[fltsim.0] title=Piper Embraer Tupi Aeroclube do RGS sim=Piper Archer-II_wwf model= panel= sound= texture=args kb_checklists=Archer_check kb_reference=Archer_ref ui_manufacturer=Embraer (Piper) ui_type=EMB-712 Tupi ui_variation=Aeroclube do RGS description=The Embraer EMB-712 Tupi is used as a trainer for new applicants. Repaint by Luiz Foernges atc_id=PT-RKD atc_heavy=0 atc_airline= atc_flight_number= [fltsim.1] title=Piper Embraer Tupi Aeroclube de Eldorado do Sul sim=Piper Archer-II_wwf model= panel= sound= texture=aes_tupi kb_checklists=Archer_check kb_reference=Archer_ref ui_manufacturer=Embraer (Piper) ui_type=EMB-712 Tupi ui_variation=Aeroclube de Eldorado do Sul description=The Embraer EMB-712 Tupi is used as a trainer for new applicants. Repaint by Luiz Foernges atc_id=PT-NRQ atc_heavy=0 atc_airline= atc_flight_number= [fltsim.2] title=Piper Archer II Aeroclube de Eldorado do Sul sim=Piper Archer-II_wwf model= panel= sound= texture=aes kb_checklists=Archer_check kb_reference=Archer_ref ui_manufacturer=Piper ui_type=Archer II ui_variation=Aeroclube de Eldorado do Sul description=The Piper PA 28 180 is used as a trainer for new applicants. Repaint by Luiz Foernges atc_id=PT-KQU atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=PIPER atc_model=P28A editable=1 performance=Maximum Speed\t138 kts \nCruise Speed\t112 kts \nEngine\tLycoming O-320-D2A, 180 bhp\nPropeller\t Sensenich 74DM6-06-60 Fixed Pitch, \n\tTwo-Bladed\nMaximum Range\t525 nm \nService Ceiling\t11,000 ft\t \nFuel Capacity\t50 gal\t \nEmpty Weight\t1,541 lb\\n\nMax. Gross Weight\t2,440 lb\t \nLength\t\t23 ft, 9.6 in\nWingspan\t\t35 ft \t \nHeight\t\t7 ft, 3.6 in\t \nSeating\t \t 4\nUseful Load\t899 lb\t \n [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=5 station_load.0=170.000000, 0.500000, -1.500000, 0.000000, Station 1 station_load.1=0.000000, 0.500000, 1.500000, 0.000000, Station 2 station_load.2= 0.000, -2.7, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3= 0.000, -2.7, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4= 0.000, -5.0, 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 ;CG_forward_limit= 1.500 ;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=0.5 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [GeneralEngineData] engine_type= 0 Engine.0= 7.000, 0.150, 0.000 fuel_flow_scalar= 0.800 min_throttle_limit=0.000000 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement= 90.000 compression_ratio= 8.500 number_of_cylinders= 4 max_rated_rpm= 2700.000 max_rated_hp= 180.000 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=1.2 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type= 1 propeller_diameter= 5.800 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= 1.000 fixed_pitch_beta= 24.500 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= 0.000 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) 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 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 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 flap_motor=0, 0 , 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, 5.300, 0.000, -3.300, 3500.000, 0.000, 0.600, 22.000, 0.250, 3.000, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, -1.500, -4.900, -3.100, 3500.000, 1.000, 0.700, 0.000, 0.300, 3.000, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, -1.500, 4.900, -3.100, 3500.000, 2.000, 0.700, 0.000, 0.300, 3.000, 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= 3.500 static_cg_height= 2.860 gear_system_type=0 [Views] eyepoint=0.15, -0.9, 2.2 //(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, -1.250, -17.820, 1.300, fx_strobe light.1=2, -1.250, 17.820, 1.300, fx_strobe light.2=4, 0.175, -0.925, 2.350, fx_vclighth, light.3=4, 0.175, -0.925, 2.350, fx_vclight, [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= -2.000, -5.100, -0.300, 25.000, 0.000 RightMain= -2.000, 5.100, -0.300, 25.000, 0.000 fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area= 169.000 wing_span= 35.000 wing_root_chord= 5.300 wing_dihedral= 6.000 wing_incidence= 1.500 wing_twist= -3.000 oswald_efficiency_factor= 0.750 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= -1.550 wing_pos_apex_vert= 1.000 htail_area= 18.000 htail_span= 4.800 htail_pos_lon= -12.500 htail_pos_vert= 2.5000 htail_incidence= 3.200 htail_sweep= 40.000 vtail_area= 18.000 vtail_span= 4.800 vtail_sweep= 40.000 vtail_pos_lon= -12.500 vtail_pos_vert= 2.500 elevator_area= 35.000 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= 112.000 max_indicated_speed=160.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 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 [exits] number_of_exits=2 exit_rate.0=0.2 [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 [brakes] toe_brakes_scale=1.0 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] normal_pressure=0.000000 [stall_warning] type=2 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [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= 6.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 40.000, 0.000
