[FLTSIM.0] title=Cessna C-206 Stationair 6 II sim=Cessna C-206 Stationair OH-CHZ model= panel= sound= texture= kb_checklists=Cessna C-206 Stationair OH-CHZ_CHECK kb_reference=Cessna C-206 Stationair OH-CHZ_ref atc_type=Cessna 206 atc_id_enable=1 atc_id=OH-CHZ editable=0 ui_manufacturer=Cessna ui_type=C206 Stationair 6 II ui_variation=OH-CHZ Amphibious description=Cessna's model 185 had the civil name Skywagon and when an improved version was evolved this was designated Cessna Model 206 Super Skywagon. Changes included replacement of the tailwheel landing gear with one of tricycle type; introduction of conical-camber wingtips to reduced induced drag: enlargement of the tailplane and flaps: addition of double cargo doors; and a more powerful 285hp Continental IO-520A flat-six engine. Production of the Model 206 ended in 1964, but many examples still remain in service. - Complete Encylopedia of World Aircraft [General] performance=Maximum Speed\t150 kts\nCruise Speed\t144 kts\nMaximum Range\t1015 nm\nService Ceiling\t16,100 ft\nFuel Capacity\t65 U.S gal\nMax Gross Weight\t3,500 lb\nSeating\t\t6\n atc_type=Cessna atc_model=Stationair [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.25, -18.31, 1.50, fx_navred light.1=3, 0.25, 18.31, 1.50, fx_navgre light.2=2, 0.05, -18.31, 1.50, fx_strobe light.3=2, 0.05, 18.31, 1.50, fx_strobe light.4=1, -17.50, 0.00, 4.20, fx_beacon light.5=4, 0.00, 0.00, 1.00, fx_vclight [WEIGHT_AND_BALANCE] max_gross_weight=3500 // (pounds) empty_weight=1750 // (pounds) reference_datum_position=0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=210, 0.0, -0.9, -1.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=000, 0.0, 0.9, -1.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=000, -2.5, -0.9, -1.0 //Rear Passenger 1 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=000, -2.5, 0.9, -1.0 //Rear Passenger 2 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=000, -5.0, -0.9, -1.0 //Rear Passenger 3 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=000, -5.0, 0.9, -1.0 //Rear Passenger 4 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=000, -6.5, 0.0, -1.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_roll_MOI=4200.000000 empty_weight_pitch_MOI=9900.000000 empty_weight_yaw_MOI=7200.000000 empty_weight_coupled_MOI=0.000000 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.2 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 [fuel] //Tanks Position and capacity: //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=0.00, -2.50, 1.10, 32.5, 0.00 RightMain=0.00, 2.50, 1.10, 32.5, 0.00 //Fuel type: 1=Avgas, 2 = JetA fuel_type=1 number_of_tank_selectors=1 [airplane_geometry] wing_area=175.500000 wing_span=36.600000 wing_root_chord=4.916670 wing_dihedral=1.735840 wing_incidence=1.499634 wing_twist=-2.999268 oswald_efficiency_factor=0.89 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=1.500000 wing_pos_apex_vert=0.000000 htail_area=39.000000 htail_span=11.666667 htail_pos_lon=-14.666667 htail_pos_vert=-1.300000 htail_incidence=3.246460 htail_sweep=0.000000 vtail_area=18.000000 vtail_span=4.837355 vtail_sweep=0.000000 vtail_pos_lon=-16.000000 vtail_pos_vert=1.500000 elevator_area=16.610000 aileron_area=18.300000 rudder_area=6.650000 elevator_up_limit=26.000447 elevator_down_limit=18.000903 aileron_up_limit=21.000227 aileron_down_limit=14.000035 rudder_limit=23.995472 elevator_trim_limit=24.497754 spoiler_limit=90.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) point.0=1, 9.65, -4.30, -8.30, 1573.93, 0.00, 0.52, 34.50, 0.100, 6.00, 0.70, 4.00, 4.00, 0.00, 0.00, 0.00 point.1=1, 9.65, 4.30, -8.30, 1573.93, 0.00, 0.52, 34.50, 0.100, 6.00, 0.70, 4.00, 4.00, 0.00, 0.00, 0.00 point.2=1, -0.85, -4.55, -8.30, 2124.81, 1.00, 0.92, 0.00, 0.300, 2.50, 0.70, 4.00, 4.00, 2.00, 0.00, 0.00 point.3=1, -0.85, 4.55, -8.30, 2124.81, 2.00, 0.92, 0.00, 0.300, 2.50, 0.70, 4.00, 4.00, 3.00, 0.00, 0.00 point.4=1, -0.85, -3.95, -8.30, 2124.81, 0.00, 0.92, 0.00, 0.211, 2.50, 0.70, 4.00, 4.00, 2.00, 0.00, 0.00 point.5=1, -0.85, 3.95, -8.30, 2124.81, 0.00, 0.92, 0.00, 0.211, 2.50, 0.70, 4.00, 4.00, 3.00, 0.00, 0.00 point.6=4, 8.25, -4.33, -7.00, 3000.00, 0.00, 0.00, 50.00, 0.500, 2.50, 1.00, 0.00, 0.00, 0.00, 0.00, 0.00 point.7=4, 8.25, 4.33, -7.00, 3000.00, 0.00, 0.00, 50.00, 0.500, 2.50, 1.00, 0.00, 0.00, 0.00, 0.00, 0.00 point.8=4, -7.00, -4.33, -6.50, 3000.00, 0.00, 0.00, 0.00, 0.500, 2.50, 1.00, 0.00, 0.00, 0.00, 0.00, 0.00 point.9=4, -7.00, 4.33, -6.50, 3000.00, 0.00, 0.00, 0.00, 0.500, 2.50, 1.00, 0.00, 0.00, 0.00, 0.00, 0.00 point.10=2, 0.00, -18.50, 1.40, 3000.00, 0.00, 0.00, 0.00, 0.000, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00 point.11=2, 0.00, 18.50, 1.40, 3000.00, 0.00, 0.00, 0.00, 0.000, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00 point.12=2,-19.55, 0.00, 3.80, 3000.00, 0.00, 0.00, 0.00, 0.000, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00 point.13=2, 7.40, 0.00, -3.80, 3000.00, 0.00, 0.00, 0.00, 0.000, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 point.14=2,-13.90, 0.00, 3.20, 3000.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 7.00, 0.00, 0.00 point.15=2, -1.00, 0.00, -3.30, 3000.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 8.00, 0.00, 0.00 static_pitch=1.000000 static_cg_height=7.934892 [Flaps.0] type=1 span-outboard=0.500000 extending-time=7.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=12.666187,0.000000 flaps-position.2=25.332374,0.000000 flaps-position.3=37.998561,0.000000 [GeneralEngineData] engine_type=0 Engine.0=6.000000,0.000000,0.000000 fuel_flow_scalar=1.000000 [piston_engine] cylinder_displacement=86.666667 compression_ratio=8.500000 number_of_cylinders=6 max_rated_rpm=2700.000000 max_rated_hp=285.000000 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=0 max_design_mp=0.000000 min_design_mp=0.000000 critical_altitude=0.000000 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=7.333000 propeller_blades=3 propeller_moi=5.700000 beta_max=36.000000 beta_min=09.000000 min_gov_rpm=1400.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=25.000000 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=54.000000 full_flaps_stall_speed=43.200000 cruise_speed=148.000000 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint=0.205052,-0.884289,0.781763 [direction_indicators] direction_indicator.0=1,0 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 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
