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Help - trying to adapt Rob Young Cessna 208b fs2002 fil...

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Hi,Have recently been trying out the fs2004 cessna caravan which seems to be pretty nice. Then read about the free realairsimulations fs2002 aircraft.cfg / air file which I downloaded. Has stabliised things really nicely except there is a small problem. When the engine is shut down the propellor keeps spinning like in the wind or something (and at a considerable speed!). Anyone know of an easy thing I can do to the aircraft.cfg file which might be able to fix this without changing the excellent flight dynamics?Have included below the main parts of the original and realairsimulations aircraft.cfg's that I'm usingAny help appreciatedThanks,Pps any way I can get this thing to stop taxiing like crazy too??!!fs2004 original:[General]atc_type=Cessnaatc_model=C208editable=0performance="Maximum Speedn175 kts 324 km/hrnnCruise Speedn164 kts t 305 km/hr at 20,000 ftnnEnginenPratt & Whitney Canada, Inc., PT6A-114A Free Turbine Flat Rated at 675 Shaft hp nnPropellernThree-Bladed, Constant Speed, Full Feathering, Reversible McCauley, 106-inch diameternnMaximum Endurancen5.1 hours maximum cruise at 10,000 ftn6.6 hours maximum cruise at 18,000 ftn6.4 hours maximum range at 10,000 ftn7.2 hours maximum range at 18,000 ftnnService Ceilingn22,800 ft 6,949 mnnFuel Capacityn335 gal 1,268 LnnEmpty Weightn4,575 lb 2,075 kgnnMaximum Gross Weightn8,785 lbt 3,985 kgnnUseful Loadn4,000 lbt 1,814 kgnnLengthn41 ft, 7 in 12.7 mnnWingspann52 ft, 1 int 15.8 mnnHeightn15 ft, 5-1/2 in 4.8 mnnSeatingnUp to 14"[WEIGHT_AND_BALANCE]max_gross_weight = 8785 // (pounds)empty_weight = 4575 // (pounds)reference_datum_position = 16.2, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)empty_weight_CG_position = -15.4, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datummax_number_of_stations = 50station_load.0 = "170, -11.3, -1.5, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.1 = "170, -11.3, 1.5, 0.0, Passenger 2" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.2 = "0, -13.9, -1.5, 0.0, Passenger 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.3 = "0, -13.9, 1.5, 0.0, Passenger 4" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.4 = "170, -17.2, -1.5, 0.0, Passenger 5" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.5 = "170, -17.2, 1.5, 0.0, Passenger 6" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.6 = "150, -20.2, -1.5, 0.0, Passenger 7" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.7 = "150, -20.2, 1.5, 0.0, Passenger 8" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.8 = "0, -23.2, -1.5, 0.0, Passenger 9" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.9 = "0, -23.2, 1.5, 0.0, Passenger 10" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.10= "0, -10.6, 0.0,-5.0, Cargo Pod 1" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.11= "0, -15.2, 0.0,-5.0, Cargo Pod 2" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.12= "50, -19.4, 0.0,-5.0, Cargo Pod 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.13= "50, -24.6, 0.0,-5.0, Cargo Pod 4" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet);Moments of Inertiaempty_weight_pitch_MOI = 8874.87empty_weight_roll_MOI = 6026.96empty_weight_yaw_MOI = 11858.54empty_weight_coupled_MOI = 0.0[flight_tuning]cruise_lift_scalar = 1.0parasite_drag_scalar = 1.0induced_drag_scalar = 1.0elevator_effectiveness = 1.0aileron_effectiveness = 1.0rudder_effectiveness = 1.0pitch_stability = 1.0roll_stability = 1.0yaw_stability = 1.0elevator_trim_effectiveness = 1.0aileron_trim_effectiveness = 1.0rudder_trim_effectiveness = 1.0[GeneralEngineData]engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=TurbopropEngine.0 = -2.4, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datumfuel_flow_scalar = 1.12 //Scalar for fuel flow efficiencymin_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser[propeller]thrust_scalar = 1.0 //Propeller thrust scalarpropeller_type = 0 //0=Constant Speed, 1=Fixed Pitchpropeller_diameter = 8.8 //Propeller Diameter, (feet)propeller_blades = 3 //Number of propeller bladespropeller_moi = 19 //Propeller moment of inertiabeta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees)beta_min = 15.6 //Minimum blade pitch angle for constant speed prop, (degrees)min_gov_rpm = 25520 //Miminum governed RPMprop_tc = 0.004 //Prop time-constantgear_reduction_ratio = 17.4 //Propeller gear reduction ratiofixed_pitch_beta = 0 //Fixed pitch angle of fixed pitch prop, (degrees)low_speed_theory_limit = 80 //Speed at which low speed theory becomes blended in (feet/second)prop_sync_available = 0 //Prop synchronization available? 