[fltsim.0] title=Fiat_G-55_Centauro sim=Fiat_G-55_Centauro model= panel= sound= texture= ui_manufacturer=Fiat ui_type=G55 Centauro ui_variation=Default kb_checklists= description=The Fiat G55 Centauro was a single engine single seat WW2 Fighter used by the Italian Air Force from 1943-1945.\nThe first prototype flew on April 30, 1942. Around 130 Centauro were produced, most of them seeing service with the Aeronautica Nazionale Repubblicana in northern Italy. After suffering repeated bombing attacks on the Turin Fiat's production plant in northern Italy, supplies of the Fiat G.55 dwindled and eventually all Italian fighter squadrons in Italy were intended to be equipped with the Me 109G. Italian pilots however tended to avoid the substitution of the G55 with a plane that they consider inferior. For this, the production of G55 and spare parts never ceased and, when the allies reached Fiat factory, they found 19 planes ready to be delivered and spare parts to build several others.\n\n [fltsim.1] title=Fiat_G-55_Centauro_1 sim=Fiat_G-55_Centauro model= panel=2 sound= texture= ui_manufacturer=Fiat ui_type=G55 Centauro ui_variation=High view Panel kb_checklists= description=The Fiat G55 Centauro was a single engine single seat WW2 Fighter used by the Italian Air Force from 1943-1945.\nThe first prototype flew on April 30, 1942. Around 130 Centauro were produced, most of them seeing service with the Aeronautica Nazionale Repubblicana in northern Italy. After suffering repeated bombing attacks on the Turin Fiat's production plant in northern Italy, supplies of the Fiat G.55 dwindled and eventually all Italian fighter squadrons in Italy were intended to be equipped with the Me 109G. Italian pilots however tended to avoid the substitution of the G55 with a plane that they consider inferior. For this, the production of G55 and spare parts never ceased and, when the allies reached Fiat factory, they found 19 planes ready to be delivered and spare parts to build several others.\n\n [General] atc_type=FIAT atc_model=G55 editable=0 performance=Length: 30'9" (9.37 m)\nWingspan: 38'10" (11.85 m)\nHeight: 10'3 1/4" (3.13 m)\nWing area: 227.23 ft² (21.11 m²)\nEmpty weight: 5,798 lb (2,630 kg)\nMaximum Take-Off Weight: 8,179 lb (3,718 kg)\nPowerplant: 1× Fiat R.A 1050 Tifone (license-built Daimler-Benz DB 605A-1) liquid-cooled inverted V-12, 1,475 hp (1,085 kW)\nMaximum speed: 385 mph (620 km/h)\nRange: 746 miles (1,160 km)\nService ceiling: 42,650 (ft12,700 m)\nArmament: 3x20 mm Mg 151/20 cannons, one engine-mounted and two wing-mounted 4x12.7 mm Breda-SAFAT machine guns Provision for two 160 kg (353 lb) bombs on underwing racks.\n\n reference_datum_position=0.0, 0.0, 0.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.095, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=10 [pitot_static] vertical_speed_time_constant = 1 [WEIGHT_AND_BALANCE] max_gross_weight = 8179 empty_weight = 5798 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 = 6193 empty_weight_roll_MOI = 5511 empty_weight_yaw_MOI = 10832 empty_weight_coupled_MOI=0.000000 max_gross_weight=9796.500000 reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 [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=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [piston_engine] power_scalar=1.0 cylinder_displacement=181.500000 compression_ratio=8.500000 number_of_cylinders=12 max_rated_rpm=2800.000000 max_rated_hp=1400.000000 fuel_metering_type=0 cooling_type=1 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=39.869999 min_design_mp=9.000000 critical_altitude=22966.000000 emergency_boost_type=2 emergency_boost_mp_offset=2.210000 emergency_boost_gain_offset=0.185178 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=11.000000 propeller_blades=2 propeller_moi=27.580348 beta_max=65.000000 beta_min=15.000000 min_gov_rpm=420.000000 prop_tc=0.010000 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=70.000000 beta_feather=88.500000 power_absorbed_cf=0.900000 defeathering_accumulators_available=0 prop_reverse_available=0.000000 minimum_on_ground_beta=1.000000 minimum_reverse_beta=-14.000000 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 [contact_points] point.0=1.0,-13.416667, 0.0, -2.40, 2165.354400,0.0,0.557255,12.0,0.292829,2.50,0.462118,3.0,3.0,0.0,0.0,0.0 point.1=1.0, 3.250, -5.916667,-6.70, 2165.354400,1.0,0.557255,0.0,0.965931,2.50,0.649925,5.50,6.50,2.0,0.0,0.0 point.2=1.0, 3.250, 5.916667,-6.70, 2165.354400,2.0,0.557255,0.0,0.965931,2.50,0.649925,5.50,8.0,3.0,0.0,0.0 point.3=2.0, 0.0, -18.50, 0.0, 1181.102400,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,5.0,0.0,0.0 point.4=2.0, 0.0, 18.50, 0.0, 1181.102400,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0 point.5=2.0,-14.166667,0.0, -0.50, 1181.102400,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0 point.6=2.0, 9.250, 0.0, -1.916667,1181.102400,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0 static_pitch=12.0 static_cg_height=4.8 gear_system_type=1 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.22,0.21 ;Percent per second [TailHook] tailhook_length=4 ;(feet) tailhook_position = -17.5, 0.0, -0.5 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust = 1.0 [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 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 [Views] eyepoint=-2.9,0.0,2.5 [LIGHTS] panel=0.00, 0.65, -0.50, fx_vclight [General] performance=Weight: 6531 lbs\nPower: 1350 hp\n7.5g Corner speed: 242 mph\nMax speed @ SL: 331 mph\nMax speed: 391 mph @ 22966 ft\nClimb rate: 4000 ft\/min @ 141 mph\nFlight Model By: Jerry Beckwith Visual model By: Ignacio Alfredo Mendive\n\n [fuel] Center1=0.010000,0.000000,0.000000,65.000000,0.000000 LeftMain=0.000000,-4.000000,-2.000000,25.000000,0.000000 RightMain=0.000000,4.000000,-2.000000,25.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=227.000000 wing_span=38.916667 wing_root_chord=5.833333 wing_dihedral=4.998779 wing_incidence=0.999756 wing_twist=0.000000 oswald_efficiency_factor=0.889527 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=27.000000 htail_span=15.583333 htail_pos_lon=-16.916667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=13.000000 vtail_span=4.110961 vtail_sweep=0.000000 vtail_pos_lon=-16.916667 vtail_pos_vert=5.833333 elevator_area=18.100000 aileron_area=21.900000 rudder_area=9.800000 elevator_up_limit=30.000000 elevator_down_limit=20.000000 aileron_up_limit=15.000000 aileron_down_limit=15.000000 rudder_limit=30.000000 elevator_trim_limit=18.000000 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=0.640889 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=15.000000,0.000000 flaps-position.2=30.000000,0.000000 flaps-position.3=45.000000,0.000000 [GeneralEngineData] engine_type=0 Engine.0=9.250000,0.000000,-0.083333 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=97.000000 full_flaps_stall_speed=77.600000 cruise_speed=250.000000 max_indicated_speed=484.000000 [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=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 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 [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 empty_weight=6331.000000 empty_weight_roll_MOI=5511.000000 empty_weight_pitch_MOI=6193.000000 empty_weight_yaw_MOI=10832.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=9496.500000