,  1.0
propeller_device   = 0, 0 ,  1.0

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 18.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 250.000
lift_scalar= 1.000
drag_scalar= 1.500
pitch_scalar= 3.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.000, 0.000
flaps-position.2= 14.000, 0.000
flaps-position.3= 22.000, 0.000
flaps-position.4= 32.000, 0.000

[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 25.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.500
pitch_scalar= 3.000
flaps-position.0=  0.000, 0.000
flaps-position.1= 20.000, 0.000

[brakes]
toe_brakes_scale=1.000000
parking_brake=1
auto_brakes=4

[gear_warning_system]
gear_warning_available=0
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
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0


[TailHook]    // For opening cargo door.
tailhook_length=1                               ;(feet)
tailhook_position = 0.0, 0.0, 0.0            ;(feet) longitudinal, lateral, vertical positions from datum

[folding_wings]  // For opening main deck cargo door.
wing_fold_system_type = 4                       ;0=None
fold_rates = 0.05,0.05                          ;Percent per second
cable_force_adjust = 1.0

[exits]
number_of_exits = 2
exit_rate.0 = 0.2                               ;Percent per second
exit_rate.1 = 0.1                               ;Percent per second


[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0