[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