[fltsim.0] title=dukeb60 sim=dukeb60 model= panel= sound= texture= checklists= atc_id=N8511L ui_manufacturer=Beechcraft description=The Beechcraft Duke is one of the coolest aircraft ever. This one was created with Flight Sim Design Studio (FSDS) by ABACUS Publishing (abacuspub.com). ui_type=Duke B60 ui_variation=White with Turquoise [General] performance=Cruise Speed: 283 mph\nMaximum Range: 1,287 sm\nService Ceiling: 35,800 ft\nMax Gross Weight: 6,775 lb\nHorsepower: 380 x 2\nDesigner: Chuck Dome\nDate: November, 2002 atc_type=duke editable=1 [WEIGHT_AND_BALANCE] max_gross_weight= 5524.000 empty_weight= 3911.000 reference_datum_position= 6.960, 0.000, 0.000 empty_weight_CG_position= -6.060, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, -6.540, -1.200, 0.000 station_load.1= 170.000, -6.540, 1.200, 0.000 station_load.2= 170.000, -9.800, -1.200, 0.000 station_load.3= 170.000, -9.800, 1.200, 0.000 station_load.4=0, -12.67, -1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=0, -12.67, 1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=0, -15.00, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI= 3905.650 empty_weight_roll_MOI= 2718.640 empty_weight_yaw_MOI= 5291.040 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [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= -1.400, -5.300, 0.000 Engine.1= -1.400, 5.300, 0.000 fuel_flow_scalar= 0.500 [piston_engine] power_scalar=1.000 cylinder_displacement= 91.700 compression_ratio= 8.000 number_of_cylinders= 12 max_rated_rpm= 2700.000 max_rated_hp= 500.000 fuel_metering_type= 0 cooling_type= 0 normalized_starter_torque= 0.300 turbocharged= 1 max_design_mp= 0.000 min_design_mp= 1.000 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=1.000 [propeller] thrust_scalar=1.000 propeller_type= 0 propeller_diameter= 6.400 propeller_blades= 3 propeller_moi= 6.900 beta_max= 45.000 beta_min= 15.200 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= 1 prop_deice_available= 1 prop_feathering_available= 1 prop_auto_feathering_available= 0 min_rpm_for_feather= 700.000 beta_feather= 82.500 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 [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 (0=Undamped, 1=Critically Damped) //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) //GEAR point.0= 1.000, 0.820, 0.000, -4.000, 1600.000, 0.000, 0.633, 40.000, 0.200, 2.500, 0.900, 3.000, 3.000, 0.000, 0.000, 0.000 point.1= 1.000, -8.040, -4.790, -4.100, 1600.000, 1.000, 0.886, 0.000, 0.500, 2.500, 0.850, 4.100, 4.300, 2.000, 152.000, 337.611 point.2= 1.000, -8.040, 4.790, -4.100, 1600.000, 2.000, 0.886, 0.000, 0.500, 2.500, 0.850, 4.300, 4.100, 3.000, 152.000, 337.611 //SCRAPES point.3= 2.000, -6.200, -18.910, 0.500, 800.000, 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, -6.200, 18.910, 0.500, 800.000, 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, -24.040, 0.000, -0.500, 800.000, 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, 0.400, 0.000, -1.240, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 1.560 static_cg_height= 3.430 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 [pitot_static] vertical_speed_time_constant=1.0 //Increasing this value will cause a more instantaneous reaction in the VSI [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [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 [Views] eyepoint=-4.500, -1.000, 3.00 //Longitudinal, Lateral, Vertical (feet) [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=150, 250 aileron=150, 250 rudder=150, 250 [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=3,0 [fuel] LeftMain= -8.460, -6.450, 0.000, 71.000, 0.000 RightMain= -8.460, 6.450, 0.000, 71.000, 0.000 fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=2 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [airplane_geometry] wing_area= 199.000 wing_span= 37.800 wing_root_chord= 5.300 wing_dihedral= 6.900 wing_incidence= 1.000 wing_twist= -1.000 oswald_efficiency_factor= 0.700 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= -5.600 wing_pos_apex_vert= 0.000 htail_area= 60.000 htail_span= 15.900 htail_pos_lon= -20.100 htail_pos_vert= 0.000 htail_incidence= 0.500 htail_sweep= 0.000 vtail_area= 88.000 vtail_span= 10.700 vtail_sweep= 0.000 vtail_pos_lon= -22.900 vtail_pos_vert= 3.100 elevator_area= 20.000 aileron_area= 11.300 rudder_area= 10.500 elevator_up_limit= 17.000 elevator_down_limit= 15.500 aileron_up_limit= 18.000 aileron_down_limit= 18.000 rudder_limit= 30.000 elevator_trim_limit= 15.000 spoiler_limit= 90.000 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= 96.000 full_flaps_stall_speed= 76.800 cruise_speed= 200.000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 use_no_default_bank=1 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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 [Flaps.0] type= 1 span-outboard= 0.410 extending-time= 4.000 system_type= 0 damaging-speed= 152.000 blowout-speed= 250.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 30.000, 0.000