0=FALSE, 1=TRUEprop_deice_available = 1 //Prop de-icing available? 0=FALSE, 1=TRUEprop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUEprop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUEmin_rpm_for_feather = 700 //Minimum RPM for prop featheringbeta_feather = 88.0 //Feathering pitch angle (degrees)power_absorbed_cf = 0.9 //Coefficient of friction for power absorbed by propellerdefeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUEminimum_on_ground_beta = 1.0 //Miminum pitch angle on ground, (degrees)minimum_reverse_beta = -14.0 //Minimum pitch angle in reverse, (degrees)[TurbineEngineData]fuel_flow_gain = 0.011 //Gain on fuel flowinlet_area = 1.0 //Square Feet, engine nacelle inlet arearated_N2_rpm = 33000 //RPM, second stage compressor rated valuestatic_thrust = 158 //Lbs, max rated static thrust at Sea Level[turboprop_engine]power_scalar = 1.0 //Scalar on Turboprop powermaximum_torque = 1865 //Maximum torque available (ft-lbs)[Flaps.0]type=1span-outboard=0.5 // Percent span for flap positionextending-time=5.7 // Seconds, time to fully extendsystem_type=0 // 0 = electricaldamaging-speed = 175 // KIASblowout-speed = 175 // KIASflaps-position.0= 0 // degreesflaps-position.1=10,175 // degreesflaps-position.2=20,150 // degreesflaps-position.3=30,125 // degrees[pitot_static]vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI[Radios]// Radio Type = availiable, standby frequency, has glide slopeAudio.1 = 1Com.1 = 1, 1Com.2 = 1, 1Nav.1 = 1, 1, 1Nav.2 = 1, 1, 0Adf.1 = 1Transponder.1 = 1Marker.1 = 1[LIGHTS]//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, -16.30, -26.41, 3.35, fx_navredlight.1 = 3, -16.30, 26.41, 3.35, fx_navgrelight.2 = 3, -42.28, 0.00, 2.10, fx_navwhilight.3 = 2, -16.56, -26.51, 3.35, fx_strobelight.4 = 2, -16.56, 26.51, 3.35, fx_strobelight.5 = 1, -40.25, 0.00, 10.01, fx_beaconlight.6 = 4, -11.61, 0.00, 0.98, 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, 180aileron = 200, 1000rudder = 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 = 4direction_indicator.0=3,0[attitude_indicators]//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyroattitude_indicator.0 = 1 [turn_indicators]//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyroturn_indicator.0=1,0[airspeed_indicators]airspeed_indicator.0 = 1.183, -24.75[electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)flap_motor = 0, 5 , 17.0gear_motor = 0, 5 , 17.0autopilot = 0, 5 , 17.0avionics_bus = 0, 5 , 17.0avionics = 1, 5 , 17.0pitot_heat = 0, 2 , 17.0additional_system = 0, 2 , 17.0marker_beacon = 1, 2 , 17.0gear_warning = 0, 2 , 17.0fuel_pump = 0, 5 , 17.0starter1 = 0, 20, 17.0light_nav = 0, 5 , 17.0light_beacon = 0, 5 , 17.0light_landing = 0, 5 , 17.0light_taxi = 0, 5 , 17.0light_strobe = 0, 5 , 17.0light_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, -4.70, 0.00, -5.40, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 0.0, 0.0, 0point.1 = 1, -18.00, -6.00, -5.40, 2500, 1, 0.5, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2point.2 = 1, -18.00, 6.00, -5.40, 2500, 2, 0.5, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3point.3 = 2, -15.90, -26.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5point.4 = 2, -15.90 26.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6point.5= 2, -39.23, 0.0, 0.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9point.6= 2, -2.50, 0.0, -2.17, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4point.7= 2, -42.00, 0.0, 10.