[fltsim.0]
title			=MB339A "Prototipo"
sim			=MB339A
model			=
panel			=
sound			=
texture			=prototipo
kb_checklists		=Aermacchi MB339 A_CHECK.TXT
kb_reference		=Aermacchi MB339 A_REF.TXT

atc_model		=
atc_parking_codes	=
atc_id			= I-NOVE
atc_airline		=
atc_flight_number	= MM 588
ui_manufacturer		=AerMacchi
ui_Type			=MB339-A
ui_variation		=Aermacchi MB339A "Prototipo"
ui_createdby   		= Massimo Taccoli
visual_damage		=1

description=AerMacchi MB.339-A Prototipo, 1981\nAdvanced Trainer destined to be used by Italian Air Force and By many other Air forces in the world\n Flight Dynamics: Paolo Zamparo \nAircraft and Panel design: Massimo Taccoli\Sounds: Aaron Swindle

[fltsim.1]
title			=MB339A "NATO paint 1"
sim			=MB339A
model			=
panel			=
sound			=
texture			=NATO1
kb_checklists		=Aermacchi MB339 A_CHECK.TXT
kb_reference		=Aermacchi MB339 A_REF.TXT

atc_model		=
atc_parking_codes	=
atc_id			= 42
atc_airline		=
atc_flight_number	= MM 54498
ui_manufacturer		=AerMacchi
ui_Type			=MB339-A
ui_variation		=Aermacchi MB339A "NATO paint 1"
ui_createdby   		= Massimo Taccoli
visual_damage		=1

description=AerMacchi MB.339-A 61° Stormo, Galatina Lecce 1985\nAdvanced Trainer destined to be used by Italian Air Force and By many other Air forces in the world\n Flight Dynamics: Paolo Zamparo \nAircraft and Panel design: Massimo Taccoli\Sounds: Aaron Swindle

[fltsim.2]
title			=MB339A "Marlboro paint"
sim			=MB339A
model			=
panel			=
sound			=
texture			=MAR
kb_checklists		=Aermacchi MB339 A_CHECK.TXT
kb_reference		=Aermacchi MB339 A_REF.TXT

atc_model		=
atc_parking_codes	=
atc_id			= 15
atc_airline		=
atc_flight_number	= MM 54449
ui_manufacturer		=AerMacchi
ui_Type			=MB339-A
ui_variation		=Aermacchi MB339A "Marlboro paint"
ui_createdby   		= Massimo Taccoli
visual_damage		=1

description=AerMacchi MB.339-A SVBIA Galatina Lecce 1983\nAdvanced Trainer destined to be used by Italian Air Force and By many other Air forces in the world\n Flight Dynamics: Paolo Zamparo \nAircraft and Panel design: Massimo Taccoli\Sounds: Aaron Swindle

[fltsim.3]
title			=MB339A "NATO paint 2"
sim			=MB339A
model			=SL
panel			=
sound			=
texture			=NATO2
kb_checklists		=Aermacchi MB339 A_CHECK.TXT
kb_reference		=Aermacchi MB339 A_REF.TXT

atc_model		=
atc_parking_codes	=
atc_id			= 61-85
atc_airline		=
atc_flight_number	= MM 54546
ui_manufacturer		=AerMacchi
ui_Type			=MB339-A
ui_variation		=Aermacchi MB339A "NATO paint 2"
ui_createdby   		= Massimo Taccoli
visual_damage		=1

description=AerMacchi MB.339-A 61°Stormo, Galatina Lecce\nAdvanced Trainer destined to be used by Italian Air Force and By many other Air forces in the world\n Flight Dynamics: Paolo Zamparo \nAircraft and Panel design: Massimo Taccoli\Sounds: Aaron Swindle


[fltsim.4]
title			=MB339A "Bassa visibilità"
sim			=MB339A
model			=SL
panel			=
sound			=
texture			= 
kb_checklists		=Aermacchi MB339 A_CHECK.TXT
kb_reference		=Aermacchi MB339 A_REF.TXT

atc_model		=
atc_parking_codes	=
atc_id			= 61-20
atc_airline		=
atc_flight_number	= MM 54464
ui_manufacturer		= AerMacchi
ui_Type			= MB339-A
ui_variation		= Aermacchi MB339A "Bassa Visibilità"
ui_createdby   		= Massimo Taccoli
visual_damage		= 1

description=AerMacchi MB.339-A, 61* stormo Galatina 1996, Lecce\nAdvanced Trainer destined to be used by Italian Air Force and By many other Air forces in the world\n Flight Dynamics: Paolo Zamparo \nAircraft and Panel design: Massimo Taccoli\Sounds: Aaron Swindle

