[fltsim.0] title=F4F-4 Wildcat sim=F4F4_Wildcat model= panel=//F35 sound= texture= KB_checklists=f4f4_wildcat_check ui_manufacturer=Grumman ui_type=F4F-4 Wildcat ui_variation=Navy description=This tubby little carrier fighter was easy, forgiving, and even fun to fly. It was Grumman's first modern all-metal monoplane fighter. The Wildcat was stoutly constructed, well-armored, and well-armed, with the same six .50-caliber Brownings carried by the Hellcat, Corsair, and Mustang. While its greater weight and less efficient wing were liabilities in a dogfight, the Wildcat's larger, more powerful engine combined with its best traits to give the Wildcat superior diving ability. [WEIGHT_AND_BALANCE] empty_weight = 5785 // (pounds) reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 170, -3.0, 0.0, 3.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 5365.14 empty_weight_roll_MOI = 4056.82 empty_weight_yaw_MOI = 7615.70 empty_weight_coupled_MOI=0.00 max_gross_weight=8932.500 [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=130.700 compression_ratio=6.700 number_of_cylinders=14 max_rated_rpm=2700.00 max_rated_hp=1200.00 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.03500 turbocharged=1 max_design_mp=46.50 min_design_mp=1.00 critical_altitude=17000.00 emergency_boost_type=0 emergency_boost_mp_offset=6.00 emergency_boost_gain_offset=0.3900 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.20 idle_rpm_mechanical_efficiency_scalar=1.00 max_rpm_friction_scalar=1.00 idle_rpm_friction_scalar=0.700 [propeller] thrust_scalar = 1.0 propeller_type=0 propeller_diameter=10.83300 propeller_blades=3 propeller_moi=33.3700 beta_max=53.500 beta_min=18.500 min_gov_rpm=1800.00 prop_tc=0.0100 gear_reduction_ratio=1.7000 fixed_pitch_beta=0.00 low_speed_theory_limit=80.00 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.00 beta_feather=0.00 power_absorbed_cf=0.00 defeathering_accumulators_available=0 prop_reverse_available=0.00 minimum_on_ground_beta=0.00 minimum_reverse_beta=0.00 [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;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, -16.80, 0.00, -3.35, 3200, 0, 0.40,180.0, 0.30, 2.5, 0.90, 0.0, 0.0, 0, 0, 0 point.1=1, 1.40, -3.91, -6.65, 2200, 1, 1.13, 0.0, 0.45, 2.5, 0.83, 4.5, 4.5, 2, 0, 235 point.2=1, 1.40, 3.91, -6.65, 2200, 2, 1.13, 0.0, 0.45, 2.5, 0.83, 4.5, 4.5, 3, 0, 235 point.3=2, 0.00,-20.00, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 point.4=2, 0.00, 20.00, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 point.5=2, -16.25, 0.00, -1.66, 2400, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 point.6=2, 2.41, 0.00, -2.08, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 static_cg_height = 5.85 //(feet) altitude of CG when at rest (altitude when loaded on ground) static_pitch = 10.69 //degrees (pitch when loaded on ground) gear_system_type=2 [TailHook] tailhook_length=3.41 ;(feet) tailhook_position = -18.9, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust = 1.0 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.125 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=11 // degrees, KIAS flaps-position.2=22 // degrees, KIAS flaps-position.3=32 // degrees, KIAS flaps-position.4=43 // degrees, KIAS damaging-speed=165 // KIAS blowout-speed=250 // KIAS [Views] eyepoint= -3.1, 0.00, 4.0 //(feet) longitudinal, lateral, vertical distance from reference datum [LIGHTS] panel=0.00, 0.70, -0.80, fx_vclight light.0=3, 0.0, -19.30, 0.70, fx_navred light.1=3, 0.0, 19.30, 0.70, fx_navgre light.2=3,-20.8, 0.00,-0.50, fx_navwhi [General] performance=Weight: 5,785 \/ 7,951 lbs\nEngine: Pratt & Whitney R-1830-86\nTwin Wasp 14-cyl. radial, \n1,200 hp\nMax speed: 318 mph @ 19,400 ft\nCeiling: 34,900 ft\nInitial climb rate: 1,950 ft\/min\nRange: 770 miles\n [fuel] Center1= -1.500, 0.00, -1.20, 117.00, 0.00 External1=0.00, -5.10, -2.50, 58.00, 0.00 External2=0.00, 5.10, -2.50, 58.00, 0.00 fuel_type=1 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=260.00 wing_span=38.00 wing_root_chord=8.40 wing_dihedral=6.300659 wing_incidence=0.999756 wing_twist=0.00 oswald_efficiency_factor=0.699497 wing_winglets_flag=0 wing_sweep=0.00 wing_pos_apex_lon=2.00 wing_pos_apex_vert=0.0 htail_area=24.00 htail_span=13.40 htail_pos_lon=-16.50 htail_pos_vert=1.60 htail_incidence=-0.999756 htail_sweep=15.00 vtail_area=15.00 vtail_span=4.20 vtail_sweep=15.00 vtail_pos_lon=-16.00 vtail_pos_vert=2.20 elevator_area=13.00 aileron_area=20.400 rudder_area=13.0600 elevator_up_limit=26.000825 elevator_down_limit=26.000825 aileron_up_limit=21.497376 aileron_down_limit=20.345731 rudder_limit=28.997394 elevator_trim_limit=19.996227 spoiler_limit=0.00 spoilerons_available=0 aileron_to_spoileron_gain=0.00 min_ailerons_for_spoilerons=0.00 min_flaps_for_spoilerons=0.00 [brakes] toe_brakes_scale=0.48420 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.00 flap_limit_power=0.00 flap_limit_idle=0.00 [GeneralEngineData] engine_type=0 Engine.0=7.00,0.00,0.00 fuel_flow_scalar=1.00 min_throttle_limit=0.00 [Reference Speeds] flaps_up_stall_speed=81.00 full_flaps_stall_speed=64.800 cruise_speed=152.0 max_indicated_speed=460.500 [keyboard_response] elevator=150.00,250.00 aileron=150.00,250.00 rudder=150.00,250.00 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=700.00 autothrottle_available=0 pitch_takeoff_ga=8.00 max_pitch=10.00 max_pitch_acceleration=1.00 max_pitch_velocity_lo_alt=2.00 max_pitch_velocity_hi_alt=1.500 max_pitch_velocity_lo_alt_breakpoint=20000.00 max_pitch_velocity_hi_alt_breakpoint=28000.00 max_bank=25.00 max_bank_acceleration=1.800 max_bank_velocity=3.00 max_throttle_rate=0.100 nav_proportional_control=9.00 nav_integrator_control=0.2500 nav_derivative_control=0.00 nav_integrator_boundary=2.500 nav_derivative_boundary=0.00 gs_proportional_control=9.5200 gs_integrator_control=0.2600 gs_derivative_control=0.00 gs_integrator_boundary=0.700 gs_derivative_boundary=0.00 yaw_damper_gain=0.00 [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