[fltsim.0] title=ATC DHC-2 Turbo Beaver sim=F33An model= panel= sound= texture= atc_id=C-FBKB atc_heavy=0 ui_manufacturer=ATC ui_type=de Havilland DHC-2 Turbo Beaver Mklll ui_variation=C-FBKB description=de Havilland DHC-2T Turbo Beaver Mk III [General] atc_type=DEHAVILLAND atc_model=DH2T performance=Length: 35 ft 3 in\nWing span: 48 ft\nWeight: 2996 \/ 5370 lb\nPower: 550 hp P&W PT6A-20 Turbine\nDesigner: Fred Banting\nDate: Nov 2001\n [WEIGHT_AND_BALANCE] 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.0=0.000000,0.000000,0.000000,0.000000 empty_weight=1800.000 empty_weight_roll_MOI=2400.000 empty_weight_pitch_MOI=5200.000 empty_weight_yaw_MOI=4400.000 empty_weight_coupled_MOI=0.000 max_gross_weight=2244.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [Reference Speeds] flaps_up_stall_speed=52.0 full_flaps_stall_speed=41.0 cruise_speed=125.0 [flight_tuning] cruise_lift_scalar=0.900 parasite_drag_scalar=0.900 induced_drag_scalar=0.900 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.500 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 [airplane_geometry] wing_area=182.000 wing_span=33.500 wing_root_chord=4.917 wing_dihedral=5.999 wing_incidence=0.000 wing_twist=-0.994 oswald_efficiency_factor=1.008 //was 1.508 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=1.229 wing_pos_apex_vert=0.000 htail_area=38.000 htail_span=10.500 htail_pos_lon=-13.917 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=0.000 vtail_area=15.000 vtail_span=4.416 vtail_sweep=0.000 vtail_pos_lon=-14.583 vtail_pos_vert=1.500 elevator_area=16.610 aileron_area=18.300 rudder_area=6.650 elevator_up_limit=28.000 elevator_down_limit=20.999 aileron_up_limit=19.996 aileron_down_limit=15.000 rudder_limit=23.995 elevator_trim_limit=19.498 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 [ground_reaction] main_gear_static_compression=0.3 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.3 // (feet), The distance the center gear strut is compressed when at rest on the ground main_gear_damping_ratio=1.0 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=1.0 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [pitot_static] vertical_speed_time_constant=1.0 [propeller] thrust_scalar=1.500 propeller_type=0 propeller_diameter=6.833 propeller_blades=2 propeller_moi=5.000 beta_max=43.000 beta_min=15.000 min_gov_rpm=1100.000 prop_tc=0.100 gear_reduction_ratio=1.000 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 [piston_engine] power_scalar=1.000 cylinder_displacement=86.667 compression_ratio=8.500 number_of_cylinders=6 max_rated_rpm=2700.000 max_rated_hp=285.000 fuel_metering_type=0 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=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [fuel] LeftMain=0.000, -13.333, 0.000, 37.000, 0.000 RightMain=0.000, 13.333, 0.000, 37.000, 0.000 fuel_type=1.000000 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) // vertical positions were -2.35 -6.85 point.0=1, -20.4, 0.0, -1.95, 1600, 0, 0.66, 90.0, 0.46, 2.5, 0.79, 0.0, 0.0, 0, 0.0, 0.0 point.1=1, 2.58, -5.1, -6.18, 1600, 1, 0.83, 0.0, 0.54, 2.5, 0.79, 0.0, 0.0, 2, 0.0, 0.0 point.2=1, 2.58, 5.1, -6.18, 1600, 2, 0.83, 0.0, 0.54, 2.5, 0.79, 0.0, 0.0, 3, 0.0, 0.0 // Scrapes point.3=2, 0.0, -24.0, 4.0, 308.5, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 //left wing point.4=2, 0.0, 24.0, 4.0, 308.5, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 //right wing point.5=2, -22.0, 0.0, 0.3, 916.5, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 //tail cone point.6=2, 11.0, 0.0, -1.0, 1274.5, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 //nose point.7=2, -19.6, 0.0, 7.5, 308.5, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0 //tail static_pitch=10.795 static_cg_height=5.05 //was 5.5 [Views] eyepoint=3.203945,-1.320025,2.665682 [GeneralEngineData] engine_type=0 Engine.0=8.333, 0.000, 1.250 fuel_flow_scalar=1.000 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [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=700.000000 autothrottle_available=0 pitch_takeoff_ga=8 [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [direction_indicators] direction_indicator.0=1,0 [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 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits=2 exit_rate.0=0.4 exit_rate.1=0.4 [Flaps.0] type=1 span-outboard=0.500 extending-time=5.000 system_type=0 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=16., 0.000 flaps-position.2=37.999, 0.000 [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