[fltsim.0]
title=Aermacchi M-346
sim=Macchi M-346
model=
panel=
sound=
texture=
kb_checklists=

atc_heavy=0
atc_airline=Air Force
atc_flight_number=B 306
ui_manufacturer=Aermacchi
ui_type=M-346
ui_variation=1_Trainer
description=Aermacchi is now developing a next-generation jet trainer designated the "M-346".This program began as a joint effort with the Yakovlev organization , resulting in the construction of a demonstrator, which is now performing test flights. 

[fltsim.1]
title=Aermacchi M-346PAINTprototype
sim=Macchi M-346
model=
panel=
sound=
texture=prototype
kb_checklists=

atc_heavy=0
atc_airline=Air Force
atc_flight_number=X616
ui_manufacturer=Aermacchi
ui_type=M-346
ui_variation=Prototype factory paint
description=Aermacchi is now developing a next-generation jet trainer designated the "M-346".This program began as a joint effort with the Yakovlev organization , resulting in the construction of a demonstrator, which is now performing test flights. 




[General]
atc_type=Macchi M-346
atc_model=Macchi M-346
editable=1

performance=Max Speed: 720 Kts\nCruise Speed: Mach n° 0.88\nMax Ceiling: 45000ft\nRange: 2.590 Km.\nMax Mach:  1.2 in steep dive.


[WEIGHT_AND_BALANCE]
max_gross_weight=22000.00 
empty_weight=10200.00	

reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, -1.000

max_number_of_stations=50



;Moments of Inertia
empty_weight_pitch_MOI=320000.000
empty_weight_roll_MOI=50000.000
empty_weight_yaw_MOI=120000.000
empty_weight_coupled_MOI=0.000
CG_forward_limit=0.000
CG_aft_limit=1.000
station_load.0=0.00,0.00,0.00,0.00


[electrical]
max_battery_voltage=12.0
generator_alternator_voltage=13.8
max_generator_alternator_amps=40.0

;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus=0, 10, 9.5
avionics=1, 5 , 9.5
additional_system=0, 20, 9.5
marker_beacon=1, 2 , 9.0
fuel_pump=0, 5 , 9.0


[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.11
induced_drag_scalar=3.35
elevator_effectiveness=1.00
aileron_effectiveness=4.5
rudder_effectiveness=1.00
pitch_stability=3.6
roll_stability=1.00
yaw_stability=1.00
elevator_trim_effectiveness=0.6
aileron_trim_effectiveness=1.10
rudder_trim_effectiveness=1.10


[GeneralEngineData]
engine_type=1
Engine.0=-19.000, -3.000, 0.000
Engine.1=-19.000, 3.000, 0.000
fuel_flow_scalar=0.200
min_throttle_limit=-0.25


[TurbineEngineData]
fuel_flow_gain=0.003
inlet_area=3.000
rated_N2_rpm=29000.0	
static_thrust=4300.0
afterburner_available=0
reverser_available=0


[jet_engine]
thrust_scalar=1.000


//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, 13.500, 0.000, -6.150, 1200.000, 0.000, 0.800, 45.000, 0.200, 2.500, 0.900, 3.000, 3.000, 0.000, 0.000, 0.000
point.1=1.000, -2.000, -4.000, -6.350, 1600.000, 1.000, 1.000, 0.000, 0.500, 2.500, 0.900, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1.000, -2.000, 4.000, -6.350, 1600.000, 2.000, 1.000, 0.000, 0.500, 2.500, 0.900, 5.000, 5.000, 3.000, 0.000, 0.000
point.3=2.000, -3.330, -23.920, -3.000, 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, -3.330, 23.920, -3.000, 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, -22.670, 0.000, 0.000, 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, 23.030, 0.000, -1.500, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch=-0.750
static_cg_height=5.200
gear_system_type=0


[Views]
eyepoint=7.45, 0.00, 0.90 




[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3,  -6.72, -15.90, 0.15, fx_navred ,
light.1 = 3,  -6.72,  15.90, 0.15, fx_navgre ,
light.2 = 3, -19.50,   0.00,  0.20, fx_navwhi ,
light.3 = 1, -1.00, 0.00, 2.10,  fx_beacon ,   
light.4 = 4, 9.10,0.0,2.2,  fx_vclight
light.5 = 4, 6.10,0.0,2.2,  fx_vclight


[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
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


[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn,0.0


[fuel]
Center1=0.000, 0.000, 0.000, 300.000, 0.000
LeftMain=0.000, -5.000, 0.000, 135.000, 0.000
RightMain=0.000, 5.000, 0.000, 135.000, 0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0


[airplane_geometry]
wing_area=280.000
wing_span=39.000
wing_root_chord=9.500
wing_dihedral=3.000
wing_incidence=-0.500
wing_twist=-1.000
oswald_efficiency_factor=0.800
wing_winglets_flag=0
wing_sweep=37.000
wing_pos_apex_lon=8.000
wing_pos_apex_vert=-2.000
htail_area=70.000
htail_span=12.800
htail_pos_lon=-25.000
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=35.000
vtail_area=60.000
vtail_span=7.000
vtail_sweep=35.000
vtail_pos_lon=-25.000
vtail_pos_vert=2.000
elevator_area=25.000
aileron_area=26.000
rudder_area=6.500
elevator_up_limit=17.000
elevator_down_limit=15.000
aileron_up_limit=18.000
aileron_down_limit=18.000
rudder_limit=30.000
elevator_trim_limit=25.00
spoiler_limit=66.0
spoilerons_available=0
aileron_to_spoileron_gain=4.600
min_ailerons_for_spoilerons=5.000
min_flaps_for_spoilerons=0.000


[Reference Speeds]
flaps_up_stall_speed=110.00
full_flaps_stall_speed=95.00
cruise_speed=580.000
max_indicated_speed=840.00
max_mach=1.20


[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm=90
autothrottle_takeoff_ga=0
pitch_takeoff_ga=8;
max_pitch=10.00
max_pitch_acceleration=1.00
max_pitch_velocity_lo_alt=2.00
max_pitch_velocity_hi_alt=1.50
max_pitch_velocity_lo_alt_breakpoint=20000.00
max_pitch_velocity_hi_alt_breakpoint=28000.00
max_bank=25.00
max_bank_acceleration=1.80
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=9.522
gs_integrator_control=0.260
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.00


[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

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


[brakes]
toe_brakes_scale=1.30
parking_brake=1


[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.10
flap_limit_power=30.0
flap_limit_idle=15.00

[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=3000.0


[stall_warning]
type=1


[attitude_indicators]
attitude_indicator.0=1


[turn_indicators]
turn_indicator.0=1,0


[Flaps.0]
type=1
span-outboard=0.500
extending-time=7.000
system_type=0
damaging-speed=250.0
blowout-speed=300.0
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
flaps-position.0=0.00
flaps-position.1=10.00
flaps-position.2=20.00
flaps-position.3=30.00
flaps-position.4=40.00


[Flaps.1]
type=2
span-outboard=0.5
extending-time=6.0
system_type=0
damaging-speed=250.0
blowout-speed=300.0
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
flaps-position.0=0.00
flaps-position.1=9.00
flaps-position.2=18.00




[SMOKESYSTEM]
smoke.0=0.00, -20.0, 0.0, fx_smoke_w