[fltsim.0] title=P-26A sim=P-26A model= panel= sound= texture= description=The 1934 Boeing P-26 "Peashooter" was the first all-metal monoplane fighter adopted by the U.S. Army Air Corps. On January 10, 1934, the first production model took to the air. This model had no flaps and lands hot. A P-47 fighter pilot in WW 2 said that when he saw three P-26's land he knew he must become a pilot. ui_manufacturer=Boeing ui_type=P-26A Peashooter ui_variation= atc_heavy=0 atc_id=P-26A 8 atc_airline=Army Air Corps atc_flight_number=8 editable=1 performance=Maximum Speed\t\n203 kts 234 mph\t377 km\/h\n\nCruise Speed\t\n152 kts 175 mph \282 km\/h\n\nEngine\t\nPratt & Whitney R-1340-27 Wasp [WEIGHT_AND_BALANCE] max_gross_weight=5200.000 empty_weight=2995.000 reference_datum_position=0.00, 0.000, 0.700 empty_weight_CG_position=0.500, 0.000, 0.700 max_number_of_stations=50 ;Moments of Inertia empty_weight_pitch_MOI=6000.000 empty_weight_roll_MOI=1177.000 empty_weight_yaw_MOI=8460.000 empty_weight_coupled_MOI=0.000 CG_forward_limit=0.000 CG_aft_limit=1.000 station_load.0=0.000000,0.000000,0.000000,0.000000 [flight_tuning] cruise_lift_scalar=1.201 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.300 roll_stability=1.000 yaw_stability=1.400 elevator_trim_effectiveness=1.601 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type=0 Engine.0=6.300, 0.000, 0.000 fuel_flow_scalar=1.000 [piston_engine] power_scalar=1.000 cylinder_displacement=130.700 compression_ratio=6.700 number_of_cylinders=9 max_rated_rpm=2400.000 max_rated_hp=507.000 fuel_metering_type=2 cooling_type=0 normalized_starter_torque=0.2 turbocharged=0 max_design_mp=0.000 min_design_mp=0.000 critical_altitude=0.000 emergency_boost_type=0 emergency_boost_mp_offset=0.000 emergency_boost_gain_offset=0.000 fuel_air_auto_mixture=1 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=1.300 propeller_type=1 propeller_diameter=7.000 propeller_blades=2 propeller_moi=15.000 //beta_max=53.500 //beta_min=18.500 //min_gov_rpm=1800.000 prop_tc=0.020 gear_reduction_ratio=1.778 fixed_pitch_beta=18.000 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 beta_max=53.500 beta_min=18.500 min_gov_rpm=1800.000 [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) max_number_of_points=9 point.0=1.000, -16.917, 0.000, -3.100, 1181.102, 0.000, 0.250, 30.000, 0.096, 2.500, 0.990, 3.500, 3.500, 0.000, 0.000, 0.000 point.1=1.000, 2.083, -3.850, -6.617, 1574.803, 1.000, 0.530, 0.000, 0.469, 2.500, 0.991, 4.700, 4.700, 2.000, 0.000, 0.000 point.2=1.000, 2.083, 3.850, -6.617, 1574.803, 2.000, 0.530, 0.000, 0.469, 2.500, 0.991, 5.200, 5.200, 3.000, 0.000, 0.000 point.3=2.000, 0.000, -18.000, -1.367, 1574.803, 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, 18.000, -1.367, 1574.803, 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, -19.667, 0.000, 0.217, 1574.803, 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, 10.333, 0.000, -0.700, 1574.803, 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, -16.333, 0.000, 6.133, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.8=2.000, -1.000, 0.000, -2.533, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 static_pitch=15.000 static_cg_height=5.918 [Views] eyepoint=-3.1, 0.00, 3.17 //(feet) longitudinal, lateral, vertical distance from reference datum [LIGHTS] panel=0.00, 0.70, -0.80, fx_vclight [fuel] Center1=-1.500, 0.000, -1.200, 117.000, 0.000 External1=0.000, -5.100, -2.500, 58.000, 0.000 External2=0.000, 5.100, -2.500, 58.000, 0.000 fuel_type=1.000 number_of_tank_selectors=1 [airplane_geometry] wing_area=294.000 wing_span=28.000 wing_root_chord=6.000 wing_dihedral=6.301 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=1.500 wing_pos_apex_vert=-1.589 htail_area=18.120 htail_span=9.500 htail_pos_lon=-12.700 htail_pos_vert=0.000 htail_incidence=1.000 htail_sweep=0.000 vtail_area=15.000 vtail_span=4.800 vtail_sweep=0.000 vtail_pos_lon=-14.310 vtail_pos_vert=0.800 elevator_area=9.500 aileron_area=9.000 rudder_area=6.750 elevator_up_limit=20.001 elevator_down_limit=19.001 aileron_up_limit=21.497 aileron_down_limit=20.346 rudder_limit=18.997 elevator_trim_limit=16.001 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 [Reference Speeds] flaps_up_stall_speed=45.000 full_flaps_stall_speed=45.000 cruise_speed=175.000 [keyboard_response] elevator=350.000, 500.000 aileron=450.000, 1000.000 rudder=200.000, 1000.000 [autopilot] autopilot_available=0 flight_director_available=0 default_vertical_speed=700.000 autothrottle_available=0 pitch_takeoff_ga=8.000 [direction_indicators] direction_indicator.0=1,0 [Flaps.0] type=0 span-outboard=0.000 extending-time=0.100 system_type=0 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=0.000 drag_scalar=0.000 pitch_scalar=0.000 [General] performance=\n [FlightZip] Hide0=
