[fltsim.0] title=P40 Tomahawk sim=P40STUD model= panel= sound= texture= kb_checklists= ui_manufacturer=CURTISS ui_type=P-40B ui_variation=Tamahawk description=P-40B Tomahawk USAAC flown by George Welch, 1 of 2 P-40's that made it into the air during the attack at Pearl Harbor on Dec. 7th, 1941 atc_heavy=0 atc_id= atc_airline= atc_flight_number= [fltsim.1] title=P40B Flying Tiger sim=P40STUD model= panel= sound= texture=tiger kb_checklists= ui_manufacturer=CURTISS ui_type=P-40B Flying Tiger ui_variation=Flying Tiger description=Early Pacific Theatre of Operations "Screamin Demons 7th" of the 7th Air Force Based in Micronesia. 1941 atc_heavy=0 atc_id= atc_airline= atc_flight_number= [fltsim.2] title=P40 KittyHawk sim=P40STUD model= panel= sound= texture=Kitty kb_checklists= ui_manufacturer=CURTISS ui_type=P-40 KittyHawk ui_variation=KittyHawk description=Flown By the RAAF during the Defense of Australia from Japanese invading Forces in WW II atc_heavy=0 atc_id= atc_airline= atc_flight_number= [fltsim.3] title=P40N Pink Lady sim=P40STUD model= panel= sound= texture=Pink kb_checklists= ui_manufacturer=CURTISS ui_type=P-40N ui_variation=Pink Lady description=This Was actually Tan, only to be faded to Pink atc_heavy=0 atc_id= atc_airline= atc_flight_number= [WEIGHT_AND_BALANCE] empty_weight= 6300.000 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= 7856.000 empty_weight_roll_MOI= 6245.000 empty_weight_yaw_MOI= 10254.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 8238.800 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= 138.000 compression_ratio= 6.100 number_of_cylinders= 12 max_rated_rpm= 3000.000 max_rated_hp= 1300.000 fuel_metering_type= 0 cooling_type= 1 normalized_starter_torque= 0.035 turbocharged= 1 max_design_mp= 54.000 min_design_mp= 1.000 critical_altitude= 24000.000 emergency_boost_type= 3 emergency_boost_mp_offset= 10.000 emergency_boost_gain_offset= 0.800 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 ;Percent per second propeller_type= 0 propeller_diameter= 11.500 propeller_blades= 3 propeller_moi= 39.920 beta_max= 65.000 beta_min= 23.000 min_gov_rpm= 1800.000 prop_tc= 0.010 gear_reduction_ratio= 2.237 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, -15.710, 0.000, -3.105, 3200.000, 0.000, 0.380, 45.000, 0.450, 2.500, 0.900, 1.000, 4.000, 0.000, 200.000, 673.424 point.1= 1.000, 2.290, -4.420, -8.050, 2200.000, 1.000, 1.350, 0.000, 0.800, 2.500, 0.660, 5.500, 6.500, 2.000, 200.000, 721.524 point.2= 1.000, 2.290, 4.420, -8.050, 2200.000, 2.000, 1.350, 0.000, 0.800, 2.500, 0.660, 5.500, 5.000, 3.000, 200.000, 721.524 point.3= 2.000, 1.079, -19.300, 0.000, 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, 1.079, 19.300, 0.000, 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, -18.250, 0.000, -0.910, 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, -6.200, 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= 8.050 static_pitch= 12.300 gear_system_type=1 [Views] eyepoint=-2.80,0.0,1.80 [LIGHTS] panel=0.00, 0.45, -2.00, fx_vclight [General] performance=P-40F Specifications\nSpan\t37 ft 4 in\nLength\t33 ft 4 in\nHeight\t12 ft 4 in\nWing Area\t236 sq ft\nEmpty Weight 6,590 lb\nLoaded Weight 9,350 lb\nMax. Speed 364 mph\nCruise Speed 290 mph\nCeiling 33,500 ft\nRate of Climb 3,250 fpm\nRange 575 miles\nPowerplant Packard V-1650-1 of 1,300 hp atc_type= atc_model= [fuel] Center1= 1.000, 0.000, -1.000, 71.300, 0.000 Center2= -4.000, 0.000, 0.000, 68.700, 0.000 LeftMain= 0.000, -4.000, -1.000, 24.600, 0.000 RightMain= 0.000, 4.000, -1.000, 24.600, 0.000 External1= 0.000, 0.000, -4.000, 105.600, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area= 253.000 wing_span= 39.333 wing_root_chord= 6.417 wing_dihedral= 8.696 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= 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= 5.417, 0.000, 0.000 fuel_flow_scalar= 1.000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed= 81.000 full_flaps_stall_speed= 64.800 cruise_speed= 251.933 max_indicated_speed=740.000000 [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= 203.000 blowout-speed= 307.000 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= 30.000, 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