[fltsim.0] title=VMF 211 F4F3 Wildcat sim=F4VF72 model= panel= sound= texture= kb_checklists= description=FS2002\/2004 FSDS V2 Model\nby JRLucariny\nhttp:\/\/lucariny.sites.uol.com.br\nThis F4F-3 Wildcat of VMF 211 (Wake Island Avengers) carries the early war color scheme of sprayed Silver/Blue lacquer fuselage and wings. Wake Island Was Lost to the Enemy Due to Command errors and Being Fooled into believing the Island was completely surrounded. ui_manufacturer=Grumman ui_type=Grumman F4F-3 Wildcat ui_variation= atc_heavy=0 atc_id= atc_airline= atc_flight_number= [WEIGHT_AND_BALANCE] empty_weight= 3704.000 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= 3673.150 empty_weight_roll_MOI= 2788.860 empty_weight_yaw_MOI= 5226.170 empty_weight_coupled_MOI= 0.000 max_gross_weight= 5229.400 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.12,0.11 ;Percent per second [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= 125.857 compression_ratio= 7.200 number_of_cylinders= 14 max_rated_rpm= 2600.000 max_rated_hp= 1050.000 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 0.035 turbocharged= 1 max_design_mp= 39.000 min_design_mp= 1.000 critical_altitude= 14400.000 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= 6.000 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= 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 [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 [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, -20.210, 0.000, -1.500, 3200.000, 0.000, 0.300, 180.000, 0.400, 2.500, 0.800, 7.500, 5.000, 0.000, 0.000, 0.000 point.1= 1.000, 1.451, -5.760, -4.800, 2200.000, 1.000, 1.050, 0.000, 0.500, 2.500, 0.830, 2.500, 4.000, 2.000, 0.000, 0.000 point.2= 1.000, 1.451, 5.760, -4.800, 2200.000, 2.000, 1.050, 0.000, 0.500, 2.500, 0.830, 2.500, 8.250, 3.000, 0.000, 0.000 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, 1.000, 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, 2.410, 0.000, -2.080, 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= 4.693 static_pitch= 11.770 gear_system_type=1 [TailHook] tailhook_length=4 ;(feet) tailhook_position=-17.5, 0.0, -0.5 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [Views] eyepoint=-1.5,0.0000,3.25 [LIGHTS] panel=0.00, 0.35, -0.80, fx_vclight [General] performance=Specifications (F4F):\nEngine: 1200hp Pratt & Whitney R-1830-36 Twin Wasp, 14-cylinder radial piston engine\nWeight: Empty 5760 lbs, Maximum Takeoff 7950 lbs.\nWing Span: 38ft. 0 in.\nLength: 28ft. 9in.\nHeight: 9ft. 2.5in.\nPerformance:\nMaximum Speed at 20,000ft: 318mph\nCruising Speed: 155mph\nService Ceiling: 39,500ft\nInitial Climb Rate: 1950 feet\/min.\nRange: 770 miles\nArmament:\n Six 12.7-mm (0.50 in) Browning machine guns (FM-2 had four guns)\s\nTwo 100-lb bombs (FM-2 could carry two 250-lb bombs).\nNumber Built: 7,885 (All production variants)\n atc_type= atc_model= [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= 228.000 wing_span= 39.417 wing_root_chord= 6.417 wing_dihedral= 6.998 wing_incidence= 1.000 wing_twist= 0.000 oswald_efficiency_factor= 0.697 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= 0.000 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= 6.250, 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= 245.912 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 [direction_indicators] direction_indicator.0=1,0 [Flaps.0] type= 1 span-outboard= 0.125 extending-time= 5.000 system_type= 0 damaging-speed= 172.000 blowout-speed= 260.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 14.000, 0.000 flaps-position.2= 28.000, 0.000 flaps-position.3= 42.000, 0.000 flaps-position.4= 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=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
