[fltsim.0]
title=FMA IA-58 Pucará
sim=FMA IA-58 Pucará
model=
panel=
sound=
texture=
checklists=
description=Avión de combate de la Fuerza Aérea Argentina.  Para apoyo a fuerzas terrestres y exploración.
ui_manufacturer=FMA
ui_type=IA-58 Pucará
ui_variation=FAA
visual_damage=1
atc_id=A557

[General]
performance=País de fabricación:  Argentina\nFabricante:  FMA\nEnvergadura:  14,25 m\nLongitud:  14,50 m \nPeso Vacío:  4.000 kg\nPeso máx. decolaje:  6.800 kg \nPlanta motriz y potencia:\n2 Turbomeca Astazou 965 HP c\/u \nVelocidad máxima:  500 km\/h \nVelocidad crucero:  480 km\/h \nAlcance:  700 km \nArmamento: \n4 ametralladoras de 7.62 mm \n2 cañones de 20 mm \n3 fijaciones para 1500 kg de armas en total \n\n\n\n

[forcefeedback]
stick_shaker_magnitude=5000		; 0 - 10000
stick_shaker_direction=0		; 0 - 35999 degrees
stick_shaker_period=111111		; in microseconds
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=9000		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=2700		; 0 - 10000
gear_bump_right_direction=27000		; 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

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=8626.000000
empty_weight_roll_MOI=16183.000000
empty_weight_pitch_MOI=20179.000000
empty_weight_yaw_MOI=34865.000000
empty_weight_coupled_MOI=1300.000000

[fuel]
LeftMain=0.000000,-10.000000,0.000000,195.000000,0.000000
RightMain=0.000000,10.000000,0.000000,195.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=293.000000
wing_span=47.666667
wing_root_chord=6.166667
wing_dihedral=3.999023
wing_incidence=-0.494385
wing_twist=3.999023
oswald_efficiency_factor=2.347381
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=90.000000
htail_span=18.416667
htail_pos_lon=-24.583333
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=52.000000
vtail_span=8.221922
vtail_sweep=0.000000
vtail_pos_lon=-21.500000
vtail_pos_vert=5.833333
elevator_area=22.500000
aileron_area=11.720000
rudder_area=8.840000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0=1.000000,8.250000,0.000000,-6.500000,1574.803150,0.000000,0.577913,35.940000,1.003357,2.500000,0.353920,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,-4.000000,-6.833333,-6.166667,1574.803150,1.000000,0.577913,0.000000,0.539850,2.500000,0.839128,5.000000,5.000000,2.000000,0.000000,0.000000
point.2=1.000000,-4.000000,6.833333,-6.166667,1574.803150,2.000000,0.577913,0.000000,0.539850,2.500000,0.839128,5.000000,5.000000,3.000000,0.000000,0.000000
point.3=2.000000,-1.916667,-23.500000,1.416667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-1.916667,23.500000,1.416667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-28.666667,0.000000,2.833333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,14.500000,0.000000,0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.000000
static_cg_height=5.668066

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=4.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=13.330818,0.000000
flaps-position.2=26.661636,0.000000
flaps-position.3=39.992454,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=9.500000,-8.500000,-0.166667
Engine.1=9.500000,8.500000,-0.166667
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=1.726200
rated_N2_rpm=29920.000000
static_thrust=1438.500000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=102.000000
full_flaps_stall_speed=81.600000
cruise_speed=280.002395

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=6.792364,0.000000,5.126312

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=3,0