[fltsim.0] title=Rans S-6S sim=s6 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=G-RICH ui_manufacturer=Rans ui_type=S-6S ui_variation=White and blue visual_damage=1 description=The design goal of the S-6S was to create a fast build kit plane with traditional aircraft fabric covering. The basic airframe is based off the successful S-6ES. In the tradition of the ES series most parts are preformed and prefinished. Typically on fabric planes, the inside is painted or covered with fabric. Many hours of tedious labor is saved with the use of a molded interior kit. atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=Rans atc_model= editable=1 performance=Maximum Speed\n120 kts \n\nCruise Speed\n110 kts \n\nEngine\nRotax 912\/912S\n\nPropeller\nWood\n\nMaximum Range\n440 miles\/432 miles\n\nService Ceiling\n17,000 ft\/17,500 ft\n\nFuel Capacity\n18 gal US\t \n\nEmpty Weight\n610 lbs\n\nMaximum Gross Weight\n1100 lbs\nLength\n20 ft\n\nWingspan\n34.5 ft\n\nHeight\n9 ft\n\nSeating\t 2\n\nUseful Load\n490 lbs\n [WEIGHT_AND_BALANCE] max_gross_weight= 1100.000 empty_weight= 600.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations= 50 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 station_load.0= 0.000, 0.000, 0.000, 0.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 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 [GeneralEngineData] engine_type= 0 Engine.0= 4.500, 0.000, 0.000 fuel_flow_scalar= 0.880 [piston_engine] power_scalar=1.000 cylinder_displacement= 45.000 compression_ratio= 9.000 number_of_cylinders= 4 max_rated_rpm= 5800.000 max_rated_hp= 100.000 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=0.508 [propeller] thrust_scalar=1.000 propeller_type= 1 propeller_diameter= 6.000 propeller_blades= 2 propeller_moi= 5.000 beta_max= 0.000 beta_min= 0.000 min_gov_rpm= 0.000 prop_tc= 0.000 gear_reduction_ratio= 2.270 fixed_pitch_beta= 20.000 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 [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 //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, 3.500, 0.000, -3.900, 1500.000, 0.000, 0.600, 22.000, 0.250, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, -0.900, -2.700, -3.900, 3500.000, 1.000, 0.600, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, -0.900, 2.700, -3.900, 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, 0.000, -17.000, 1.800, 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, 0.000, 17.000, 1.800, 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, -11.000, 0.000, -1.000, 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, 5.200, 0.000, -2.400, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 max_number_of_points=21 static_pitch= 0.000 static_cg_height= 3.900 [Views] eyepoint=-0.2, -0.7, 1 //(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=3, -0.88, -17.5, 1.8, fx_navred light.1=3, -0.88, 17.5, 1.8, fx_navgre light.2=2, -0.15, -17.5, 1.8, fx_strobe light.3=2, -0.15, 17.5, 1.8, fx_strobe light.4=1, -11, 0.00, 3.9, fx_beacon light.5=4, 0, 0.00, 1.5, 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 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain= 0.000, -2.100, 1.800, 9.000, 0.000 RightMain= 0.000, 2.100, 1.800, 9.000, 0.000 fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area= 155.250 wing_span= 34.500 wing_root_chord= 4.500 wing_dihedral= 1.700 wing_incidence= 1.500 wing_twist= -3.000 oswald_efficiency_factor= 0.680 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.500 wing_pos_apex_vert= 2.100 htail_area= 25.000 htail_span= 11.700 htail_pos_lon= -13.000 htail_pos_vert= 1.000 htail_incidence= 3.200 htail_sweep= 10.000 vtail_area= 18.000 vtail_span= 4.800 vtail_sweep= 30.000 vtail_pos_lon= -11.000 vtail_pos_vert= 2.500 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= 30.000 elevator_trim_limit= 90.000 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= 41.000 full_flaps_stall_speed= 36.000 cruise_speed= 108.000 [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=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 [Flaps.0] type= 0 span-outboard= 0.000 extending-time= 0.100 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 [Flaps.1] type= 1 span-outboard= 0.500 extending-time= 7.000 system_type= 3 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= 12.700, 0.000 flaps-position.2= 25.300, 0.000 flaps-position.3= 38.000, 0.000
