[fltsim.0]
title=Macchi M416
sim=Macchi M416
model=
panel=
sound=
texture=
kb_checklists=
atc_id=B306
ui_manufacturer=Macchi
ui_type="Macchi M416"
ui_variation="Aerobatic and Instrument Trainer"
ui_typerole="Single Engine Prop"
ui_createdby="I. D'Attomo & G. Quai"
description=The Aermacchi started the production of this trainer in Summer 1951 under license from Fokker, while a second production line was established at Aerfer (Naples).
[General]
atc_type=M416
atc_model=M416
editable=0
performance= Engine: Avco Lycoming O-435-A flat-six piston 190 HP\nTop speed:206 kmh\nrange:925km.\nWingspan: 11.00 mt\nLenght: 8.20 mt\nEmpty weight: 850 Kg\nMaxToffWeight: 1135 Kg.
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight =2497 // (pounds)
empty_weight = 1870 // (pounds)
reference_datum_position = 1.8, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position= -2.1, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170,0.0, -2.0, 0.0, Pilot"
station_load.1 = "170,0.0, 2.0, 0.0, Copilot"
;Moments of Inertia
empty_weight_pitch_MOI = 717
empty_weight_roll_MOI = 395
empty_weight_yaw_MOI = 856
empty_weight_coupled_MOI = 0.0
[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, 5 , 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 2 , 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0
[flight_tuning]
cruise_lift_scalar =2.5
parasite_drag_scalar =1.7
induced_drag_scalar =0.85
elevator_effectiveness = 1.0
aileron_effectiveness = 0.35
rudder_effectiveness = 0.6
pitch_stability =1.4
roll_stability =1.3
yaw_stability =1.5
elevator_trim_effectiveness = 1.8
aileron_trim_effectiveness = 1.5
rudder_trim_effectiveness = 1.0
p_factor_on_yaw = 0.5
torque_on_roll = 0.5
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees, KIAS
flaps-position.1 = 20 // degrees, KIAS
flaps-position.2 = 60 // degrees, KIAS
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar =0.4
drag_scalar =0.5
pitch_scalar= 1.0
system_type = 0
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 3.5, 0.0, 0.60 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 90.3 //Cubic inches per cylinder
compression_ratio= 8.7 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm= 2550 //Max rated RPM
max_rated_hp=190 //Max rated HP
fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0 //Max design manifold pressure, (inHg)
min_design_mp= 0 //Min design manifold pressure, (inHg)
critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar =0.9 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.2 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 5.9 //Propeller moment of inertia
beta_max= 34 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 17 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1400 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 0 //Minimum RPM for prop feathering
beta_feather= 0 //Feathering pitch angle (degrees)
power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees)
//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, -16.50, 0.00, -1.9, 1377.95, 0, 0.4100, 180.0, 0.4, 2.5, 0.6, 0.0, 0.0, 0.0, 0.0, 0.0
point.1=1, -0.05, -2.92, -5.0, 1968.50, 1, 1.1660, 0.0, 0.6, 2.5, 0.6, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=1, -0.05, 2.92, -5.0, 1968.50, 2, 1.1660, 0.0, 0.6, 2.5, 0.6, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=2, -1.80, -12.25, -1.17, 787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2, -1.80, 12.25, -1.17, 787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2, -15.80, 0.00, 4.33, 787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2, 1.67, 0.00, -1.83, 787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch = 10.54
static_cg_height = 3.45
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.6 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint =0.90, 0.00, 2.10
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Nav.1 = 1, 1, 1
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[SMOKESYSTEM]
smoke.0=-10.00, 0.00, 0.00, fx_smoke_w
[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 = 140, 240
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=1,0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 2.78, -18.00,-0.18, fx_navred
light.1 = 3, 2.78, 18.00,-0.18, fx_navgre
light.2 = 4,3.30,-0.30,2.50,fx_vclighth
light.3 = 4,3.20, 0.30,2.50,fx_vclighth
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -1.8, -2.1, -0.8, 15.9, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -1.8, 2.1, -0.8, 15.9, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 112.0 //Square feet
wing_span = 24.6 //Feet
wing_root_chord = 4.8 //Feet
wing_dihedral = 2.6 //Degrees
wing_incidence = 0.0 //Degrees
wing_twist = 0.0 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 3.0 //Degrees, wing leading edge
wing_pos_apex_lon = -0.2 //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 = 28.0 //Square feet
htail_span = 10.5 //Feet
htail_pos_lon = -13.1 //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 = 10.0 //Degrees, horizontal tail leading edge
vtail_area = 15.0 //Square feet
vtail_span = 4.4 //Feet, tip to body
vtail_sweep = 20.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -14.3 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going up
elevator_area = 10.0 //Square feet
aileron_area = 18.4 //Square feet
rudder_area = 7.0 //Square feet
elevator_up_limit = 26.0 //Degrees
elevator_down_limit = 26.0 //Degrees
aileron_up_limit = 30.0 //Degrees
aileron_down_limit = 30.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 0.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available=0
positive_g_limit_flaps_up=10.000000
positive_g_limit_flaps_down=10.000000
negative_g_limit_flaps_up=-10.000000
negative_g_limit_flaps_down=-10.000000
[Reference Speeds]
flaps_up_stall_speed = 45.0 //Knots True (KTAS)
full_flaps_stall_speed = 40.0 //Knots True (KTAS)
cruise_speed = 150.0 //Knots True (KTAS)
max_indicated_speed = 220 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available= 0
default_vertical_speed=700.00
autothrottle_available=0
pitch_takeoff_ga=8.00
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=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.00
[forcefeedback]
ground_bumps_magnitude1=3000 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=4.0
ground_bumps_slope1=0.25
ground_bumps_magnitude2=350 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=0.7
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=2
stick_shaker=0
[pitot_static]
pitot_heat=1.00
[vacuum_system]
max_pressure=5.15
vacuum_type=1
electric_backup_pressure=0.00
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.00
bleed_air_scalar=1.00
[deice_system]
structural_deice_type=0
