[fltsim.0]
title=Airbus A320-200
sim=a320200
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=
atc_id_color=0xffffffff
atc_airline=DRAGONAIR
atc_flight_number=940
ui_manufacturer=Airbus
ui_type=A320-200
ui_variation=Dragonair
description=The Airbus A320 is a mid-size, short to medium range airliner which set new standards for comfort and reliability upon its introduction in 1987.  The first "all electric" airliner it features a fly-by-wire, computerized flight control system.  Advanced aerodynamics coupled with electronic engine controls make it both comfortable and efficient in the air. The A320 has enjoyed great success in direct competition with the Boeing 737.
atc_heavy=0


[General]
atc_type=AIRBUS
atc_model=A320
performance=Max weight: 161,000 lbs\nMax speed: Mach 0.8\nRange: 3500 nm\nPassengers: 150-180

[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=162000.000
empty_weight=90400.000

reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000

max_number_of_stations=100

station_load.0=20000.000, 0.000, 0.000, 0.000

;Moments of Inertia
empty_weight_pitch_MOI=1200000.000
empty_weight_roll_MOI=680000.000
empty_weight_yaw_MOI=1900000.000
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=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[GeneralEngineData]
engine_type=1
Engine.0=2.000, -18.000, -2.500
Engine.1=2.000, 18.000, -2.500
fuel_flow_scalar=1.000

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=25.000
rated_N2_rpm=29920.000
static_thrust=26500.000
afterburner_available=0
reverser_available=1

[jet_engine]
thrust_scalar=1.000

[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=1.000, 38.000, 0.000, -8.000, 1181.100, 0.000, 1.250, 55.920, 1.000, 1.000, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000
point.1=1.000, -5.000, -11.600, -8.200, 1574.800, 1.000, 2.000, 0.000, 1.000, 1.000, 0.900, 7.000, 7.000, 2.000, 0.000, 0.000
point.2=1.000, -5.000, 11.600, -8.200, 1574.800, 2.000, 2.000, 0.000, 1.000, 1.000, 0.900, 7.000, 7.000, 3.000, 0.000, 0.000

point.3=2.000, -14.170, -47.330, 0.000, 787.400, 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, -14.170, 47.330, 0.000, 787.400, 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, -54.000, 0.000, 2.830, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

max_number_of_points=21

static_pitch=0.620
static_cg_height=7.800

[Views]
eyepoint=47.5, -2.3, 7.5   //(feet) longitudinal, lateral, vertical distance from reference datum


[Radios] 
// Radio Type=availiable, standby frequency, has glide slope 
Audio.1=1 
Com.1=1, 
Com.2=1, 
Nav.1=1, 
Nav.2=1, 
Adf.1=1 
Transponder.1=1 
Marker.1=1 


[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -13.55, -52.75,  7.75, fx_navredm ,
light.1=3, -13.55,  52.75,  7.75, fx_navgrem ,
light.2=3, -67.45,   0.00,  8.90, fx_navwhih ,
light.3=2, -19.70,  52.75,  7.40, fx_strobeh ,
light.4=2, -19.70, -52.75,  7.40, fx_strobeh ,
light.5=1,   4.14,   0.00, 14.00, fx_beaconb ,
light.6=1,  -8.10,   0.00, -1.85, fx_beaconh ,

[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

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 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;

[fuel]
Center1=0.000, 0.000, 0.000, 3100.000, 0.000
LeftMain=-3.000, -19.000, 0.000, 1600.000, 0.000
RightMain=-3.000, 19.000, 0.000, 1600.000, 0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
                   

[airplane_geometry]
wing_area=1300.000
wing_span=111.000
wing_root_chord=23.000
wing_dihedral=7.000
wing_incidence=1.000
wing_twist=0.000
oswald_efficiency_factor=0.750
wing_winglets_flag=1
wing_sweep=25.000
wing_pos_apex_lon=3.000
wing_pos_apex_vert=0.000
htail_area=240.000
htail_span=40.000
htail_pos_lon=-50.000
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=30.000
vtail_area=231.000
vtail_span=21.000
vtail_sweep=35.000
vtail_pos_lon=-40.000
vtail_pos_vert=12.000
elevator_area=78.000
aileron_area=26.400
rudder_area=75.000
elevator_up_limit=22.500
elevator_down_limit=19.500
aileron_up_limit=20.000
aileron_down_limit=20.000
rudder_limit=26.000
elevator_trim_limit=20.000
spoiler_limit=60.000
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=142.000
full_flaps_stall_speed=113.000
cruise_speed=477.000


[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

[SMOKESYSTEM]
smoke.1=-11.00, -1.00, 18.00, fx_smoke_rx
smoke.2=-11.00, -1.00, -18.00, fx_smoke_rx

[Flaps.0]
type=1
span-outboard=0.800
extending-time=8.000
system_type=1
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=5.000, 0.000
flaps-position.2=15.000, 0.000
flaps-position.3=25.000, 0.000
flaps-position.4=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=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=1.000, 0.000

[Flaps.2]
type=2
span-outboard=0.800
extending-time=2.000
system_type=1
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=1.000, 0.000