[fltsim.5]
title			=MB339-AA "Argentina Armada"
sim			=MB339A
model			=
panel			=
sound			=
texture			= ARG
kb_checklists		= Aermacchi MB339 A_CHECK.TXT
kb_reference		= Aermacchi MB339 A_REF.TXT

atc_model		=
atc_parking_codes	=
atc_id			= 4-A-15
atc_airline		=
atc_flight_number	= 0766
ui_manufacturer		= AerMacchi
ui_Type			= MB339-A
ui_variation		= Aermacchi MB339A "Argentina Armada"
ui_createdby   		= Massimo Taccoli
visual_damage		= 1

description=AerMacchi MB.339-AA Argentina Armada during the Falkland war, 1982 \nAdvanced Trainer destined to be used by Italian Air Force and by many other Air forces in the world\n Flight Dynamics: Paolo Zamparo \nAircraft and Panel design: Massimo Taccoli\Sounds: Aaron Swindle


[General]

atc_type=MB339-A
atc_model=MB339-A
editable=0
performance=Aircraft infoes are on the Knee-Board\nEnjoy !!!!!!!

//-------------------------------------------------------------------------------------

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1
Com.1=1,0
Com.2=1,0
Nav.1=1,0,1
Nav.2=1,0,0
Adf.1=1
//Adf.2=1
Transponder.1=1
Marker.1=1

//-------------------------------------------------------------------------------------

[LIGHTS]

//   Types: 1=beacon 2=strobe 3=navigation 4=cockpit 5=landing 6=Taxi 7=recognition
//          8=wing 9=logo 10=cabinlight 

light.0 = 1, -16.64,   0.00,  9.15,  fx_beaconh 
light.1 = 3,  -1.43, -18.20,  0.02,  fx_navred       // <== Sn
light.2 = 2,  -1.43, -18.20,  0.02,  fx_strobe 
light.3 = 3,  -1.43,  18.20,  0.02,  fx_navgre 
light.4 = 2,  -1.43,  18.20,  0.02,  fx_strobe 
light.5 = 3, -20.22,   0.00,  1.16,  fx_navwhi 
light.6 = 3,  -2.04,   0.00, -2.40,  fx_navwhi
light.7 = 3,  -6.44,   0.00,  2.62,  fx_navwhi
 
light.8 = 4,  10.23,   0.00,  0.229, Pz339_fx_vclight 
light.9 = 4,   5.23,   0.00,  0.229, Pz339_fx_vclight

light.10= 8, -24.00,   0.00,  0.000, Pz339_fx_engsmoke  // <== Black Smoke  

light.11 = 10, -2.24, -17.42,  0.000, Pz339_fx_WVortex  // <== Wing Vortex 
light.12 = 10, -2.24,  17.42,  0.000, Pz339_fx_WVortex  // <== Wing Vortex


//-------------------------------------------------------------------------------------

[SMOKESYSTEM]

smoke.0=0.00, -23.00, 0.00, Pz339_fx_smoke_engin    // <== Exhaust

//-------------------------------------------------------------------------------------

[EFFECTS]

wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
contrail=fx_contrail_s
//startup=fx_engstrt

//-------------------------------------------------------------------------------------

[electrical]

//BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)

max_Battery_voltage = 24.5
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 70.0

flap_motor         =0, 5 , 22.0
gear_motor         =0, 5 , 22.0
autopilot          =0, 5 , 22.0
avionics_bus       =0, 10, 22.0
avionics           =1, 5 , 23.0
pitot_heat         =0, 2 , 22.0
additional_system  =0, 14, 23.0
marker_beacon      =1, 2 , 22.0
gear_warning       =0, 2 , 22.0
fuel_pump          =0, 5 , 22.0
hydraulic_pump     =0, 5 , 22.0
starter1           =0, 10, 22.0
light_nav          =0, 5 , 22.0
light_beacon       =0, 2 , 22.0
light_landing      =0, 2 , 22.0
light_taxi         =0, 2 , 22.0
light_strobe       =0, 2 , 22.0
light_panel        =0, 5 , 22.0

//-------------------------------------------------------------------------------------

[flight_tuning]

//Flight Control effectiveness stability

elevator_effectiveness =1.000
aileron_effectiveness  =1.000
rudder_effectiveness   =1.000

elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

//Stability parameters

pitch_stability        =1.000
roll_stability         =1.000
yaw_stability          =1.000

