[FLTSIM.0]
TITLE=IKARUS
SIM=IKARUS
MODEL=
PANEL=
SOUND=
TEXTURE=
KB_CHECKLISTS=

UI_MANUFACTURER=COMCO
UI_TYPE=IKARUS C42
UI_VARIATION=G-CDZG
ATC_HEAVY=0
ATC_ID=G-CDZG
ATC_AIRLINE=
ATC_FLIGHT_NUMBER=
DESCRIPTION=COMCO IKARUS C42 ULTRALIGHT AIRCRAFT OF BARTON AIRPORT IN MANCHESTER ENGLAND .



ATC_TYPE=EXPERIMENTAL
ATC_MODEL=C42
EDITABLE=1
PERFORMANCE=
CATEGORY=AIRPLANE


[WEIGHT_AND_BALANCE]
MAX_GROSS_WEIGHT = 992.000
EMPTY_WEIGHT = 585.000

REFERENCE_DATUM_POSITION     = 3.600, 0.000, 0.000
EMPTY_WEIGHT_CG_POSITION     = -3.000, 0.000, 0.000

MAX_NUMBER_OF_STATIONS = 50

STATION_LOAD.0 =170.000000, -3.000000, -1.500000, 0.000000, PILOT          
STATION_LOAD.1 =170.000000, -3.000000, 1.500000, 0.000000, FRONT PASSENGER



;MOMENTS OF INERTIA
EMPTY_WEIGHT_PITCH_MOI  = 1917.000
EMPTY_WEIGHT_ROLL_MOI   = 1150.000
EMPTY_WEIGHT_YAW_MOI    = 2389.000
EMPTY_WEIGHT_COUPLED_MOI= 0.000
CG_FORWARD_LIMIT= 0.000
CG_AFT_LIMIT= 1.000

NUMBER_OF_EXITS=2
EXIT_RATE.0=1.4                               
EXIT_RATE.1=1.4 


[FLIGHT_TUNING]
CRUISE_LIFT_SCALAR     =1.000
PARASITE_DRAG_SCALAR   =1.701
INDUCED_DRAG_SCALAR    =1.000
ELEVATOR_EFFECTIVENESS =1.000
AILERON_EFFECTIVENESS  =1.000
RUDDER_EFFECTIVENESS   =1.403
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 = 0
ENGINE.0 = 2.400, 0.000, 0.000
FUEL_FLOW_SCALAR= 0.880
MIN_THROTTLE_LIMIT = 0.0
MASTER_IGNITION SWITCH=0                        //MINIMUM PERCENT THROTTLE.  GENERALLY NEGATIVE FOR TURBINE REVERSER


[PISTON_ENGINE]
POWER_SCALAR =1.000
CYLINDER_DISPLACEMENT= 84.000
COMPRESSION_RATIO= 8.500
NUMBER_OF_CYLINDERS= 4
MAX_RATED_RPM= 2300.000
MAX_RATED_HP= 80.000
FUEL_METERING_TYPE= 2
COOLING_TYPE= 0
NORMALIZED_STARTER_TORQUE= 0.600
TURBOCHARGED= 0
MAX_DESIGN_MP= 0.000
MIN_DESIGN_MP= 0.000
CRITICAL_ALTITUDE= 0.000
EMERGENCY_BOOST_TYPE= 0
EMERGENCY_BOOST_MP_OFFSET= 0.000
EMERGENCY_BOOST_GAIN_OFFSET= 0.000
FUEL_AIR_AUTO_MIXTURE= 0
AUTO_IGNITION= 0
MAX_RPM_MECHANICAL_EFFICIENCY_SCALAR=1.000
IDLE_RPM_MECHANICAL_EFFICIENCY_SCALAR=1.000
MAX_RPM_FRICTION_SCALAR=1.000
IDLE_RPM_FRICTION_SCALAR=1.000


[PROPELLER]
THRUST_SCALAR =0.623
PROPELLER_TYPE= 1
PROPELLER_DIAMETER= 6.300
PROPELLER_BLADES= 3
PROPELLER_MOI= 7.000
BETA_MAX= 0.000
BETA_MIN= 0.000
MIN_GOV_RPM= 1200.000
PROP_TC= 0.000
GEAR_REDUCTION_RATIO= 0.980
FIXED_PITCH_BETA= 20.000
LOW_SPEED_THEORY_LIMIT= 80.000
PROP_SYNC_AVAILABLE= 0
PROP_DEICE_AVAILABLE= 0
PROP_FEATHERING_AVAILABLE= 0
PROP_AUTO_FEATHERING_AVAILABLE= 0
MIN_RPM_FOR_FEATHER= 0.000
BETA_FEATHER= 0.000
POWER_ABSORBED_CF= 0.000
DEFEATHERING_ACCUMULATORS_AVAILABLE= 0 
PROP_REVERSE_AVAILABLE= 0.000
MINIMUM_ON_GROUND_BETA= 0.000
MINIMUM_REVERSE_BETA= 0.000


