[FLTSIM.0] title=Cessna 206 Turbo Stationair 3A-MLS sim=Cessna TU206G Turbo-Stationair model= panel= sound= texture= kb_checklists=Cessna_TU206G_Check kb_reference=Cessna_TU206G_Ref atc_type=Cessna atc_id_enable=0 atc_id=3A-MLS ui_manufacturer=Cessna ui_type=T206 Turbo Stationair ui_variation=My registration description=My 206 (copy your original aircraft description) [General] atc_type=STATIONAIR atc_model=C206 editable=1 performance=My 206 performances (copy your original aircraft performances) [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 [WEIGHT_AND_BALANCE] empty_weight=2228 reference_datum_position=0.0, 0, 0 empty_weight_CG_position=0.0, 0, 0 max_number_of_stations=50 station_load.0=170, 3.0, -1.5, 0.0 //Pilot # 1 station_load.1=170, 3.0, 1.5, 0.0 //Co-Pilot # 2 station_load.2=160, 0.2, -1.5, 0.0 //Rear Pax # 3 station_load.3=160, 0.2, 1.5, 0.0 //Rear Pax # 4 station_load.4=0, -3.4, -1.5, 0.0 //Rear Pax # 5 station_load.5=0, -3.4, 1.5, 0.0 //Rear Pax # 6 station_load.6=100, -4.5, 0.0, 0.0 //Baggage Aft 100Lbs max empty_weight_roll_MOI=4200.000000 empty_weight_pitch_MOI=9900.000000 empty_weight_yaw_MOI=7200.000000 empty_weight_coupled_MOI=0.000000 [ground_reaction] main_gear_damping_ratio=1.0 center_gear_damping_ratio=1.0 [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 [fuel] LeftMain=-0.25,-7.5,2.5,44.0,2.5 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), RightMain=-0.25,7.5,2.5,44.0,2.5 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=182.000000 wing_span=39.666667 wing_root_chord=4.916670 wing_dihedral=2.999268 wing_incidence=0.900879 wing_twist=-0.999756 oswald_efficiency_factor=0.815740 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=1.229000 wing_pos_apex_vert=0.000000 htail_area=46.000000 htail_span=14.500000 htail_pos_lon=-15.833333 htail_pos_vert=0.000000 htail_incidence=3.246460 htail_sweep=0.000000 vtail_area=18.000000 vtail_span=4.837355 vtail_sweep=0.000000 vtail_pos_lon=-14.583333 vtail_pos_vert=4.666667 elevator_area=17.500000 aileron_area=14.000000 rudder_area=11.000000 elevator_up_limit=25.000001 elevator_down_limit=20.000001 aileron_up_limit=20.000001 aileron_down_limit=15.000001 rudder_limit=27.000001 elevator_trim_limit=20.000001 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1.000000,6.250000,0.000000,-5.250000,1416.544276,0.000000,0.525705,34.500000,0.268107,2.500000,1.000000,0.000000,0.000000,0.000000,0.000000,0.000000 point.1=1.000000,-2.000000,-5.333333,-5.250000,1967.422605,1.000000,0.525705,0.000000,0.256005,2.500000,1.000000,0.000000,0.000000,2.000000,0.000000,0.000000 point.2=1.000000,-2.000000,5.333333,-5.250000,1967.422605,2.000000,0.525705,0.000000,0.256005,2.500000,1.000000,0.000000,0.000000,3.000000,0.000000,0.000000 point.3=2.000000,-1.500000,-19.916667,2.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-1.500000,19.916667,2.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-21.750000,0.000000,-0.083333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,7.666667,0.000000,-3.833333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.7=2.000000,-16.333333,0.000000,6.833333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000, 0.000000, 7.000000, 0.000000, 0.000000 point.8=2.0,-1.0, 0.0, -1.333333,1574.803150, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8.0, 0.0, 0.0 static_pitch=0.000000 static_cg_height=5.031272 [Flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=8.0 // seconds system_type=0 flaps-position.0=0.0,0.0 // degrees flaps-position.1=10.0,0.0 // degrees flaps-position.2=20.0,0.0 // degrees