//Lift parameter

cruise_lift_scalar     =1.000

//High Angle Of Attack parameters

hi_alpha_on_roll=1.0

//Drag Parameters

parasite_drag_scalar   =1.000
induced_drag_scalar    =1.000

//-------------------------------------------------------------------------------------

[pitot_static]

vertical_speed_time_constant=1.0  //Increasing this value will cause a more instantaneous 
                                  reaction in the VSI

//-------------------------------------------------------------------------------------

[WEIGHT_AND_BALANCE]

reference_datum_position= 0.000, 0.000, 0.000  // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)

empty_weight_CG_position= 0.000, 0.000, 0.000  // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations= 10

//Load Weight(lbs) longitudinal lateral vertical positions from datum (feet)

station_load.0="200,   9.00,   0.00,  -0.65,  Pilot"             //  Pilot
station_load.1="0.0,   4.00,   0.00,   0.00,  CoPilot"           //  Co-Pilot
station_load.2="0.0,   0.35, -11.50,  -1.60,  Free ExtLeftPyl"   //  Pyl
station_load.3="0.0,   0.70,  -9.02,  -1.80,  Free IntLeftPyl"   //  Pyl
station_load.4="0.0,   0.70,   9.02,  -1.80,  Free IntRightPyl"  //  Pyl
station_load.5="0.0,   0.35,  11.50,  -1.60,  Free ExtRightPyl"  //  Pyl

//Moments of Inertia

empty_weight= 6955.000          // (pounds)
max_gross_weight= 13007.000     // (pounds)

//FSEDIT
empty_weight_pitch_MOI= 6668
empty_weight_roll_MOI= 6199
empty_weight_yaw_MOI= 12930

empty_weight_coupled_MOI= 0.000

CG_forward_limit= 0.000
CG_aft_limit= 1.000

//-------------------------------------------------------------------------------------

[fuel]

//Tanks Position and capacity: 
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

LeftAux= -1.600, -17.420, 0.000, 132.000, 0.000
LeftMain= -0.300, -14.300, -1.000, 86.000, 0.000 
Center1= 0.000, 0.000, 2.000, 206.000, 0.000 
RightMain= -0.300, 14.300, -1.000, 86.000, 0.000
RightAux= -1.600, 17.420, 0.000, 132.000, 0.000

//Fuel type: 1=Avgas, 2=JetA
fuel_type=2
                                  
number_of_tank_selectors=1
electric_pump=1

//-------------------------------------------------------------------------------------

[airplane_geometry]

wing_area= 208.000                       //Square feet
wing_span= 35.000                        //Feet
wing_root_chord= 8.0                     //Feet
wing_sweep= 10.6000                      //Degrees, wing leading edge
wing_dihedral= 3.500                     //Degrees
wing_incidence= 0.000                    //Degrees
wing_twist= 0.000                        //Degrees

//wing_pos_apex_lon= 1.486  // FMW
wing_pos_apex_lon= 2.9                   //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert= -1.000               //Feet, vertical distance from reference point, positive going up

wing_winglets_flag= 0                    //Are winglets available?

oswald_efficiency_factor= 0.8            //Measure of lift effeciency of wing

htail_area= 38.000                       //Square feet
htail_span= 13.800                       //Feet
htail_pos_lon= -14.600                   //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert= 1.000                    //Feet, vertical distance from reference point, positive going up
htail_incidence= 0.000                   //Degrees
htail_sweep= 12.000                      //Degrees, horizontal tail leading edge

vtail_area= 22.000                       //Square feet
vtail_span= 6.600                        //Feet, tip to body
vtail_sweep= 52.000                      //Degrees, vertical tail leading edge
vtail_pos_lon= -10.5                     //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert= 2.45                     //Feet, vertical distance from reference point, positive going up

elevator_area= 14.400                    //Square feet
elevator_up_limit= 30.000                //Degrees
elevator_down_limit= 24.000              //Degrees
elevator_trim_limit= 19.500              //Degrees

aileron_area= 14.400                     //Square feet
aileron_up_limit= 20.000                 //Degrees
aileron_down_limit= 20.000               //Degrees

rudder_area= 10.000                      //Square feet
rudder_limit= 30.000                     //Degrees

spoiler_limit= 80.000                    //Degrees

spoilerons_available= 0                  //Spoilerons Available?
aileron_to_spoileron_gain= 0.000         //Aileron to spoileron gain
min_ailerons_for_spoilerons= 0.000       //Degrees
min_flaps_for_spoilerons= 0.000          //Minimum flap handle position when spoilerons activate

//-------------------------------------------------------------------------------------