[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, 5 , 17.0
AVIONICS           = 1, 5 , 17.0
PITOT_HEAT         = 0, 2 , 17.0
ADDITIONAL_SYSTEM  = 0, 2 , 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
        //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

[CONTACT_POINTS]
POINT.0= 1.000, 2.750, 0.000, -3.720, 1500.000, 0.000, 0.322, 25.000, 0.180, 2.500, 1.000, 0.000, 0.000, 0.000, 0.000, 0.000
POINT.1= 1.000, -4.950, -3.500, -3.780, 3500.000, 1.000, 0.422, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
POINT.2= 1.000, -4.950, 3.500, -3.780, 3500.000, 2.000, 0.422, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000
POINT.3= 2.000, -3.800, -13.950, 0.000, 1.000, 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, -3.800, 13.950, 0.000, 1.000, 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, -10.900, 0.000, 0.300, 1800.000, 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, 1.480, 0.000, -2.170, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
POINT.7= 2.000, -10.900, 0.000, 2.830, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
POINT.8= 2.000, -3.900, 0.000, -2.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000

MAX_NUMBER_OF_POINTS = 9

STATIC_PITCH= 3.020
STATIC_CG_HEIGHT= 3.565


[BRAKES]
PARKING_BRAKE = 1        //PARKING BRAKE AVAILABLE
TOE_BRAKES_SCALE = 0.78  //BRAKE SCALAR


[HYDRAULIC_SYSTEM]
NORMAL_PRESSURE = 0.0    //PSI


[VIEWS]
EYEPOINT=-3.866790,-0.986815,1.350420

[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        
LIGHT.4 = 2,  -17.00,   0.00, 4.25, FX_STROBE
LIGHT.5 = 4,  -2.27,   0.00, 1.45, FX_VCLIGHT

[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 = 100,  180
AILERON  = 200, 1000
RUDDER   = 200, 1000


[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=1,0


[ATTITUDE_INDICATORS]
//TYPE: 0=NONE, 1=VACUUM GYRO, 2=ELECTRIC GYRO
ATTITUDE_INDICATOR.0 = 1 


[TURN_INDICATORS]
//TYPE: 0=NONE, 1=ELECTRIC GYRO, 2= VACUUM GYRO
TURN_INDICATOR.0=1,1    //TURN AND BANK


[EFFECTS]
WAKE=FX_WAKE
WATER=FX_SPRAY
DIRT=FX_TCHDRT
CONCRETE=FX_SPARKS
TOUCHDOWN=FX_TCHDWN_S, 1


[FUEL]
LEFTMAIN  = -3.900, -2.100, 2.500, 26.500, 0.000
RIGHTMAIN = -3.900, 2.100, 2.500, 26.500, 0.000
FUEL_TYPE = 1                                //FUEL TYPE: 1 = AVGAS, 2 = JETA
NUMBER_OF_TANK_SELECTORS = 1                    
ELECTRIC_PUMP=1


[AIRPLANE_GEOMETRY]
WING_AREA               = 154.000
WING_SPAN               = 27.170
WING_ROOT_CHORD         = 4.140
WING_DIHEDRAL           = 1.700
WING_INCIDENCE          = 1.500
WING_TWIST              = -3.000
OSWALD_EFFICIENCY_FACTOR= 0.680
WING_WINGLETS_FLAG      = 1
WING_SWEEP              = 0.000
WING_POS_APEX_LON       = -2.400
WING_POS_APEX_VERT      = 0.000
HTAIL_AREA              = 39.000
HTAIL_SPAN              = 11.700
HTAIL_POS_LON           = -12.300
HTAIL_POS_VERT          = 0.000
HTAIL_INCIDENCE         = 2.000
HTAIL_SWEEP             = 10.000
VTAIL_AREA              = 18.000
VTAIL_SPAN              = 4.800
VTAIL_SWEEP             = 40.000
VTAIL_POS_LON           = -11.940
VTAIL_POS_VERT          = 1.500
ELEVATOR_AREA           = 16.600
AILERON_AREA            = 18.300
RUDDER_AREA             = 3.000
ELEVATOR_UP_LIMIT       = 20.000
ELEVATOR_DOWN_LIMIT     = 20.000
AILERON_UP_LIMIT        = 20.000
AILERON_DOWN_LIMIT      = 20.000
RUDDER_LIMIT            = 24.000
ELEVATOR_TRIM_LIMIT     = 19.500
SPOILER_LIMIT           = 0.000
SPOILERONS_AVAILABLE    = 0
AILERON_TO_SPOILERON_GAIN = 0.000
MIN_AILERONS_FOR_SPOILERONS = 0.000
MIN_FLAPS_FOR_SPOILERONS = 0.000






