[fltsim.0] title=DHC-2 Beaver Harbour Air sim=Bvr7F model= panel= sound= texture= kb_checklists=Beaverf_check kb_reference=Beaverf_ref atc_id=NUSA3F ui_manufacturer=de Havilland ui_type=DHC-2 Beaver Harbour Air ui_variation=Float description=de Havilland Canada DHC-2 Beaver MkI. The world's greatest bush plane. [General] editable=0 atc_type=Beaver atc_model=DHC2 performance=Length: 30' 4'\nWing span: 48 '\nWeight: 3316 lb \/ 5090 lb\nPower: 450 hp P&W R-985 Wasp Jr. radial\n\nDesigner: Fred Banting\nDate: Nov 2001\n [WEIGHT_AND_BALANCE] max_gross_weight=5090.0 empty_weight=3316 reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=10 ;MAX station loads (Including Fuel) 1774 lbs. ;Weight (lbs), long, lat, vert positions from datum (feet) station_load.0=170, 0.7, -1.1, -0.6 //Pilot station_load.1=000, 0.7, 1.1, -0.6 //Front Passenger station_load.2=460, -1.6, 0.0, -0.6 //Freight Forward station_load.3=000, -4.7, 0.0, -0.6 //Freight Rear station_load.4=100, -6.5, 1.0, -1.5 //Emergency equipment station_load.5=000, -7.8, 0.0, 1.0 //Baggage compartment ;Moments of Inertia empty_weight_roll_MOI=10835.0 empty_weight_pitch_MOI=13150.0 empty_weight_yaw_MOI=24125.0 empty_weight_coupled_MOI=0.0 CG_forward_limit= 0.0 CG_aft_limit= 1.0 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=50.0 ;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 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, 0 Com.2=0, 0 Nav.1=1, 0, 0 Nav.2=0, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=0 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.0 use _no_default_bank=1 use _no_default_pitch=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.4, -24.4, 3.85, fx_navred , light.1=3, 0.4, 24.4, 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 , [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 [effects] wake=fx_wake water=/fx_spray water=fx_waterland dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] Center1=-1.5,0.0,-1.5,35.0,0.0 //Long, Lat, Vert, Useable, Unuseable LeftMain=0.3,0.0,-1.5,35.0,0.0 RightMain=-3.0,0.0,-1.5,26.0,0.0 fuel_type=1.0 //1=Avgas, 2=JetA number_of_tank_selectors=1 [contact_points] //0 Class //1 Longitudinal Position (feet, + = fwd) //2 Lateral Position (feet, + = right) //3 Vertical Position (feet, + = above) //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=4, 9.5, -5.1, -6.75, 1600, 0, 0.0, 25.0, 0.4, 2.2, 0.75, 0.0, 0.0, 2, 0.0, 0.0 point.1=4, 9.5, 5.1, -6.75, 1600, 0, 0.0, 25.0, 0.4, 2.2, 0.75, 0.0, 0.0, 3, 0.0, 0.0 point.2=4, -6.5, -5.1, -6.55, 1600, 0, 0.0, 0.0, 0.4, 2.2, 0.75, 0.0, 0.0, 2, 0.0, 0.0 point.3=4, -6.5, 5.1, -6.55, 1600, 0, 0.0, 0.0, 0.4, 2.2, 0.75, 0.0, 0.0, 3, 0.0, 0.0 // Scrapes 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, 5, 0.0, 0.0 //left wing point.5=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.6=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.7=2, 6.5, 0.0, -2.2, 1274.5, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 //nose point.8=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 //point.9=5, -12.5, -5.1, -6.75, 1600, 0, 0.00, 40.0, 0.0, 0.0, 1.0, 1.0, 1.2, 0, 0.0, 0.0 //left water rudder //point.10=5, -12.5, 5.1, -6.75, 1600, 0, 0.00, 40.0, 0.0, 0.0, 1.0, 1.1, 1.5, 0, 0.0, 0.0 //right water rudder max_number_of_points=21 static_pitch=1.345825 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=6.014998 //feet, altitude of CG when at rest on the ground [Flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.6 // Percent span for flap position extending-time=7.0 // Seconds, time to fully extend system_type=3 //0=Elec, 1=Hyd, 2=Pneu, 3=Man, 4=None system_type= 3 damaging-speed= 0.0 //KIAS blowout-speed= 0.00 //KIAS lift_scalar= 1.0 drag_scalar= 1.0 pitch_scalar= 1.0 flaps-position.0= 0.0, 0.0 flaps-position.1= 10.0, 0.0 flaps-position.2= 17.0, 0.0 flaps-position.3= 23.0, 0.0 flaps-position.4= 30.0, 0.0 flaps-position.5= 37.0, 0.0 flaps-position.6= 43.0, 0.0 flaps-position.7= 50.0, 0.0 flaps-position.8= 60.0, 0.0 [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=252.0 wing_span=48.0 wing_root_chord=5.208333 wing_dihedral=2.0 wing_incidence=.689 wing_twist=0.0 oswald_efficiency_factor=0.89 //lift effeciency of wing wing_winglets_flag=0 wing_sweep=0.0 //Degrees, wing leading edge wing_pos_apex_lon=1.458 //Feet, longitudinal from reference point, negative going aft wing_pos_apex_vert=4.0 //Feet, vertical from reference point, positive going up htail_area=65.0 htail_span=15.83 htail_pos_lon=-19.583 htail_pos_vert=0.0 htail_incidence=1.374 htail_sweep=0.0 vtail_area=30.0 vtail_span=6.245 //Feet, tip to body vtail_sweep=0.0 vtail_pos_lon=-19.583 vtail_pos_vert=6.5 elevator_area=17.95 aileron_area=25.00 rudder_area=10.5 elevator_up_limit=28.0 elevator_down_limit=20.0 aileron_up_limit=18.0 aileron_down_limit=11.0 rudder_limit=25.0 elevator_trim_limit=20.0 spoiler_limit=0.000057 spoilerons_available=0 aileron_to_spoileron_gain=0.0 min_ailerons_for_spoilerons=0.0 min_flaps_for_spoilerons=0.0 [propeller] thrust_scalar=1.0 propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=8.5 propeller_blades=2 propeller_moi=8.0 beta_max=43.0 beta_min=15.0 min_gov_rpm=1400.0 prop_tc=0.1 gear_reduction_ratio=1.0 fixed_pitch_beta=0.0 low_speed_theory_limit=80.0 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.0 beta_feather=0.0 power_absorbed_cf=0.0 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.0 minimum_reverse_beta=0.0 [Reference Speeds] flaps_up_stall_speed=52.0 //Knots True (KTAS) full_flaps_stall_speed=41.0 cruise_speed=124.0 [GeneralEngineData] engine_type=0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=7.25,0.0,0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=109.44 //Cubic inches per cylinder compression_ratio=6.7 number_of_cylinders=9 max_rated_rpm=2300.0 max_rated_hp=450.0 fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque=0.155 //Starter torque factor turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp=36.5 //Max design manifold pressure, (inHg) min_design_mp=1.0 //Min design manifold pressure, (inHg) critical_altitude=15000.0 //Altitude to which turbocharger will provide max manifold pressure (feet) emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=WEP emergency_boost_mp_offset=0.0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset=0.0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction [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=85,135 aileron=75,135 rudder=100,135 [Views] eyepoint=0.884289,-1.320025,2.665682 //(feet) longitudinal, lateral, vertical distance from reference datum [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
