[fltsim.0] title=SM95C sim=SM95C model= panel= sound= texture= kb_checklists=SM95C_chek kb_reference=SM95C_ref ui_manufacturer=Savoia Marchetti ui_type="SM95C" ui_variation="ALITALIA" atc_id=I-DALN atc_airline=ALITALIA description=With Fiat G12 was one of the first airliner of ALITALIA, the new Italian company after the War. This type of aircraft entered in service in July 1947 on the route Roma-OsloThe last flight in September 1954,due to the enter in service american DC4, more modern,cabin pressurized and modern avionics. [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //6=taxi light, 7=recognition light, 8=wing light, 9=logo light light.0=3, 10.00, 58.00, 1.20, fx_navgre light.1=2, 10.00, 58.00, 1.20, fx_strobeh light.2=3, 10.00, -57.40, 1.20, fx_navred light.3=2, 10.00, -57.40, 1.20, fx_strobeh light.4=1, -31.60, 0.00, 13.20, fx_beaconb light.5=3, -38.00, 0.00, 0.50, fx_navwhih light.6=2, 3.50,0.0,-4.10, fx_strobeh light.7=4, 25.90,0.00,3.70, fx_vclight // cabina aereo light.8=4, 19.700,0.00,2.00,fx_vclight_ju // fusoliera light.9=4, 17.00,0.00,2.000,fx_vclight_ju // fusoliera light.10=4, -4.00,0.00,2.000,fx_vclight_ju // fusoliera light.11=4, 11.80,-1.900,3.800,fx_vclight_yellow //pannello light.12=3, 16.50,12.70,-3.95, fx_sm95_scarico //0 light.13=3, 16.50,-12.90,-3.50,fx_sm95_scarico //1 light.14=3, 14.40,-21.90,-3.65,fx_sm95_scarico //2 light.15=3, 14.40,22.40,-3.60,fx_sm95_scarico //3 light.16=5,15.05,30.10,-1.150, fx_sm95_land //atterraggio light.17=5,15.05,-30.10,-1.150,fx_sm95_land light.18=6,25.50,0.00,-4.050, fx_sm95_taxi //rullaggioDX [WEIGHT_AND_BALANCE] empty_weight=23360 // (pounds) reference_datum_position=0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, 8.0, -4.0, 2.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.0=170, 8.0, 4.0, 2.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=556044 //slug-ft^2 empty_weight_roll_MOI=1104581 //slug-ft^2 empty_weight_yaw_MOI=1130739 //slug-ft^2 empty_weight_coupled_MOI=0.000000 max_gross_weight=35295.000000 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.25 aileron_trim_effectiveness=1.25 rudder_trim_effectiveness=1.25 [piston_engine] power_scalar=1.3 cylinder_displacement=202.200000 compression_ratio=6.000000 number_of_cylinders=9 max_rated_rpm=2700.000000 max_rated_hp=1200.000000 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=50.999999 min_design_mp=1.000000 critical_altitude=24000.000000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [propeller] thrust_scalar=1.0 propeller_type=0 propeller_diameter=10.833000 propeller_blades=3 propeller_moi=33.370000 beta_max=53.500000 beta_min=18.500000 min_gov_rpm=1800.000000 prop_tc=0.010000 gear_reduction_ratio=1.778000 fixed_pitch_beta=0.000000 low_speed_theory_limit=80.000000 prop_sync_available= 1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available= 1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE rotation=-1,1 min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering beta_feather= 89.5 //Feathering pitch angle (degrees) power_absorbed_cf= 0.9 //Coefficient of friction for power absorbed by propeller in feather defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0.000000 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Radios] 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 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 engine_generator_map = 1,1,1,1 electric_always_available = 0 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 15, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 22 starter2 = 0, 20, 22 starter3 = 0, 20, 22 starter4 = 0, 20, 22 light_nav = 0, 5, 22 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_recognition = 0, 0, 0 light_wing = 0, 0, 0 light_logo = 0, 0, 0 light_strobe = 0, 0, 0 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 propeller_deice = 0, 5, 17 light_cabin = 0, 5, 17 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.125 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=16 // degrees, KIAS flaps-position.2=32 // degrees, KIAS flaps-position.3=48 // degrees, KIAS damaging-speed=200 // KIAS blowout-speed=305 // KIAS [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 point.0=1.000000,-29.300,0.000000,-4.0000,1574.803200,0.000000,1.000,18.540000,0.273735,2.500000,0.6500,13.000000,13.000000,0.000000,0.000000,0.000000 point.1=1.000000,14.4000,-9.8000,-10.5000,1574.803200,1.000000,1.9000,0.000000,0.512976,2.500000,0.65000,5.000000,5.000000,2.000000,0.000000,0.000000 point.2=1.000000,14.4000,9.8000,-10.50000,1574.803200,2.000000,1.9000,0.000000,0.512976,2.500000,0.65000,5.000000,5.000000,3.000000,0.000000,0.000000 point.3=2.000000,-8.500000,-47.500000,0.833333,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-8.500000,47.500000,0.833333,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-27.333333,0.000000,0.750000,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,18.833333,0.000000,-1.666667,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=7.9 static_cg_height=8.6 gear_system_type=0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_DC3_Sparks touchdown=fx_DC3_Tiremark, 1 contrail=fx_DC3_Contrail [Views] eyepoint=10.600,-.98,3.80 [General] performance=SPECIFICATIONS \nSpan: 34.28 meters\nLength:22.24 meters \nHeight: 5.70 meters \nWeight: 21,000 Kg. loaded \nEngines: Four Alfa Romeo 128 R.C.18 .HP 860 each \nPERFORMANCE \nMaximum speed:400 Km/h. \nCruising speed: 360 Km/h. \nRange: 2,000 Km. \nService Ceiling: 6,500 meters \n [fuel] LeftMain=0.000000,-5.100000,0.000000,1400.000000,0.000000 RightMain=0.000000,5.100000,0.000000,1400.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=1420.000000 wing_span=104.000000 wing_root_chord=14.000000 wing_dihedral=5.998535 wing_incidence=1.999512 wing_twist=0.000000 oswald_efficiency_factor=0.646541 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=331.000000 htail_span=43.000000 htail_pos_lon=-38.750000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=220.000000 vtail_span=16.911535 vtail_sweep=0.000000 vtail_pos_lon=-38.750000 vtail_pos_vert=7.166667 elevator_area=94.410000 aileron_area=80.250000 rudder_area=39.490000 elevator_up_limit=28.000447 elevator_down_limit=22.998526 aileron_up_limit=26.000825 aileron_down_limit=18.999280 rudder_limit=28.000447 elevator_trim_limit=19.996227 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [GeneralEngineData] engine_type=0 Engine.0=12.916667,-21.750000,0.000000 Engine.1=14.333333,-10.000000,-0.833333 Engine.2=14.333333,10.000000,-0.833333 Engine.3=12.916667,21.750000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=110.000000 full_flaps_stall_speed=88.000000 cruise_speed=239.134659 max_indicated_speed=760.500000 [keyboard_response] elevator=350.000000,450.000000 aileron=400.000000,400.000000 rudder=200.000000,400.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 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 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=6.930556 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0