[fltsim.0] title=F-11 sim=F-11 model= panel= sound= texture= kb_checklists= description=En 1932 cuando el Perú invadió el sur de Colombia el gobierno nacional tubo que recurrir al gigante del norte para que nos proporcionara material bélico para poder hacerle frente a la nueva amenaza. Así en 1932 llegaron 30 aviones Hawk F-11 C-2 los cuales fueron numerados desde el FAC 800 hasta el 829. Tuvieron grandes actuaciones sobre el 14 de febrero de 1933 cuando 7 Hawk participaron en la acción de Tarapacá. Por desgracia fue un Hawk el que causo la desgracia de Santa Ana, cuando el hawk de Abadía al salir de un royo se precipito contra el suelo luego de golpear el palco presidencial, dejando 93 muertos y 201 heridos. Los Hawk estuvieron en servicio hasta 1945, año en el que fueron dados de baja definitivamente. ui_manufacturer=Curtiss ui_type=Hawk F-11 C-2 ui_variation=Fuerza Aérea Colombiana atc_heavy=0 atc_id=814 atc_airline=Fuerza Aérea Colombiana atc_flight_number=Fac [General] performance=Largo:\t\t7.62 m\nAlto:\t\t3.23 m\nEnvergadura:\t9.60 m\n\nMotor:\tWright Cyclone R-1820-72\nVelocidad maxima:\t172 nudos\nVelocidad crucero:\t150 nudos\n\nPeso Max despegue: 2.104 Kg\nTecho:\t24.500 pies\nRadio de accion:\t280 millas\n\nArmamento: 2 ametralladoras .30\nbombas de 500 lb en los planos.\n\nModelo, textura y panel: Eduardo Fadul\neduardofadul@yahoo.com atc_type=Curtiss atc_model=F-11 [contact_points] //0 Class //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) point.0= 1.000, -11.110, 0.000, -2.050, 3200.000, 0.000, 0.300, 180.000, 0.300, 2.500, 0.900, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, 0.568, -4.000, -5.190, 2200.000, 1.000, 1.360, 0.000, 0.450, 2.500, 0.830, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, 0.568, 4.000, -5.190, 2200.000, 2.000, 1.360, 0.000, 0.450, 2.500, 0.830, 0.000, 0.000, 3.000, 0.000, 0.000 point.3= 2.000, 0.000, -15.750, 3.670, 1200.000, 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, 0.000, 15.750, 3.670, 1200.000, 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, -17.400, 0.000, 0.280, 2400.000, 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, 4.670, 0.000, -2.190, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_cg_height = 3.370 static_pitch = 15.120 gear_system_type=1 [Views] eyepoint=-0.974409, 0, 2.8644357 //(feet) longitudinal, lateral, vertical distance from reference datum [LIGHTS] //Position Order: Z, X, Y //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 9=logo light.0=4, -0.974409, 0.0, 2.644357, fx_vclight , // cockpit [WEIGHT_AND_BALANCE] empty_weight= 3524.000 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= 170.000, -6.000, 0.000, 1.500 ;Moments of Inertia empty_weight_pitch_MOI= 2400.910 empty_weight_roll_MOI= 1869.540 empty_weight_yaw_MOI= 3459.640 empty_weight_coupled_MOI= 0.000 max_gross_weight= 5541.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [piston_engine] power_scalar=1.000 cylinder_displacement= 202.538 compression_ratio= 6.400 number_of_cylinders= 9 max_rated_rpm= 2200.000 max_rated_hp= 785.000 fuel_metering_type= 0 cooling_type= 0 normalized_starter_torque= 0.035 turbocharged= 1 max_design_mp= 39.000 min_design_mp= 1.000 critical_altitude= 4166.667 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [propeller] thrust_scalar=1.000 propeller_type= 0 propeller_diameter= 9.843 propeller_blades= 3 propeller_moi= 22.500 beta_max= 45.000 beta_min= 25.000 min_gov_rpm= 1400.000 prop_tc= 0.010 gear_reduction_ratio= 1.710 fixed_pitch_beta= 22.500 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 [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 [fuel] Center1= 0.600, 0.000, 0.000, 38.300, 0.000 LeftMain= -1.600, 2.300, -1.200, 50.200, 0.000 RightMain= -1.600, -2.300, -1.200, 50.200, 0.000 External1= -2.100, 0.000, -3.300, 87.200, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area= 225.000 wing_span= 31.500 wing_root_chord= 4.917 wing_dihedral= 0.000 wing_incidence= 0.511 wing_twist= 0.511 oswald_efficiency_factor= 1.077279 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 18.000 htail_span= 11.833 htail_pos_lon= -11.917 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 7.000 vtail_span= 3.017 vtail_sweep= 0.000 vtail_pos_lon= -12.500 vtail_pos_vert= 2.083 elevator_area= 14.155 aileron_area= 14.594 rudder_area= 13.796 elevator_up_limit= 26.001 elevator_down_limit= 26.001 aileron_up_limit= 21.497 aileron_down_limit= 20.346 rudder_limit= 23.997 elevator_trim_limit= 19.996 spoiler_limit= 0.573 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [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 [GeneralEngineData] engine_type= 0 Engine.0= 5.833, 0.000, 0.000 fuel_flow_scalar= 1.000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed= 74.000 full_flaps_stall_speed= 59.200 cruise_speed= 232.601 max_indicated_speed=760.500000 [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=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0 [Flaps.0] type=0 span-outboard=0.500000 extending-time=5.000000 system_type=1 flaps-position.0=0.000000,0.000000 flaps-position.1=13.750987,0.000000 flaps-position.2=27.501974,0.000000 flaps-position.3=41.252961,0.000000 flaps-position.4=55.003948,0.000000
