[fltsim.0] title=ACSP Tupi sim=EMB_712 model= panel= sound= texture=ACSP kb_checklists= kb_reference= atc_id=PT-NTY ui_manufacturer=Embraer ui_type=EMB-712 Tupi ui_variation=ACSP description=Flight dynamics derived from FS2002 Cessna 182RG, adapted by Rien Cornelissen to match Arrow-III flight characteristics\n\n\n\n\n atc_heavy=0 atc_airline= atc_flight_number= visual_damage=1 [fltsim.1] title=Tupi sim=EMB_712 model= panel= sound= texture=Particular kb_checklists= kb_reference= atc_id=PT-MTJ ui_manufacturer=Embraer ui_type=EMB-712 Tupi ui_variation=Particular description=Flight dynamics derived from FS2002 Cessna 182RG, adapted by Rien Cornelissen to match Arrow-III flight characteristics\n\n\n\n\n atc_heavy=0 atc_airline= atc_flight_number= visual_damage=1 [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=25000 [General] performance=Engine 200 hp at 2,700 RPM, constant speed prop\nMaximum Speed at MSL 148 kts\n75% Power Cruise 138 kts at 6,600 ft\nMax. Rate of Climb 820 ft\/min at MSL, 90 kts,2750 lbs\nMaximum Range\t 1100 nm\nService Ceiling 16,000 ft\nFuel Capacity\t 72 U.S gal\nEmpty Weight 1641 lbs \nMax Gross Weight\t 2750 lbs\nSeating\t\t 4\n atc_type=Arrow atc_model=PA28 [WEIGHT_AND_BALANCE] empty_weight=1641.000 max_gross_weight=2750.000 reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=1.500, 0.000, 0.000 max_number_of_stations=50 station_load.0=170.000, -1.000, -0.500, 0.000 station_load.1=0.000, -1.000, 1.500, 0.000 station_load.2=0.000, -3.800, -1.500, 0.000 station_load.3=0.000 -3.800, 1.500, 0.000 station_load.4=0.000, -5.500, 0.000, 0.000 ;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=-1.000 CG_aft_limit=1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.100 induced_drag_scalar=1.150 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [piston_engine] power_scalar=1.000 cylinder_displacement=100.000 compression_ratio=8.500 number_of_cylinders=4 max_rated_rpm=2700.000 max_rated_hp=200.000 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=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.302 [propeller] thrust_scalar=1.000 propeller_type=0 propeller_diameter=6.833 propeller_blades=2 propeller_moi=2.500 beta_max=27.000 beta_min=14.000 min_gov_rpm=1100.000 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 [pitot_static] vertical_speed_time_constant=0.7 [fuel] LeftMain=-1.200, -6.500, 0.85, 36.000, 0.000 RightMain=-1.200, 6.500, 0.85, 36.000, 0.000 fuel_type=1 number_of_tank_selectors=1 [airplane_geometry] wing_area=140.00 wing_span=30.0 wing_root_chord=5.25 wing_dihedral=6.0 wing_incidence=2.0 wing_twist=-3.0 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=39.0 //Square feet htail_span=11.667 htail_pos_lon=-18.327 htail_pos_vert=0.000 htail_incidence=3.246 htail_sweep=0.000 vtail_area=18.000 vtail_span=4.837 vtail_sweep=0.000 vtail_pos_lon=-16.243 vtail_pos_vert=1.500 elevator_area=16.610 aileron_area=18.300 rudder_area=6.650 elevator_up_limit=28.000 elevator_down_limit=20.999 aileron_up_limit=19.996 aileron_down_limit=15.000 rudder_limit=23.995 elevator_trim_limit=19.498 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 htail_area=39.000000 //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, 5.370, 0.000, -3.42, 3500, 0, 0.500, 22.0, 0.250, 2.5, 0.90, 5.000, 5.000, 0 point.1= 1.000, -1.300, -5.192, -3.15, 3500, 1, 0.517, 0.0, 0.250, 2.5, 0.90, 5.000, 5.000, 2 point.2= 1.000, -1.300, 5.192, -3.15, 3500, 2, 0.517, 0.0, 0.250, 2.5, 0.90, 5.000, 5.000, 3 point.3= 2, -2.20, -18.5, 0.600, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.4= 2, -2.20, 18.5, 0.600, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.5= 2,-16.90, 0.0, 0.60, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.6= 2, 4.40, 0.0, -1.33, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 point.7= 2,-16.90, 0.0, 5.50, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0 point.8= 2, -1.60, 0.0, -1.33, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8, 0.0, 0.0 static_pitch=3.5 static_cg_height=2.8 [GeneralEngineData] engine_type=0 Engine.0=6.840, 0.000, 0.000 fuel_flow_scalar=1.000 [Reference Speeds] flaps_up_stall_speed=60.000 full_flaps_stall_speed=55.000 cruise_speed=125.000 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint=0.152, -0.920, 2.340 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 use_no_default_bank=1 use_no_default_pitch=1 [direction_indicators] direction_indicator.0=2,0 [electrical] ;BusType, MaxAmpLoad, MinVoltage //BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 0 , 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=2, 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 [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, -1.763, -17.800, 1.435, fx_strobe light.1=2, -1.763, 17.800, 1.435, fx_strobe light.2=4, 0.175, -0.925, 2.350,fx_vclighth, light.3=4, 0.175, -0.925, 2.350,fx_vclight, [exits] number_of_exits=2 exit_rate.0=0.2 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [Flaps.0] type=1 span-outboard=0.500 extending-time=0.5 system_type=0 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=12.666, 0.000 flaps-position.2=25.332, 0.000 flaps-position.3=37.999, 0.000
