[fltsim.0] title=P47 Senta a Pua sim=P47DT model= panel= sound= texture=1 kb_checklists= description=FS2002\2004 P-47D Painted By Cristiano Magnani ui_manufacturer=Republic ui_type=1st Brazilian Fighter Squadron ui_variation=P-47D atc_heavy=0 atc_id= atc_airline= atc_flight_number= [General] atc_type= atc_model= performance=Engine: Pratt & Whitney R-2800-59\nHorsepower: 2000\/2430 in War Emergency setting\nPropeller: Curtis Electric C542S with 13' diameter\nSpan: 40' 9 5\/16''\nLength: 36' 1 3\/4''\nHeight: 14' 8 1\/16''\nWeight: 10,000 lbs empty, 17,500 lbs maximum\nSpeed: 426 mph @ 30,000feet\nCeiling: 42,000 feet\nRange: 1030 miles @ 10,000 feet\nArmament: Eight .50 calibre machine guns plus 2500 lbs ordnance\n [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 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] empty_weight=8873.000 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, -3.000, 0.000, 3.000 ;Moments of Inertia empty_weight_pitch_MOI=11059.000 empty_weight_roll_MOI=7243.000 empty_weight_yaw_MOI=14484.000 empty_weight_coupled_MOI=0.000 max_gross_weight=12259.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 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=155.560 compression_ratio=6.700 number_of_cylinders=18 max_rated_rpm=2700.000 max_rated_hp=2000.000 fuel_metering_type=2 cooling_type=0 normalized_starter_torque=0.035 turbocharged=1 max_design_mp=53.000 min_design_mp=1.000 critical_altitude=21500.000 emergency_boost_type=1 emergency_boost_mp_offset=10.000 emergency_boost_gain_offset=0.660 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=13.330 propeller_blades=3 propeller_moi=62.170 beta_max=65.000 beta_min=13.000 min_gov_rpm=1800.000 prop_tc=0.010 gear_reduction_ratio=2.000 fixed_pitch_beta=0.000 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 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.12,0.11 ;Percent per second [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 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=900.0 autothrottle_available=0 pitch_takeoff_ga=8.0 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 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=0, 0 Nav.1=1, 0, 0 Nav.2=0, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=0 [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [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, -18.000, 0.000, -3.700, 3200.000, 0.000, 0.500, 180.000, 0.250, 2.500, 0.900, 1.000, 4.000, 0.000, 0.000, 337.611 point.1=1.000, 1.800, -5.930, -8.500, 2200.000, 1.000, 1.350, 0.000, 0.540, 2.500, 0.760, 5.500, 4.500, 2.000, 0.000, 337.611 point.2=1.000, 1.800, 5.930, -8.500, 2200.000, 2.000, 1.350, 0.000, 0.540, 2.500, 0.760, 5.500, 4.500, 3.000, 0.000, 337.611 point.3=2.000, 0.000, -20.000, -1.250, 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, 20.000, -1.250, 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, -20.250, 0.000, -1.660, 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, 5.410, 0.000, -3.500, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.7=2.000, 0.000, -5.430, -3.750, 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.8=2.000, 0.000, 5.430, -3.750, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 static_cg_height=7.000 static_pitch=13.900 gear_system_type=1 [Views] eyepoint=-6.2, 0.00, 3.55 //(feet) longitudinal, lateral, vertical distance from reference datum [LSO] LSOAdjustSpeed=1.2 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing panel=0.00, 0.45, -2.00, fx_vclight [fuel] Center1=-1.940, 0.000, -0.500, 187.000, 0.000 Center2=-1.940, 0.000, -0.500, 50.000, 0.000 LeftMain=-0.970, -12.250, -1.610, 62.000, 0.000 RightMain=-0.970, 12.250, -1.610, 62.000, 0.000 External1=1.940, 0.000, -3.870, 175.000, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=314.000 wing_span=41.000 wing_root_chord=7.833 wing_dihedral=13.596 wing_incidence=1.000 wing_twist=0.000 oswald_efficiency_factor=0.699 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=24.000 htail_span=11.000 htail_pos_lon=-18.833 htail_pos_vert=0.000 htail_incidence=-1.000 htail_sweep=0.000 vtail_area=15.000 vtail_span=4.416 vtail_sweep=0.000 vtail_pos_lon=-18.833 vtail_pos_vert=0.583 elevator_area=13.000 aileron_area=20.400 rudder_area=13.060 elevator_up_limit=26.001 elevator_down_limit=26.001 aileron_up_limit=21.497 aileron_down_limit=20.346 rudder_limit=28.997 elevator_trim_limit=19.996 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=0 Engine.0=7.000, 0.000, 0.000 fuel_flow_scalar=1.000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=65.000 full_flaps_stall_speed=52.000 cruise_speed=288.725 max_indicated_speed=760.500000 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=100.000000,1000.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0 [Flaps.0] type=1 span-outboard=0.125 extending-time=5.000 system_type=0 damaging-speed=201.000 blowout-speed=305.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=10.000, 0.000 flaps-position.2=20.000, 0.000 flaps-position.3=35.000, 0.000 flaps-position.4=40.000, 0.000 flaps-position.5=55.000, 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 [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 [fltsim.1] title=P47 Senta a Pua sim=P47DT model= panel= sound= texture=1 kb_checklists= description=FS2002\/2004 P-47D-25 model\nBy JRLucariny\nhttp:\/\/lucariny.sites.uol.com.br\nA P-47D-25 assigned to the 1st Grupo de Caça, Força Aerea Brasileira, and attached to the 350th Fighter Group in Italy during 1944. ui_manufacturer=Republic ui_type=1st Brazilian Fighter Squadron ui_variation=P-47 Cris atc_heavy=0 atc_id= atc_airline= atc_flight_number=