[fltsim.0] title=Piper Warrior-II_nwf sim=Piper Warrior-II_nwf model=nwf panel=high sound= texture= kb_checklists= kb_reference= ui_manufacturer=Embraer ui_type=EMB-712 Tupi Aeroclube de Bauru ui_variation=Sem carenagem de roda description=Aeronave monomotor, equipada com trem de pouso fixo, inteiramente metálica, dispondo de acomodações para um máximo de 4 ocupantes. Versão produzida sob licença pela Embraer (Brasil) e Chincul (Chile) do popular Piper PA-28 Cherokee Archer II. A série Cherokee tem mais de 20.000 unidades produzidas, sendo um dos aviões de pequeno porte mais populares em todo o mundo. Eficaz treinador no Aeroclube de Bauru junto aos AB-115 Aeroboero. atc_id=PT-VKH atc_heavy=0 atc_airline= atc_flight_number= [fltsim.1] title=Piper Warrior-II_wwf sim=Piper Warrior-II_wwf model=wwf panel=high sound= texture= kb_checklists= kb_reference= ui_manufacturer=Embraer ui_type=EMB-712 Tupi Aeroclube de Bauru ui_variation=Com carenagem de roda description=Aeronave monomotor, equipada com trem de pouso fixo, inteiramente metálica, dispondo de acomodações para um máximo de 4 ocupantes. Versão produzida sob licença pela Embraer (Brasil) e Chincul (Chile) do popular Piper PA-28 Cherokee Archer II. A série Cherokee tem mais de 20.000 unidades produzidas, sendo um dos aviões de pequeno porte mais populares em todo o mundo. Eficaz treinador no Aeroclube de Bauru junto aos AB-115 Aeroboero. atc_id=PT-VKH atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=Embraer atc_model=EMB-712 editable=2 performance= Repintado por Carlos Oliveira [WEIGHT_AND_BALANCE] max_gross_weight= 2440.000 empty_weight= 1541.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 2.000, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, -3.000, -1.500, 0.000 station_load.1= 170.000, -3.000, 1.500, 0.000 station_load.2= 0, -6.2, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3= 0, -6.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4= 0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI= 1400.000 empty_weight_roll_MOI= 1137.000 empty_weight_yaw_MOI= 2360.000 empty_weight_coupled_MOI= 0.000 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 [GeneralEngineData] engine_type= 0 Engine.0= 2.400, 0.000, 0.000 fuel_flow_scalar= 0.800 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement= 80.000 compression_ratio= 8.500 number_of_cylinders= 4 max_rated_rpm= 2700.000 max_rated_hp= 160.000 fuel_metering_type= 1 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=1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar=0.8 //Scalar on idle RPM friction [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type= 1 propeller_diameter=5.8 propeller_blades= 2 propeller_moi= 1.000 beta_max= 0.000 beta_min= 0.000 min_gov_rpm= 0.000 prop_tc= 0.000 gear_reduction_ratio= 1.0 fixed_pitch_beta=22.5 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 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 [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 point.0= 1.000, 4.970, 0.000, -3.600, 1500.000, 0.000, 0.500, 22.000, 0.250, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, -1.300, -4.300, -3.500, 3500.000, 1.000, 0.500, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, -1.300, 4.300, -3.500, 3500.000, 2.000, 0.500, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000 point.3= 2.000, -3.900, -18.000, 3.000, 1800.000, 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, -3.900, 18.000, 3.000, 1800.000, 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, -20.230, 0.000, 0.300, 1800.000, 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, 1.480, 0.000, -2.170, 1800.000, 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, -22.800, 0.000, 5.830, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 point.8= 2.000, -4.900, 0.000, -2.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 max_number_of_points=21 static_pitch= 4.300 static_cg_height= 3.150 [Views] eyepoint=-0.559, -0.897, 2.206 //(feet) longitudinal, lateral, vertical distance from reference datum [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=2, -1.30, -18.3, 1.4, fx_strobe light.1=2, -1.30, 18.3, 1.4, fx_strobe [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=100, 180 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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain= -3.900, -2.100, 2.500, 25.000, 0.000 RightMain= -3.900, 2.100, 2.500, 25.000, 0.000 fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area= 150.000 wing_span= 35.000 wing_root_chord= 4.8000 wing_dihedral= 6.000 wing_incidence= 1.500 wing_twist= -3.000 oswald_efficiency_factor= 0.60 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= -1.500 wing_pos_apex_vert= 1.000 htail_area= 39.000 htail_span= 11.700 htail_pos_lon= -18.300 htail_pos_vert= 0.000 htail_incidence= 3.200 htail_sweep= 10.000 vtail_area= 18.000 vtail_span= 4.800 vtail_sweep= 40.000 vtail_pos_lon= -16.200 vtail_pos_vert= 1.500 elevator_area= 16.600 aileron_area= 18.300 rudder_area= 6.700 elevator_up_limit= 28.000 elevator_down_limit= 21.000 aileron_up_limit= 20.000 aileron_down_limit= 15.000 rudder_limit= 24.000 elevator_trim_limit= 19.500 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= 50.000 cruise_speed= 104.000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 1.000 system_type= 0 damaging-speed= 120.000 blowout-speed= 150.000 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= 40.000, 0.000 [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 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