[contact_points]

//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
        //14 Airspeed limit for retraction     (KIAS)
        //15 Airspeed that gear gets damage at (KIAS)
//GEAR
//               1         2       3      4         5      6      7       8      9      10     11     12     13     14     15        
point.0= 1.000,  13.240,   0.000, -4.810, 1574.800, 0.000, 0.653, 56.000, 0.450, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000
point.1= 1.000,  -1.428,  -4.669, -4.850, 1574.800, 1.000, 0.891, 0.000,  0.500, 2.500, 0.850, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000,  -1.428,   4.669, -4.850, 1574.800, 2.000, 0.891, 0.000,  0.500, 2.500, 0.850, 5.000, 5.000, 3.000, 0.000, 0.000
//SCRAPES
point.3= 2.000,  -1.583, -15.920,  0.170, 1574.800, 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,  -1.583,  15.920,  0.170, 1574.800, 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, -15.420,   0.000, -2.340, 1574.800, 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,  17.000,   0.000, -1.840, 1574.800, 0.000, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch= -0.051
static_cg_height= 4.460
gear_system_type=0

//-------------------------------------------------------------------------------------
                       
[GeneralEngineData]

engine_type= 1                    //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0= -17.000, 0.000, -0.800  //(feet) longitudinal, lateral, vertical distance from reference datum
                                  // Spostare engine su aumenta VR 
fuel_flow_scalar= 3.40            //Scalar for fuel flow efficiency Regola il consumo di carburante
//fuel_flow_scalar= 2.40  
min_throttle_limit= 0.00          //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature=-30.0
master_ignition_switch=1    

//-------------------------------------------------------------------------------------

[TurbineEngineData]

fuel_flow_gain= 0.020       //Gain on fuel flow Modifica il tempo per turbina al 100%
inlet_area= 3.000           //Square Feet, engine nacelle inlet area
rated_N2_rpm= 29920.000     //RPM, second stage compressor rated value
static_thrust= 4500.000     //Lbs, max rated static thrust at Sea Level

afterburner_available= 0
reverser_available= 0

//-------------------------------------------------------------------------------------

[jet_engine]

thrust_scalar=1.000

//-------------------------------------------------------------------------------------

//[folding_wings]
//wing_fold_system_type =  4
//fold_rates =  0.12, 0.11

//-------------------------------------------------------------------------------------

//[TailHook]
//tailhook_length = 4
//tailhook_position = -15, 0, -1
//cable_force_adjust = 1

//-------------------------------------------------------------------------------------

[Reference Speeds]

flaps_up_stall_speed= 106.000     //Knots True (KTAS)
full_flaps_stall_speed= 96.000    //Knots True (KTAS)

cruise_speed= 260.000             //Knots True (KTAS)
max_indicated_speed=530.000000    //Red line (KIAS)

max_mach=0.88

//-------------------------------------------------------------------------------------

[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=350.0,500.0
aileron =450.0,1000.0
rudder  =200.0,1000.0

//-------------------------------------------------------------------------------------

[Views]

eyepoint= 8.80, 0.00, 1.40      //(feet) longitudinal, lateral, vertical distance from reference datum

//-------------------------------------------------------------------------------------

[autopilot]

autopilot_available=1
flight_director_available=1
default_vertical_speed=4000.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
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

//-------------------------------------------------------------------------------------

[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

//-------------------------------------------------------------------------------------

[Exits]

number_of_exits=1
exit_rate.0=0.5

//-------------------------------------------------------------------------------------

[forcefeedback]

stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
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=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 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]

parking_brake=1           //Parking brake available
toe_brakes_scale=1.000000 //Brake scalar

//-------------------------------------------------------------------------------------

[gear_warning_system]

gear_warning_available=0  //Normal
pct_throttle_limit=0.1    //Percent throttle that activates warning
flap_limit_idle=15        //Flap angle that activates warning at idle
flap_limit_power=30       //Flap angle that activates warning at above idle
 
//-------------------------------------------------------------------------------------

[hydraulic_system]

normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

//-------------------------------------------------------------------------------------

[stall_warning]

type=2

//-------------------------------------------------------------------------------------

[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=1,0

//-------------------------------------------------------------------------------------

[flaps.0]       //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 2
flaps-position.0 = 0
flaps-position.1 = 20
flaps-position.2 = 40
damaging-speed = 400           // 200
blowout-speed = 440            // 240
system_type = 0
lift_scalar = 1
drag_scalar = 1
pitch_scalar = 1

//-------------------------------------------------------------------------------------