[fltsim.0] title=DHC-2 16555 sim=DHC-2 model= panel= sound= texture= kb_checklists=DHC2_check kb_reference=DHC2_ref atc_id=N7783P editable=0 ui_manufacturer=De Havilland Beaver ui_type=DHC-2 Beaver MKI (Wheels) ui_variation=USAF 16555 description=The Beaver was the second design from de Havilland Canada, and is well known for its 'bush' flying role. The aircraft was developed with an eye to the Ontario Department of Lands and Forests which was looking to replace its Stinson SR-9s. The aircraft might have looked very different as it was originally planned for the 295hp Gypsy Queen 50, but development delays for that engine resulted in a change to the 450hp Pratt & Whitney R-985 Wasp Junior. First flying on August 16 1947, and beginning deliveries in April 1948, production did not cease until 1967 for a total of 1,657 aircraft (not counting the Mk.3 'Turbo' Beaver). [WEIGHT_AND_BALANCE] max_gross_weight=5100 // (pounds) empty_weight=2850 // (pounds) reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=-0.250000,0.000000,0.000000 max_number_of_stations=50 station_load.0="215.00, 2.25, -1.20, 1.75,Pilot" station_load.1="000.00, 2.25, 1.20, 1.75,CoPilot" station_load.2="000.00, -2.25, -1.20, 1.75,Passenger 1" station_load.3="000.00, -2.25, 1.20, 1.75,Passenger 2" station_load.4="000.00, -5.00, -1.20, 1.75,Passenger 3" station_load.5="000.00, -5.00, 1.20, 1.75,Passenger 4" station_load.6="000.00, -6.80, 0.00, 0.70,Baggage" empty_weight_roll_MOI=5343.00000 empty_weight_pitch_MOI=5767.00000 empty_weight_yaw_MOI=9367.00000 empty_weight_coupled_MOI=0.00000 [fuel] Center1=-1.50, 0.00, -0.75, 35.00, 0.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=0.30, 0.00, -0.75, 35.00, 0.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-3.00, 0.00, -0.75, 26.00, 0.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=1.00 number_of_tank_selectors=1 electric_pump=1 [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=250.00 wing_span=48.00 wing_root_chord=5.25 wing_dihedral=1.999512 wing_incidence=1.499634 wing_twist=0.000000 oswald_efficiency_factor=0.750294 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.00 wing_pos_apex_vert=4.00 htail_area=26.25 htail_span=17.00 htail_pos_lon=-21.00 htail_pos_vert=2.00 htail_incidence=0.417480 htail_sweep=0.00 vtail_area=30.00 vtail_span=6.244998 vtail_sweep=0.00 vtail_pos_lon=-20.00 vtail_pos_vert=4.00 elevator_area=27.95 aileron_area=25.00 rudder_area=10.50 elevator_up_limit=28.00 elevator_down_limit=20.00 aileron_up_limit=18.00 aileron_down_limit=11.00 rudder_limit=25.00 elevator_trim_limit=19.480565 spoiler_limit=0.000057 spoilerons_available=0 aileron_to_spoileron_gain=0.00 min_ailerons_for_spoilerons=0.00 min_flaps_for_spoilerons=0.00 //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=1.00, -20.41, 0.00, -1.60, 1500.00, 0.00, 0.50, 45.0, 0.52, 2.50, 0.73, 0.00, 0.00, 0.00 point.1=1.00, 2.00, -5.08, -5.25, 3500.00, 1.00, 0.53, 0.00, 0.52, 2.50, 0.73, 5.00, 5.00, 2.00 point.2=1.00, 2.00, 5.08, -5.25, 3500.00, 2.00, 0.53, 0.00, 0.52, 2.50, 0.73, 5.00, 5.00, 2.00 point.3=2.00, 0.00, -24.00, 4.00, 308.47, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00 point.4=2.00, 0.00, 24.00, 4.00, 308.47, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00 point.5=2.00, -21.83, 0.00, 0.33, 916.56, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00 point.6=2.00, 6.50, 0.00, -2.16, 1274.43, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00 point.7=2.00, 0.00, -24.00, 4.00, 308.47, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 7.00 point.8=2.00, -19.58, 0.00, 7.50, 30.03, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 8.00 static_pitch=10.00 static_cg_height=4.489594 gear_system_type=0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 1.00, -24.90, 4.45, fx_navred light.1=3, 1.00, 24.90, 4.45, fx_navgre light.2=2, 0.85, -24.90, 4.45, fx_strobe light.3=2, 0.85, 24.90, 4.45, fx_strobe light.4=1, -5.95, 0.00, 4.50, fx_beacon [SMOKESYSTEM] smoke.0=-0.20, 1.20, -1.55, fx_smoke_d3_fx [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [Flaps.0] type=1 span-outboard=0.50 extending-time=7.00 system_type=0 flaps-position.0=00.00 flaps-position.1=08.25 flaps-position.2=16.50 flaps-position.3=25.00 flaps-position.4=33.00 flaps-position.5=41.00 flaps-position.6=49.00 flaps-position.7=58.00 damaging-speed=100 // KIAS blowout-speed=120 // KIAS lift_scalar=1.8 drag_scalar=0.6 pitch_scalar=0.2 [GeneralEngineData] engine_type=0 Engine.0=2.00, 0.00, 0.75 fuel_flow_scalar=0.92 min_throttle_limit=0.000000 [piston_engine] cylinder_displacement=109.440000 compression_ratio=6.700000 number_of_cylinders=9 max_rated_rpm=2300.000000 max_rated_hp=450.000000 fuel_metering_type=2 cooling_type=0 normalized_starter_torque=0.18 turbocharged=1 max_design_mp=37.000000 min_design_mp=8.000000 critical_altitude=5000.000000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 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 [propeller] propeller_type=0 propeller_diameter=9.00 propeller_blades=3 propeller_moi=8.00 beta_max=24.00 beta_min=10.50 min_gov_rpm=1400.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=0.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Reference Speeds] flaps_up_stall_speed=52.00 full_flaps_stall_speed=38.00 cruise_speed=112.00 max_indicated_speed=180.000000 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint=0.00,0.00,1.00 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [direction_indicators] direction_indicator.0=1,0 [General] atc_type=DeHavilland atc_model=DHC2 performance=-Dimensions \nSpan : 48'0 ft \nLength : 30'4 ft \nHeight : 9'0 ft \n-Weight \nempty : 2,850 lb \nmax : 5,100 lb \n-Power Plant : 450hp P&W R-985-AN Wasp Junior \n-Performance : \nmax speed : 140 mph \nceiling : 18.000ft\nrange : 778 miles \n\nAircraft by: Steven Grant - August 2002 [brakes] toe_brakes_scale=1.023469 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0