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7max_number_of_points = 21static_pitch = 0.24 //degrees, pitch when at rest on the ground (+=Up, -=Dn)static_cg_height= 5.11 //feet, altitude of CG when at rest on the ground[brakes]parking_brake = 1 //Parking brake availabletoe_brakes_scale = 0.68 //Brake scalar[hydraulic_system]normal_pressure = 3000.0 //PSIelectric_pumps = 0 //no electric pumpsengine_map = 1,0,0,0 //pump on Eng1[Views]eyepoint= -12.1, -1.4, 2.12 //(feet) longitudinal, lateral, vertical distance from reference datum[fuel]LeftMain = -17.0, -1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)RightMain = -17.0, 1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetAnumber_of_tank_selectors = 1 electric_pump=1[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn_s, 1[exits]number_of_exits = 2exit_rate.0 = 0.4 ;Percent per secondexit_rate.1 = 0.4 ;Percent per second[airplane_geometry]wing_area = 279.0 //Square feetwing_span = 52.1 //Feetwing_root_chord = 6.4 //Feetwing_dihedral = 3.9 //Degreeswing_incidence = 2.5 //Degreeswing_twist = -1.7 //Degreesoswald_efficiency_factor= 0.7 //Measure of lift effeciency of wingwing_winglets_flag = 0 //Are winglets available?wing_sweep = 0.0 //Degrees, wing leading edgewing_pos_apex_lon = -14.5 //Feet, longitudinal distance from reference point, negative going aftwing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going uphtail_area = 39.0 //Square feethtail_span = 11.7 //Feethtail_pos_lon = -30.9 //Feet, longitudinal distance from reference point, negative going afthtail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going uphtail_incidence = 2.0 //Degreeshtail_sweep = 5.0 //Degrees, horizontal tail leading edgevtail_area = 18.0 //Square feetvtail_span = 4.8 //Feet, tip to bodyvtail_sweep = 45.0 //Degrees, vertical tail leading edgevtail_pos_lon = -28.8 //Feet, longitudinal distance from reference point, negative going aftvtail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going upelevator_area = 16.6 //Square feetaileron_area = 18.3 //Square feetrudder_area = 6.7 //Square feetelevator_up_limit = 28.0 //Degreeselevator_down_limit = 21.0 //Degreesaileron_up_limit = 20.0 //Degreesaileron_down_limit = 15.0 //Degreesrudder_limit = 24.0 //Degreeselevator_trim_limit = 19.5 //Degreesspoiler_limit = 20.0 //Degreesspoilerons_available = 1 //Spoilerons Available?aileron_to_spoileron_gain = 1 //Aileron to spoileron gainmin_ailerons_for_spoilerons = 0 //Degreesmin_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activatespoiler_handle_available = 0 //Defaults to True if spoiler limit > 0, else False. Should be False for spoilerons only[Reference Speeds]flaps_up_stall_speed = 78.0 //Knots True (KCAS)full_flaps_stall_speed = 60.8 //Knots True (KCAS)cruise_speed = 155.0 //Knots True (KTAS)max_mach = 0.60max_indicated_speed = 175 ////Red line (KIAS)[autopilot]autopilot_available= 1flight_director_available= 1default_vertical_speed= 1000.0autothrottle_available= 0pitch_takeoff_ga=8.0max_pitch=10.0max_pitch_acceleration=1.0max_pitch_velocity_lo_alt=2.0max_pitch_velocity_hi_alt=1.5max_pitch_velocity_lo_alt_breakpoint=20000.0max_pitch_velocity_hi_alt_breakpoint=28000.0max_bank=25.0max_bank_acceleration=1.8max_bank_velocity=3.00max_throttle_rate=0.10nav_proportional_control=9.00nav_integrator_control=0.25nav_derivative_control=0.00nav_integrator_boundary=2.50nav_derivative_boundary=0.00gs_proportional_control=9.52gs_integrator_control=0.26gs_derivative_control=0.00gs_integrator_boundary=0.70gs_derivative_boundary=0.00yaw_damper_gain = 0.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[stall_warning]type=2----------------------------------------------------------------------Realairsimulations:[General]atc_type=Cessnaatc_model=C208editable=0performance=Maximum Speedn175 kts 324 km/hrnnCruise Speedn164 kts t 305 km/hr at 20,000 ftnnEnginenPratt & Whitney Canada, Inc., PT6A-114A Free Turbine Flat Rated at 675 Shaft hp nnPropellernThree-Bladed, Constant Speed, Full Feathering, Reversible McCauley, 106-inch diameternnMaximum Rangen5.1 hours maximum cruise at 10,000 ftn6.6 hours maximum cruise at 18,000 ftn6.4 hours maximum range at 10,000 ftn7.2 hours maximum range at 18,000 ftnnService Ceilingn22,800 ft 6,949 mnnFuel Capacityn335 gal 1,268 LnnEmpty Weightn4,040 lb 1,830 kgnnMaximum Gross Weightn8,785 lbt 3,980 kgnnUseful Loadn4,745 lbt 2,150 kgnnLengthn41 ft, 7 in 12.7 mnnWingspann52 ft, 1 int 