[fltsim.0]
title=A310PW Defolt-1
sim=A310
model=PW
panel=
sound=
texture=1
atc_id=N737Y
atc_airline=Pacifica
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=AI
ui_type=Airbus A310
ui_variation=Defolt-1
description=

[General]
atc_type=Airbus
atc_model=A310
editable=0
performance=Cruise Speed        \nMach 0.84         555 mph         893 kmh\n\nEngine options        \nP&W 4000\nRR Trent 800\nGE 90 series\n\nMaximum Range              \n5,960 nm          6,859 sm        11,038 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     \n660,000 lb        299,370 kg\n\nLength    \n242 ft, 4 in         73.9 m\n\nWingspan      \n199 ft, 11 in          60.9 m\n\nHeight        \n60 ft, 8 in           18.5 m\n\nSeating       \nSeats 386 to 550 \n\nCargo Capacity        \n7,552 ft              213.8 m\n

[WEIGHT_AND_BALANCE]
max_gross_weight = 760000                       // (pounds)
empty_weight = 381680                           // (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  = 18000000
empty_weight_roll_MOI   = 5500000
empty_weight_yaw_MOI    = 16300000
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 = 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 = 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 = 18.0                              //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920                            //RPM, second stage compressor rated value
static_thrust = 45000                           //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 = -0.60
static_cg_height = 16.56
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

light.1 = 1,  3.00,   0.00, -9.45, fx_beaconb ,
light.2 = 1,  40.00,   0.00, 9.90, fx_beaconh ,
light.3 = 2,  45.50,   9.29, -0.90, fx_navwhih
light.4 = 2,  45.50,   -9.29, -0.90, fx_navwhih
light.5 = 3, -18.82,-79.12, 2.1, fx_navredh ,
light.6 = 3, -18.82, 79.12, 2.1, fx_navgreh ,
light.7 = 2, -19.60,-79.60, 2.3, fx_strobeh ,
light.8 = 2, -19.60, 79.60, 2.3, fx_strobeh ,

[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               = 4605.0                //Square feet
wing_span               = 200.0                 //Feet
wing_root_chord         = 23.0                  //Feet
wing_dihedral           = 6.2                   //Degrees
wing_incidence          = 1.0                   //Degrees
wing_twist              = -0.5                  //Degrees
oswald_efficiency_factor= 0.6                   //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       = 15.0                  //Degrees
elevator_down_limit     = 15.0                  //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=0.274667
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