[fltsim.0] title=Fiat G.50, sq.352 sim=Fiat_G50 model= panel= sound= texture= checklists= atc_id=G50N352 ui_manufacturer=Fiat ui_type="G.50 Freccia" ui_variation="" description="First italian monoplane fighter was first flown in 1937 and entered service early 1939. Apart a dozen that served during SCW, it was widely used during WWII in the Med theatre, mostly as a fighter and figther-bomber." [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [WEIGHT_AND_BALANCE] empty_weight=3780 // (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, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=200, -3.0, 0.0, 3.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=3717 empty_weight_roll_MOI=3613 empty_weight_yaw_MOI=6834 empty_weight_coupled_MOI=0.000000 max_gross_weight=5970.000000 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.5 aileron_effectiveness=1.0 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 [piston_engine] power_scalar=1.0 cylinder_displacement=165.630000 compression_ratio=6.700000 number_of_cylinders=14 max_rated_rpm=2520.000000 max_rated_hp=870.000000 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.0000 turbocharged=1 max_design_mp=34.999999 min_design_mp=1.000000 critical_altitude=13000.000000 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=11.500000 propeller_blades=3 propeller_moi=34.300000 beta_max=65.000000 beta_min=13.000000 min_gov_rpm=1800.000000 prop_tc=0.00000 gear_reduction_ratio=2.000000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 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 [Views] eyepoint=-4.0,0.000000,3.0735 [contact_points] point.0=1.000000,-10.333333,0.000000,-2.043333,3200,0,0.30,012.0,0.40,2.8,0.80,5,6,0,0,0 point.1=1.000000,2.416667,-5.416667,-5.583333,2200,1,1.05,0,0.50,2.9,0.78,5,9,2,130,165 point.2=1.000000,2.416667,5.416667,-5.583333,2200,2,1.05,0,0.50,2.9,0.78,5,7,3,130,165 point.3=2.000000,0.000000,-10.000000,-1.250000,1181.102400,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,0.000000,10.000000,-1.250000,1181.102400,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-10.250000,0.000000,-2.06667,1181.102400,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,2.416667,0.000000,-2.083333,1181.102400,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=15.29434 static_cg_height=4.401135 gear_system_type=1 [TailHook] tailhook_length=3.41 ;(feet) tailhook_position=-18.9, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, //(feet) long, lateral, vert, light.0=3, 2.90, -15.7, -0.8, fx_navred, light.1=3, 2.90, 15.7, -0.8, fx_navgre, light.2=2, -17.600, 0.000, 1.00, fx_strobe, light.3=4, -0.90, 0.000, 0.66, fx_vclight, [General] performance=Length: 8.3 m\nWing span: 10.98 m\nWeight: 2522 kg\nPower: 870 HP\nDetails: IS4G collection\nDesigner: Corrado La Posta\n [fuel] Center1=3.000000,0.000000,0.000000,93.000000,0.000000 LeftMain=-3.000000,-1.000000,0.000000,9.000000,0.000000 RightMain=-3.000000,1.000000,0.000000,9.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=196.000000 wing_span=36.000000 wing_root_chord=5.416667 wing_dihedral=0.000000 wing_incidence=0.999756 wing_twist=0.000000 oswald_efficiency_factor=1.029321 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=20.000000 htail_span=11.000000 htail_pos_lon=-16.666667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=9.000000 vtail_span=3.420526 vtail_sweep=0.000000 vtail_pos_lon=-16.666667 vtail_pos_vert=3.250000 elevator_area=13.000000 aileron_area=20.400000 rudder_area=13.060000 elevator_up_limit=26.000825 elevator_down_limit=12.249838 aileron_up_limit=17.486672 aileron_down_limit=17.480942 rudder_limit=20.088473 elevator_trim_limit=19.996227 spoiler_limit=11.459156 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 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=1 flaps-position.0=0.000000,0.000000 flaps-position.1=11.426415,0.000000 flaps-position.2=22.852831,0.000000 flaps-position.3=34.279246,0.000000 flaps-position.4=45.705662,0.000000 flaps-position.5=57.132077,0.000000 flaps-position.6=68.558493,0.000000 flaps-position.7=79.984908,0.000000 [GeneralEngineData] engine_type=0 Engine.0=8.416667,0.000000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=80.000000 full_flaps_stall_speed=64.000000 cruise_speed=226.036362 max_indicated_speed=700.000000 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [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=1,0,0,0 normal_pressure=6.930556 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0