15.8 mnnHeightn15 ft, 5-1/2 in 4.8 mnnSeatingnUp to 14[WEIGHT_AND_BALANCE]max_gross_weight=8785 // (pounds)empty_weight=4575 // (pounds)reference_datum_position=16.2, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)empty_weight_CG_position=-15.4, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datummax_number_of_stations=50station_load.0=170, -11.3, -1.5, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.1=170, -11.3, 1.5, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.2=150, -13.9, -1.7, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.3=150, -13.9, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.4=170, -17.2, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.5=170, -17.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.6=100, -16.2, 0.0, -3.0 //Cargo Pod (lbs), longitudinal, lateral, vertical positions from datum (feet);Moments of Inertiaempty_weight_pitch_MOI=32000empty_weight_roll_MOI=22000empty_weight_yaw_MOI=15000empty_weight_coupled_MOI=0.0[flight_tuning]cruise_lift_scalar=1.0parasite_drag_scalar=1.0induced_drag_scalar=1.0elevator_effectiveness=1.0aileron_effectiveness=1.0rudder_effectiveness=1.0pitch_stability=1.0roll_stability=1.0yaw_stability=1.0elevator_trim_effectiveness=3.0aileron_trim_effectiveness=1.0rudder_trim_effectiveness=1.0[GeneralEngineData]engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=TurbopropEngine.0=-4.4, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datumfuel_flow_scalar=1.12 //Scalar for fuel flow efficiencymin_throttle_limit=-0.379944[propeller]thrust_scalar=1.0 //Propeller thrust scalarpropeller_type=0 //0=Constant Speed, 1=Fixed Pitchpropeller_diameter=8.8 //Propeller Diameter, (feet)propeller_blades=3 //Number of propeller bladespropeller_moi=19 //Propeller moment of inertiabeta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees)beta_min=15.6 //Minimum blade pitch angle for constant speed prop, (degrees)min_gov_rpm=25520 //Miminum governed RPMprop_tc=0.004 //Prop time-constantgear_reduction_ratio=17.4 //Propeller gear reduction ratiofixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees)low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUEprop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUEprop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUEprop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUEmin_rpm_for_feather=700 //Minimum RPM for prop featheringbeta_feather=88.0 //Feathering pitch angle (degrees)power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propellerdefeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUEminimum_on_ground_beta=0.5 //Miminum pitch angle on ground, (degrees)minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees)[TurbineEngineData]fuel_flow_gain=0.011 //Gain on fuel flowinlet_area=1.0 //Square Feet, engine nacelle inlet arearated_N2_rpm=33000 //RPM, second stage compressor rated valuestatic_thrust=158 //Lbs, max rated static thrust at Sea Level[turboprop_engine]power_scalar=1.0 //Scalar on Turboprop powermaximum_torque=1865 //Maximum torque available (ft-lbs)[Flaps.0]type=1span-outboard=0.5 // Percent span for flap positionextending-time=5.7 // Seconds, time to fully extendsystem_type=0 // 0 = electricalflaps-position.0=0 // degreesflaps-position.1=10 // degreesflaps-position.2=20 // degreesflaps-position.3=30 // degrees[pitot_static]vertical_speed_time_constant=1.0 //Increasing this value will cause a more instantaneous reaction in the VSI[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[LIGHTS]//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -16.30, -26.41, 3.35, fx_navredlight.1=3, -16.30, 26.41, 3.35, fx_navgrelight.2=3, -42.28, 0.00, 2.10, fx_navwhilight.3=2, -16.56, -26.51, 3.35, fx_strobelight.4=2, -16.56, 26.51, 3.35, fx_strobelight.5=1, -40.25, 0.00, 10.01, fx_beaconlight.6=4, -11.61, 0.00, 0.98, 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, 180aileron=200, 1000rudder=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=4direction_indicator.0=3,0[attitude_indicators]//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyroattitude_indicator.0=1 [turn_indicators]//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyroturn_indicator.0=1,0[airspeed_indicators]airspeed_indicator.0=1.183, -24.75[electrical];BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)flap_motor=0, 5 , 17.0gear_motor=0, 5 , 17.0autopilot=0, 5 , 17.0avionics_bus=0, 5 , 17.0avionics=1, 5 , 17.0pitot_heat=0, 2 , 17.0additional_system=0, 2 , 17.0marker_beacon=1, 2 , 17.0gear_warning=0, 2 , 17.0fuel_pump=0, 5 , 17.0starter1=0, 20, 17.0light_nav=0, 5 , 17.0light_beacon=0, 5 , 17.0light_landing=0, 5 , 17.0light_taxi=0, 5 , 17.0light_strobe=0, 5 , 17.0light_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, -4.70, 0.00, -5.38, 1500, 0, 0.5, 35.0, 0.2, 2.5, 0.6, 0.0, 0.0, 0point.1=1, -16.77, -6.00, -5.40, 2500, 1, 0.5, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2point.2=1, -16.77, 6.00, -5.40, 2500, 2, 0.5, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3point.3=2, -15.90, -26.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5point.4=2, -15.90 26.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6point.5=2, -39.23, 0.0, 0.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9point.6=2, -2.50, 0.0, -2.17, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4point.7=2, -42.00, 0.0, 10.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7max_number_of_points=21static_pitch=0.24 //degrees, pitch when at rest on the ground (+=Up, -=Dn)static_cg_height=5.11 //feet, altitude of CG when at rest on the ground[brakes]parking_brake=1 //Parking brake availabletoe_brakes_scale=0.68 //Brake scalar[hydraulic_system]normal_pressure=3000.0 //PSIelectric_pumps=0 //no electric pumpsengine_map=1,0,0,0 //pump on Eng1[Views]eyepoint=-12.5, -1.4, 2.12 //(feet) longitudinal, lateral, vertical distance from reference datum[fuel]LeftMain=-18.4, -1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)RightMain=-18.4, 1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetAnumber_of_tank_selectors=1 electric_pump=1[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn_s, 1[exits]number_of_exits=2exit_rate.0=0.4 ;Percent per secondexit_rate.1=0.4 ;Percent per second[airplane_geometry]wing_area=279.0 //Square feetwing_span=52.1 //Feetwing_root_chord=6.4 //Feetwing_dihedral=3.9 //Degreeswing_incidence=2.5 //Degreeswing_twist=-1.7 //Degreesoswald_efficiency_factor=0.7 //Measure of lift effeciency of wingwing_winglets_flag=0 //Are winglets available?wing_sweep=0.0 //Degrees, wing leading edgewing_pos_apex_lon=-16.0 //Feet, longitudinal distance from reference point, negative going aftwing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going uphtail_area=39.0 //Square feethtail_span=11.7 //Feethtail_pos_lon=-30.9 //Feet, longitudinal distance from reference point, negative going afthtail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going uphtail_incidence=2.0 //Degreeshtail_sweep=5.0 //Degrees, horizontal tail leading edgevtail_area=18.0 //Square feetvtail_span=4.8 //Feet, tip to bodyvtail_sweep=45.0 //Degrees, vertical tail leading edgevtail_pos_lon=-28.8 //Feet, longitudinal distance from reference point, negative going aftvtail_pos_vert=1.5 //Feet, vertical distance from reference point, positive going upelevator_area=16.6 //Square feetaileron_area=18.3 //Square feetrudder_area=6.7 //Square feetelevator_up_limit=28.0 //Degreeselevator_down_limit=21.0 //Degreesaileron_up_limit=20.0 //Degreesaileron_down_limit=15.0 //Degreesrudder_limit=24.0 //Degreeselevator_trim_limit=19.5 //Degreesspoiler_limit=20.0 //Degreesspoilerons_available=1 //Spoilerons Available?aileron_to_spoileron_gain=1 //Aileron to spoileron gainmin_ailerons_for_spoilerons=0 //Degreesmin_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate[Reference Speeds]flaps_up_stall_speed=66.0 //Knots True (KTAS)full_flaps_stall_speed=52.8 //Knots True (KTAS)cruise_speed=175.0 //Knots True (KTAS)max_indicated_speed=180.000000max_mach=1.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1000.0autothrottle_available=0autoland_available=0pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=1.000000max_pitch_velocity_lo_alt=2.000000max_pitch_velocity_hi_alt=1.500000max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=1.800000max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[stall_warning]type=2

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