flaps-position.3=40.0,0.0 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS system_type=0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [GeneralEngineData] engine_type=0 Engine.0=6.666667,0.0,0.0 fuel_flow_scalar=1.0 [piston_engine] cylinder_displacement=87.000000 compression_ratio=8.000000 number_of_cylinders=6 max_rated_rpm=2700 //Max rated RPM max_rated_hp=310 //Max rated HP 285 continuous, 310 takeoff fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp=36.5 //Max design manifold pressure, (inHg) min_design_mp=1.000000 critical_altitude=27000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [propeller] propeller_type=0 propeller_diameter=6.750000 propeller_blades=2 propeller_moi=5.000000 beta_max=50.000000 beta_min=12.000000 min_gov_rpm=1100.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=0.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Reference Speeds] flaps_up_stall_speed=56.000000 full_flaps_stall_speed=44.800000 cruise_speed=134.378298 [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 [keyboard_response] elevator=150.00,250.00 aileron=150.00,250.00 rudder=150.00,250.00 [Views] eyepoint=-1.871104,-1.076526,1.460999 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=700.00 autothrottle_available=0 pitch_takeoff_ga=8.000000 use_no_default_pitch=1 use_no_default_bank=1 [direction_indicators] direction_indicator.0=1,0 [FLTSIM.0] title=Cessna 206 Turbo Stationair 3A-MLS sim=Cessna TU206G Turbo-Stationair model= panel= sound= texture= kb_checklists=Cessna_TU206G_Check kb_reference=Cessna_TU206G_Ref atc_type=Cessna atc_id_enable=0 atc_id=3A-MLS ui_manufacturer=Cessna ui_type=T206 Turbo Stationair ui_variation=3A-MLS (Bordeaux et rouge) description=C206 by Mikko Maliniemi. Flight Dynamics © Steve Small FSD 6\/2001. For specifications, see documents. COPYRIGHT : Airfile may not be used as the basis of other flight models without agreement. Please respect the works of others and build new airfiles from FS2000 defaults.\n [General] atc_type=STATIONAIR atc_model=C206 editable=1 performance=Vitesse maximale\t\n183 nds 211 mph\t339 km\/h\n\nVitesse de croisière\t\n149 nds 171 mph \t276 km\/h\n\nMotorisation\t\nTeledyne Continental TSIO-520-M 285 chevaux\n\nHélice\t\nMcCauley à trois pales et à vitesse constante\n\nRayon d'action maximal\t\n700 nm 806 sm \t1,296 km\n\nPlafond pratique\t\n27,000 pieds \t 8,235 m\n\nCapacité en carburant\t\n92 gal 348 L \n\nMasse à vide\t\n2,122 livres \t 963 kg\n\nMasse totale maximale\t\n3,600 livres \t 1,633 kg\n\nLongueur\t\n28 3' pieds\t 8,62 m\n\nEnvergure\t\n36 pieds\t 11 m\n\nHauteur\t\n9 3' pieds\t 2.82 m\n\nNombre de places\t\njusqu'à 6 \n\nCharge utile\t\n1,478 livres \t 670 kg [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 [WEIGHT_AND_BALANCE] empty_weight=2228 reference_datum_position=0.0, 0, 0 empty_weight_CG_position=0.0, 0, 0 max_number_of_stations=50 station_load.0=170, 3.0, -1.5, 0.0 //Pilot # 1 station_load.1=170, 3.0, 1.5, 0.0 //Co-Pilot # 2 station_load.2=160, 0.2, -1.5, 0.0 //Rear Pax # 3 station_load.3=160, 0.2, 1.5, 0.0 //Rear Pax # 4 station_load.4=0, -3.4, -1.5, 0.0 //Rear Pax # 5 station_load.5=0, -3.4, 1.5, 0.0 //Rear Pax # 6 station_load.6=100, -4.5, 0.0, 0.0 //Baggage Aft 100Lbs max empty_weight_roll_MOI=4200.000000 empty_weight_pitch_MOI=9900.000000 empty_weight_yaw_MOI=7200.000000 empty_weight_coupled_MOI=0.000000 [ground_reaction] main_gear_damping_ratio=1.0 center_gear_damping_ratio=1.0 [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 [fuel] LeftMain=-0.25,-7.5,2.5,44.0,2.5 