[fltsim.0] title=DHC-2 Turbo Beaver [wheel] sim=BvrtW visual_damage=1 model= panel= sound= texture= kb_checklists=Bvrtw_check kb_reference=Bvrtw_ref atc_id=N2543D ui_manufacturer=de Havilland ui_type=DHC-2 Turbo Beaver Mklll ui_variation=Wheel description=de Havilland DHC-2T Turbo Beaver Mk III atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=Turbo Beaver atc_model=DHC2T performance=Length: 35 ft 3 in\nWing span: 48 ft\nWeight:2760 \/ 5370 lb\nPower: 550 hp P&W PT6A-20 Turbine\nDesigner: Fred Banting\nDate: Nov 2001\nRepaint by Lawrance Mouat\n18\/04\/2003 [WEIGHT_AND_BALANCE] empty_weight= 2760.000 max_gross_weight= 5370.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=10 ;MAX load (including fuel) 2610 lbs. ;Weight (lbs), long, lat, vert positions from datum (feet) station_load.0= 170.000, 3.080, -1.100, -0.500 station_load.1= 370.000, 0.750, 0.000, -0.500 station_load.2= 750.000, -2.400, 0.000, -0.500 station_load.3= 100.000, -6.400, 1.700, -1.500 station_load.5=100, -6.40, 1.7, -1.5 //Emergency Equipment station_load.6=000, -7.80, 0.0, 1.0 //Baggage empty_weight_roll_MOI= 18825.000 empty_weight_pitch_MOI= 26000.000 empty_weight_yaw_MOI= 32500.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 station_load.4= 100.000, -6.400, 1.700, -1.500 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=100.0 ;BusType, MaxAmpLoad, MinVoltage ;BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 autopilot=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 10, 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=0, 0 Nav.1=1, 1, 0 Nav.2=0, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -0.2, -24.45, 3.85, fx_navred , light.1=3, -0.2, 24.45, 3.85, fx_navgre , light.2=3, -22.7, 0.00, 0.85, fx_navwhi , //light.3=2, -6.35, 0.0, 3.3, fx_strobe , [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1000.0 autothrottle_available=0 pitch_takeoff_ga=8.0 [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 [effects] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] Center1= -3.330, 0.000, -1.500, 24.000, 0.000 LeftMain= 2.580, 0.000, -1.500, 51.000, 0.000 RightMain= -0.625, 0.000, -1.500, 67.000, 0.000 RightAux= -0.830, 0.000, 4.000, 43.000, 0.000 fuel_type=2.0 //1=Avgas, 2=JetA number_of_tank_selectors=1 [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) // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0= 1.000, -20.400, 0.000, -2.350, 1600.000, 0.000, 0.660, 90.000, 0.460, 2.500, 0.790, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, 2.580, -5.100, -6.580, 1600.000, 1.000, 0.830, 0.000, 0.540, 2.500, 0.790, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, 2.580, 5.100, -6.580, 1600.000, 2.000, 0.830, 0.000, 0.540, 2.500, 0.790, 0.000, 0.000, 3.000, 0.000, 0.000 // Scrapes point.3= 2.000, 0.000, -24.000, 4.000, 308.500, 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, 24.000, 4.000, 308.500, 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, -22.000, 0.000, 0.300, 916.500, 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, 11.000, 0.000, -1.000, 1274.500, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.7= 2.000, -19.600, 0.000, 7.500, 308.500, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 static_pitch= 10.795 static_cg_height= 5.500 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 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 [airplane_geometry] wing_area= 252.000 wing_span= 48.000 wing_root_chord= 5.208 wing_dihedral= 2.000 wing_incidence= 0.689 wing_twist= 0.000 oswald_efficiency_factor= 0.890 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 1.458 wing_pos_apex_vert= 4.000 htail_area= 65.000 htail_span= 15.830 htail_pos_lon= -19.583 htail_pos_vert= 0.000 htail_incidence= 1.374 htail_sweep= 0.000 vtail_area= 48.000 vtail_span= 6.245 vtail_sweep= 0.000 vtail_pos_lon= -19.167 vtail_pos_vert= 5.833 elevator_area= 17.950 aileron_area= 25.000 rudder_area= 16.500 elevator_up_limit= 28.000 elevator_down_limit= 20.000 aileron_up_limit= 18.000 aileron_down_limit= 11.000 rudder_limit= 25.000 elevator_trim_limit= 20.000 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 [propeller] propeller_type= 0 propeller_diameter= 8.500 propeller_blades= 3 propeller_moi= 10.750 beta_max= 45.000 beta_min= 14.000 min_gov_rpm= 26670.000 prop_tc= 0.008 gear_reduction_ratio= 15.875 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 1 prop_auto_feathering_available= 0 min_rpm_for_feather= 700.000 beta_feather= 84.000 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 1 minimum_on_ground_beta= 1.000 minimum_reverse_beta= -14.000 [Reference Speeds] flaps_up_stall_speed= 52.000 full_flaps_stall_speed= 41.000 cruise_speed= 125.000 [GeneralEngineData] engine_type= 5 Engine.0= 11.700, 0.000, -0.700 fuel_flow_scalar= 1.000 [TurbineEngineData] fuel_flow_gain= 0.028 inlet_area= 0.680 rated_N2_rpm= 38100.000 static_thrust= 88.000 afterburner_available= 0 [turboprop_engine] maximum_torque= 1825.000 [keyboard_response] elevator=85.0,135.0 aileron=75.0,135.0 rudder=100.0,135.0 [Views] eyepoint=3.203945,-1.320025,2.665682 [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 [Flaps.0] type= 1 span-outboard= 0.600 extending-time= 7.000 system_type= 3 damaging-speed= 0.000 blowout-speed= 0.000 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= 17.000, 0.000 flaps-position.3= 23.000, 0.000 flaps-position.4= 30.000, 0.000 flaps-position.5= 37.000, 0.000 flaps-position.6= 43.000, 0.000 flaps-position.7= 50.000, 0.000 flaps-position.8= 60.000, 0.000