[REFERENCE SPEEDS]
FLAPS_UP_STALL_SPEED    = 45.000
FULL_FLAPS_STALL_SPEED  = 30.000
CRUISE_SPEED            = 80.000
MAX_INDICATED_SPEED     = 160                  


[AUTOPILOT]
AUTOPILOT_AVAILABLE= 0
FLIGHT_DIRECTOR_AVAILABLE= 0
DEFAULT_VERTICAL_SPEED= 700.0
AUTOTHROTTLE_AVAILABLE= 0
PITCH_TAKEOFF_GA=8.0
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=9.00
NAV_INTEGRATOR_CONTROL=0.25
NAV_DERIVATIVE_CONTROL=0.00
NAV_INTEGRATOR_BOUNDARY=2.50
NAV_DERIVATIVE_BOUNDARY=0.00
GS_PROPORTIONAL_CONTROL=9.52
GS_INTEGRATOR_CONTROL=0.26
GS_DERIVATIVE_CONTROL=0.00
GS_INTEGRATOR_BOUNDARY=0.70
GS_DERIVATIVE_BOUNDARY=0.00
YAW_DAMPER_GAIN = 0.0



[FORCEFEEDBACK]
GEAR_BUMP_NOSE_MAGNITUDE=6000           ; 0 - 10000
GEAR_BUMP_NOSE_DIRECTION=18000          ; 0 - 35999 DEGREES
GEAR_BUMP_NOSE_DURATION=250000          ; IN MICROSECONDS
GEAR_BUMP_LEFT_MAGNITUDE=6000           ; 0 - 10000
GEAR_BUMP_LEFT_DIRECTION=35500          ; 0 - 35999 DEGREES
GEAR_BUMP_LEFT_DURATION=250000          ; IN MICROSECONDS
GEAR_BUMP_RIGHT_MAGNITUDE=6000          ; 0 - 10000
GEAR_BUMP_RIGHT_DIRECTION=00500         ; 0 - 35999 DEGREES
GEAR_BUMP_RIGHT_DURATION=250000         ; IN MICROSECONDS
GROUND_BUMPS_MAGNITUDE1=3250            ; 0 - 10000
GROUND_BUMPS_ANGLE1=8900                ; 0 - 35999 DEGREES
GROUND_BUMPS_INTERCEPT1=5.0
GROUND_BUMPS_SLOPE1=0.48
GROUND_BUMPS_MAGNITUDE2=750             ; 0 - 10000
GROUND_BUMPS_ANGLE2=9100                ; 0 - 35999 DEGREES
GROUND_BUMPS_INTERCEPT2=0.075
GROUND_BUMPS_SLOPE2=1.0
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=1



[GENERAL]
PERFORMANCE=Maximum Speed\t160 kts\nCruise Speed\t80 kts\nMaximum Range\t820 nm\nService Ceiling\t10,000 ft\nFuel Capacity\t60. Ltrs\nMax Gross Weight 450kg\nSeating\t\t2\n\t\n
atc_type=
atc_model=

[FLTSIM.1]
TITLE=IKARUS 2
SIM=IKARUS
MODEL=
PANEL=2
SOUND=
TEXTURE=2
KB_CHECKLISTS=
UI_MANUFACTURER=COMCO
UI_TYPE=IKARUS C42
UI_VARIATION=G-CEGZ
ATC_HEAVY=0
ATC_ID=G-CEGZ
ATC_AIRLINE=
ATC_FLIGHT_NUMBER=
DESCRIPTION=COMCO IKARUS C42 ULTRALIGHT AIRCRAFT OF BARTON AIRPORT IN MANCHESTER ENGLAND .

ATC_TYPE=EXPERIMENTAL
ATC_MODEL=C42
EDITABLE=1
PERFORMANCE=
CATEGORY=AIRPLANE

[FLTSIM.2]
TITLE=IKARUS 3
SIM=IKARUS
MODEL=
PANEL=
SOUND=
TEXTURE=1
KB_CHECKLISTS=
UI_MANUFACTURER=COMCO
UI_TYPE=IKARUS C42
UI_VARIATION=G-CEHV
ATC_HEAVY=0
ATC_ID=G-CEHV
ATC_AIRLINE=
ATC_FLIGHT_NUMBER=
DESCRIPTION=COMCO IKARUS C42 ULTRALIGHT AIRCRAFT OF BARTON AIRPORT IN MANCHESTER ENGLAND .

ATC_TYPE=EXPERIMENTAL
ATC_MODEL=C42
EDITABLE=1
PERFORMANCE=
CATEGORY=AIRPLANE
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 1.000
system_type= 3
damaging-speed= 120.000
blowout-speed= 160.000
lift_scalar= 0.900
drag_scalar= 0.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 40.000, 0.000