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), RightMain=-0.25,7.5,2.5,44.0,2.5 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=182.000000 wing_span=39.666667 wing_root_chord=4.916670 wing_dihedral=2.999268 wing_incidence=0.900879 wing_twist=-0.999756 oswald_efficiency_factor=0.815740 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=1.229000 wing_pos_apex_vert=0.000000 htail_area=46.000000 htail_span=14.500000 htail_pos_lon=-15.833333 htail_pos_vert=0.000000 htail_incidence=3.246460 htail_sweep=0.000000 vtail_area=18.000000 vtail_span=4.837355 vtail_sweep=0.000000 vtail_pos_lon=-14.583333 vtail_pos_vert=4.666667 elevator_area=17.500000 aileron_area=14.000000 rudder_area=11.000000 elevator_up_limit=25.000001 elevator_down_limit=20.000001 aileron_up_limit=20.000001 aileron_down_limit=15.000001 rudder_limit=27.000001 elevator_trim_limit=20.000001 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1.000000,6.250000,0.000000,-5.250000,1416.544276,0.000000,0.525705,34.500000,0.268107,2.500000,1.000000,0.000000,0.000000,0.000000,0.000000,0.000000 point.1=1.000000,-2.000000,-5.333333,-5.250000,1967.422605,1.000000,0.525705,0.000000,0.256005,2.500000,1.000000,0.000000,0.000000,2.000000,0.000000,0.000000 point.2=1.000000,-2.000000,5.333333,-5.250000,1967.422605,2.000000,0.525705,0.000000,0.256005,2.500000,1.000000,0.000000,0.000000,3.000000,0.000000,0.000000 point.3=2.000000,-1.500000,-19.916667,2.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-1.500000,19.916667,2.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-21.750000,0.000000,-0.083333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,7.666667,0.000000,-3.833333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.7=2.000000,-16.333333,0.000000,6.833333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000, 0.000000, 7.000000, 0.000000, 0.000000 point.8=2.0,-1.0, 0.0, -1.333333,1574.803150, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8.0, 0.0, 0.0 static_pitch=0.000000 static_cg_height=5.031272 [Flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=8.0 // seconds system_type=0 flaps-position.0=0.0,0.0 // degrees flaps-position.1=10.0,0.0 // degrees flaps-position.2=20.0,0.0 // degrees flaps-position.3=40.0,0.0 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS system_type=0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [GeneralEngineData] engine_type=0 Engine.0=6.666667,0.0,0.0 fuel_flow_scalar=1.0 [piston_engine] cylinder_displacement=87.000000 compression_ratio=8.000000 number_of_cylinders=6 max_rated_rpm=2700 //Max rated RPM max_rated_hp=310 //Max rated HP 285 continuous, 310 takeoff fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp=36.5 //Max design manifold pressure, (inHg) min_design_mp=1.000000 critical_altitude=27000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [propeller] propeller_type=0 propeller_diameter=6.750000 propeller_blades=2 propeller_moi=5.000000 beta_max=50.000000 beta_min=12.000000 min_gov_rpm=1100.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=0.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Reference Speeds] flaps_up_stall_speed=56.000000 full_flaps_stall_speed=44.800000 cruise_speed=134.378298 [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 [keyboard_response] elevator=150.00,250.00 aileron=150.00,250.00 rudder=150.00,250.00 [Views] eyepoint=-1.871104,-1.076526,1.460999 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=700.00 autothrottle_available=0 pitch_takeoff_ga=8.000000 use_no_default_pitch=1 use_no_default_bank=1 [direction_indicators] direction_indicator.0=1,0