[fltsim.0]
title=ARA A-4Q Skyhawk 
sim=Marinha_do_Brasil_AF1_A4
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=McDonnell Douglas
ui_type=A-4Q 
ui_variation=Armada Argentina
visual_damage=1
description=Aeronave perteneciente a la Tercera Escuadrilla Aeronaval de Caza y Ataque. Su asiento natural era la Base Aeronaval Comandante Espora, Bahía Blanca.- Como perteneciente al grupo aeronaval embarcado, su destino era a bardo del portaaviones A.R.A. "25 de Mayo".- \nModelo modificado por CARLOS JOSÉ LAGIOIA, diciembre 24 de 2.003, Quilmes, Buenos Aires, República Argentina.-
atc_heavy=0
atc_id=
atc_airline=A.R.A.
atc_flight_number=301

[General]
performance=TIPO: Avión de ataque y bombardeo liviano, monoplaza.-\nDIMENSIONES: Largo 3 m.- Altura 4,57 m.- Envergadura: 8,38 m.- Superficie alar: 24,16 m\/cuad.\nPESOS: Vacío: 4.150 Kg.- Máximo  al decolaje: 10.200 Kg.-\nPERFOMANCE: Velocidad máxima: 1.065 Km\/h.- Velocidad de aterrizaje: 230  Km\/h.-\nALCANCE: A velocidad y nivel de crucero 2.000 Km.- Con tanques suplementarios 3.200 Km.-\nARMAMENTO: 2 cañones de 20 mm. con 100 cartuchos cada uno.- Carga externa: 2.000 kg.-
atc_type=MCDONNELDOUGLAS
atc_model=A-4Q

[SMOKESYSTEM]
smoke.0=0.00, -0.70, 1.40, fx_smoke_rx

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1
Nav.2=1
Adf.1=1
Transponder.1=1
Marker.1=1

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[Views]
eyepoint=8.5, 0, 3.2

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -6, -14, -1.5, fx_navredm ,
light.1=3, -6,  14, -1.5, fx_navgrem ,
light.2=2, -2.69,   0.00, 4.3, fx_beaconb ,
light.3=4, 5,   0.00,  3.50, fx_vclight ,
light.4=3, -5,  3.6, -3.2, fx_navredm ,

[flight_tuning]
cruise_lift_scalar=0.501
pitch_stability=0.65
roll_stability=2.002
yaw_stability=1.409
parasite_drag_scalar=0.65
induced_drag_scalar=1.07
elevator_effectiveness=0.6
aileron_effectiveness=2.002
rudder_effectiveness=1.000
elevator_trim_effectiveness=3.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[contact_points]
point.0= 1.000, 16.667, 0.000, -8.000, 1574.803, 0.000, 0.582, 42.000, 0.194, 2.500, 0.921, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, -1.250, -5.583, -6.750, 1574.803, 1.000, 0.582, 0.000, 0.301, 2.500, 0.689, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -1.250, 5.583, -6.750, 1574.803, 2.000, 0.582, 0.000, 0.301, 2.500, 0.689, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -8.000, -13.833, -2.500, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -8.000, 13.833, -2.500, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -18.667, 0.000, -2.167, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 18.583, 0.000, -1.667, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 3.862
static_cg_height= 5.668
[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight= 9000.000
empty_weight_roll_MOI= 16000.000
empty_weight_pitch_MOI= 15000.000
empty_weight_yaw_MOI= 37000.000
empty_weight_coupled_MOI= 1300.000
max_gross_weight= 11881.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[fuel]
LeftMain= 0.000, 0.000, 0.000, 115.000, 0.000
LeftAux= 0.000, -10.917, 0.000, 100.000, 0.000
RightMain= 0.000, 0.000, 0.000, 115.000, 0.000
RightAux= 0.000, 10.917, 0.000, 100.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1
[airplane_geometry]
wing_area= 143.000
wing_span= 27.500
wing_root_chord= 5.250
wing_dihedral= 1.500
wing_incidence= -0.659
wing_twist= -1.000
oswald_efficiency_factor= 0.936
wing_winglets_flag= 1
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 30.000
htail_span= 12.000
htail_pos_lon= -20.000
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 40.000
vtail_span= 7.211
vtail_sweep= 0.000
vtail_pos_lon= -12.167
vtail_pos_vert= 5.833
elevator_area= 7.500
aileron_area= 5.720
rudder_area= 6.800
elevator_up_limit= 27.502
elevator_down_limit= 20.626
aileron_up_limit= 27.502
aileron_down_limit= 27.502
rudder_limit= 23.491
elevator_trim_limit= 19.481
spoiler_limit= 59.989
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
[GeneralEngineData]
engine_type= 1
Engine.0= -0.833, 0.000, 0.000
fuel_flow_scalar= 1.000
[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 11.409
rated_N2_rpm= 29920.000
static_thrust= 9507.800
afterburner_available= 0
reverser_available= 0
[Reference Speeds]
flaps_up_stall_speed= 90.000
full_flaps_stall_speed= 72.000
cruise_speed= 489.776
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[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
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 13.331, 0.000
flaps-position.2= 26.662, 0.000
flaps-position.3= 39.992, 0.000