[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