[fltsim.0]
title=SIAI_208M
sim=SIAI_208
model=
panel=
sound=
texture=
kb_checklists=
atc_id=B306
ui_manufacturer="SIAI MARCHETTI"
ui_type="SIAI_208M"
ui_variation="Military Camo"
ui_typerole="Single Engine Prop"
ui_createdby="Capt. Italo D'Attomo"
description=Derived from the S205, in 1968 the S.208 version became available, produced basically as a five-seat, more powerful version of the S.205, with some 60% of its structural components in common. By February 1973 approximately 80 S.208s had been delivered to customers in Europe and Africa, including 44 S.208Ms to the Italian Air Force for liaison and training duties. A version for general duties, including agricultural and ambulance work, was developed as the S.208AG. \nDesign & Paintings : Italo D'Attomo\nDate:October 2010.
[General]
atc_type=SIAI_208
atc_model=SIAI_208
editable=0
performance="Maximum Speed\t\n148 kts\t274 kmh\n\nCruise Speed\t\n141 kts\t261 kmh\n\nEngine\t\nLycoming O-540-E4A5 260 hp\n\nPropeller\t\nTwo-bladed McCauley constant speed\n\nMaximum Range\t\n970 nm \t1,795 km\n\nService Ceiling\t\n17,500 ft 5,330 m\n\nEmpty Weight\t\n1,807 lb \t \n\nMaximum Gross Weight\t\n2,976 lb \t \n\nUseful Load\t\n1,169 lb \t 530 kg\n\nSeating\t\nUp to 5"
Category = airplane
[CameraDefinition.0]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 9.0, 0.3, 0.0
InitialPbh = 5, 0, 275
XyzAdjust = TRUE
Category=Aircraft
CycleHidden=Yes
ClipMode=Minimum
[CameraDefinition.1]
Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -9.0, 0.3, 0.0
InitialPbh = 5, 0, 85
XyzAdjust = TRUE
Category=Aircraft
CycleHidden=Yes
ClipMode=Minimum
[CameraDefinition.2]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
ShowWeather = Yes
InitialXyz = 0, 2.0, -6.5
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.001]
Title = "Right Seat"
Guid = {195EAB58-9E4A-1E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
CycleHidden=Yes
InitialXyz=0.45, -0.02, 0.0
InitialPbh=0, 0, 0
[CameraDefinition.002]
Title = "Radio Stack"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
CycleHidden=Yes
InitialXyz=0, -0.21, 0
InitialPbh=9, 0, 16
[WEIGHT_AND_BALANCE]
max_gross_weight = 2976 // (pounds)
empty_weight = 1807 // (pounds)
reference_datum_position = 3.9, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -3.7, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, -3.1, -1.5, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -3.1, 1.5, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 100, -6.1, -1.5, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 100, -6.1, 1.5, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 33, -8.5, 0.0, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_name.1 = "Front Passenger"
station_name.2 = "Rear Passenger"
station_name.3 = "Rear Passenger"
station_name.4 = "Baggage"
;Moments of Inertia
empty_weight_pitch_MOI = 2706
empty_weight_roll_MOI = 2131
empty_weight_yaw_MOI = 3932
empty_weight_coupled_MOI = 0.0
[pitot_static]
vertical_speed_time_constant = 0.8 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 0.6
aileron_effectiveness = 0.6
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 2.1, 0.0, 0.0 //(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= 8.0 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm= 2575 //Max rated RPM
max_rated_hp= 260 //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= 1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 38 //Max design manifold pressure, (inHg)
min_design_mp= 1 //Min design manifold pressure, (inHg)
critical_altitude= 18000 //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 = 1.0 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.3 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 8.0 //Propeller moment of inertia
beta_max= 43 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 15 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1100 //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= 1 //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)
[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, 1.18, 0.0, -4.35, 1500.0, 0, 0.523, 33.66, 0.296, 2.5, 0.794, 3.5, 3.5, 0, 165.0, 165.0
point.1=1, -5.48, -4.5, -4.30, 1574.8, 1, 0.523, 0.00, 0.286, 2.5, 0.808, 4.7, 4.7, 2, 165.0, 165.0
point.2=1, -5.48, 4.5, -4.30, 1574.8, 2, 0.523, 0.00, 0.286, 2.5, 0.808, 5.2, 5.2, 3, 165.0, 165.0
point.3=2, -3.90, -18.0, -0.67, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -3.90 18.0, -0.67, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -20.23, 0.0, 0.83, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, -1.48, 0.0, -2.17, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 4, 0.0, 0.0
point.7=2, -20.23, 0.0, 6.83, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 7, 0.0, 0.0
point.8=2, -4.90, 0.0, -1.83, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 8, 0.0, 0.0
max_number_of_points = 21
static_pitch = 2.9
static_cg_height = 3.7
gear_system_type=0 //Electric
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
auto_brakes = 0
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint = -3.00, -.884, 1.4
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -3.65, -17.85, -0.30, fx_navred ,
light.1 = 3, -3.65, 17.85, -0.30, fx_navgre ,
light.2 = 3, -21.15, 0.00, 0.20, fx_navwhi ,
light.3 = 1, -18.62, 0.00, 6.46, fx_beacon ,
light.4 = 4, 0.00, -0.50, 0.62, fx_vclight,
light.5 = 4, 0.00, 0.50, 0.62, fx_vclight,
[flaps.0]
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 = 15 // degrees, KIAS
flaps-position.2 = 30 // degrees, KIAS
flaps-position.3 = 45 // degrees, KIAS
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[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
[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
[altimeters]
altimeter.0=1
altimeter.1=1
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[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
attitude_indicator.1 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1 //Turn AND Bank
[vacuum_system]
max_pressure=5.15 //PSI
vacuum_type=1 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
electric_backup_pressure=4.9 //PSI
engine_map=1
[pneumatic_system]
max_pressure=0.000000
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -4.1, -7.9, -0.8, 47.5, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -4.1, 7.9, -0.8, 47.5, 3.0 //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 = 175.0 //Square feet
wing_span = 36.1 //Feet
wing_root_chord = 5.1 //Feet
wing_dihedral = 5.5 //Degrees
wing_incidence = 2.5 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = -2.6 //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 = 34.0 //Square feet
htail_span = 11.8 //Feet
htail_pos_lon = -18.6 //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 = 1.0 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 10.0 //Square feet
vtail_span = 3.6 //Feet, tip to body
vtail_sweep = 0.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -16.5 //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 = 16.6 //Square feet
aileron_area = 18.3 //Square feet
rudder_area = 6.7 //Square feet
elevator_up_limit = 28.0 //Degrees
elevator_down_limit = 21.0 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 15.0 //Degrees
rudder_limit = 24.0 //Degrees
elevator_trim_limit = 20.5 //Degrees
spoiler_limit = 90.0 //Degrees
spoiler_extension_time = 0.25 //Seconds
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 = 4.0 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down= 2.0 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up = -1.5 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= -1.5 //Design G load tolerance (negative, flaps down)
load_safety_factor = 1.5 //Design G load safety factor
[Reference Speeds]
flaps_up_stall_speed = 66.0 //Knots True (KTAS)
full_flaps_stall_speed = 52.8 //Knots True (KTAS)
cruise_speed = 180.0 //Knots True (KTAS)
max_indicated_speed = 195 //Red line (KIAS)
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.50,0.50 ;Percent per second
[autopilot]
autopilot_available= 1
flight_director_available= 1
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=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
[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots