[fltsim.0] title=Pitts_S2B sim=Pitts_S2B model= panel= sound= texture= kb_checklists= description=Piits Special S-2B manufactured by Aviat Aircraft Inc USA is a special designed aircraft for acrobatic performance. \nThe two-place Pitts Special S-2B can be flown competitively in unlimited class competition.\nIt is ideal for advanced aerobatic instruction and is most popular model.\nThe S-2B is obviously capable of highly advanced maneuvers, yet is easy enough to fly for\npilots just beginning their aerobatic training.\n ÈZòsêpÌX|[c@Å·B S-2BÍxÈ}j [oð±È·«\ðàÁĨèA³·ÊÌ£ZïÅàòs·é±Æª ū龯ÅÈAGAo`bNg[jOÌSÒÉàeÕÉòsÅ«éæ¤ÉÈÁÄ ¢Ü·B úPittsÍPÀÌS1ŵ½ªA»ÝÍ¡ÀÌS2V[YÉÈèA»ÝÅÍS-2B̶YðI¹ µS-2CªÅV@íÆÈÁĢܷB GWÉÍACJ~O@AEIO-540-D4A5@ ½Îü6C@260nÍ/2700RPMðÚB vyÍAn[cF@HC-C3YR-1A/7690C@è¬R|WbgRu[h ui_manufacturer=Aviat Aircraft Inc. ui_type=PS2 ui_variation=PS2B atc_heavy=0 atc_id=JA11AR atc_airline= atc_flight_number= [General] atc_type=PITTS atc_model=PTS2 editable=1 performance=Specification\n Length @17 feet 9 inch\n Wing span @20 feet\n Height @6 feet 5 inch\n Wing Area 127.5 sq feet\n Weight @ 1,155 lb\n Seats 2 tandem\n Engine @Lycoming@AEIO-540-D4A5\n @@@@260HP^2700RPM\n Propeller Hartzell HC-C3YR-1A\/7690C\n constant speed, composite three-blade\n [WEIGHT_AND_BALANCE] max_gross_weight= 2095.000 empty_weight= 1155.000 reference_datum_position= 1.800, 0.000, 0.000 empty_weight_CG_position= -1.400, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, -5.800, 0.000, 1.000 ;Moments of Inertia empty_weight_pitch_MOI= 665.000 empty_weight_roll_MOI= 408.000 empty_weight_yaw_MOI= 300.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [electrical] max_battery_voltage=12.0 generator_alternator_voltage=13.8 max_generator_alternator_amps=40.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=0, 10, 9.5 avionics=1, 5 , 9.5 additional_system=0, 20, 9.5 marker_beacon=1, 2 , 9.0 fuel_pump=0, 5 , 9.0 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=0.712 aileron_effectiveness=1.281 rudder_effectiveness=1.312 pitch_stability=1.011 roll_stability=0.800 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type= 0 Engine.0= 0.300, 0.000, 1.000 fuel_flow_scalar= 1.000 min_throttle_limit=0.000000 [piston_engine] power_scalar=1.345 cylinder_displacement= 90.300 compression_ratio= 8.700 number_of_cylinders= 6 max_rated_rpm= 2700.000 max_rated_hp= 300.000 fuel_metering_type= 2 cooling_type= 0 normalized_starter_torque= 0.300 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= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=0.762 idle_rpm_friction_scalar=1.000 [propeller] thrust_scalar=1.101 propeller_type= 0 propeller_diameter= 6.200 propeller_blades= 3 propeller_moi= 5.900 beta_max= 34.000 beta_min= 17.000 min_gov_rpm= 500.000 prop_tc= 0.100 gear_reduction_ratio= 1.000 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 //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 [contact_points] point.0= 1.000, -14.300, 0.000, -1.700, 1377.950, 0.000, 0.512, 30.000, 0.300, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, -0.050, -2.920, -4.200, 1968.500, 1.000, 0.512, 0.000, 0.400, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, -0.050, 2.920, -4.200, 1968.500, 2.000, 0.512, 0.000, 0.400, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000 point.3= 2.000, -0.100, -12.250, -1.170, 787.400, 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, -0.100, 12.250, -1.170, 787.400, 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, -14.100, 0.000, 4.330, 787.400, 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, 3.370, 0.000, -1.830, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 10.540 static_cg_height= 3.450 [Views] eyepoint=-7.40, 0.00, 2.0 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Nav.1=1, 1, 1 Adf.1=1 Transponder.1=1 Marker.1=1 [SMOKESYSTEM] smoke.0=0.00, -0.70, 1.40, fx_smoke_w [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=140, 240 aileron=200, 1000 rudder=200, 1000 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=1,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -3.50, -10.00,2.8, fx_navred light.1=3, -3.50, 10.00,2.8, fx_navgre light.2=2, -8.40, 0,2.2, fx_strobe light.4=4, -6.62, 0.00, 3.50, fx_vclight [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] Center1= -2.500, 0.000, 2.000, 11.100, 0.000 Center2= -0.500, 0.000, 2.000, 2.300, 0.000 LeftMain= -1.700, -2.100, 1.200, 15.900, 0.000 RightMain= -1.700, 2.100, 1.200, 15.900, 0.000 fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area= 112.000 wing_span= 24.600 wing_root_chord= 4.800 wing_dihedral= 2.600 wing_incidence= 0.000 wing_twist= 0.000 oswald_efficiency_factor= 0.600 wing_winglets_flag= 0 wing_sweep= 3.000 wing_pos_apex_lon= -1.800 wing_pos_apex_vert= 0.000 htail_area= 28.000 htail_span= 10.500 htail_pos_lon= -13.100 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 10.000 vtail_area= 15.000 vtail_span= 2.500 vtail_sweep= 20.000 vtail_pos_lon= -14.300 vtail_pos_vert= 3.000 elevator_area= 10.000 aileron_area= 18.400 rudder_area= 15.000 elevator_up_limit= 26.000 elevator_down_limit= 26.000 aileron_up_limit= 30.000 aileron_down_limit= 30.000 rudder_limit= 45.000 elevator_trim_limit= 15.000 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= 55.000 full_flaps_stall_speed= 55.000 cruise_speed= 178.000 max_indicated_speed=220.000000 [autopilot] autopilot_available=0 flight_director_available=0 [forcefeedback] ground_bumps_magnitude1=3000 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=4.0 ground_bumps_slope1=0.25 ground_bumps_magnitude2=350 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=0.7 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 [brakes] toe_brakes_scale=0.793481 parking_brake=1 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [Flaps.0] type= 0 span-outboard= 0.125 extending-time= 5.000 system_type= 4 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000
