// DHC2 MKIII TURBO BEAVER AMPHIBIAN MK3 C-FOPA ver2.7 // Copyright Premier Aircraft Design 2006 [fltsim.0] title=TurboBeaver_Mk3 C-FOPA sim=TurboBeaver_Mk3 model= panel=FOPA sound= texture=FOPA kb_checklists=DHC2_Mk3A_Check kb_reference=DHC2_Mk3A_Ref atc_id=C-FOPA atc_airline= atc_flight_number= atc_parking_types=RAMP ui_manufacturer="de Havilland" ui_type="Turbo Beaver DHC2 Mk3" ui_variation="Ontario Ministry NR C-FOPA" ui_typerole="Single Engine TurboProp" ui_createdby="Premier Aircraft Design" description=Ontario Ministry of Natural Resources DHC2MkIII Turbo Beaver C-FOPA. The Turbo Beaver is the first single-engine utility aircraft to be turbine powered.\nvisit Premier Aircraft Design at:\nwww.premaircraft.com visual_damage=0 editable=1 [General] atc_type=DeHavilland atc_model=DHC2 performance=Engine - P & W Canada PT6A-27 Turbine 680 SHP\nWingspan - 14.6 m (48 ft.)\nLength - 10.74 m (35 ft 3 in)\nWing area - 23.2 sq m (250 sq ft)\nWeight Empty - 1175 kg. (2590 lb.)\nMTOW - 2436 kg. (5370 lb.)\nNormal Cruise Max - 140 kts IAS\nNever Exceed - 160 mph IAS\nRate of Climb - 1500 ft/min\nService Ceiling- 23,000 ft\nFuel Capacity - 186 US gal. Category=airplane [Views] eyepoint=3.30, -1.00, 2.25 //2.15(feet) longitudinal, lateral, vertical distance from reference datum [weight_and_balance] max_gross_weight =6000 empty_weight = 2790 reference_datum_position = 0, 0, 0 empty_weight_CG_position = -1, 0, 0 empty_weight_pitch_MOI = 7241.36 empty_weight_roll_MOI = 5618.57 empty_weight_yaw_MOI = 10431.43 empty_weight_coupled_MOI = 0 max_number_of_stations = 7 station_load.0 = 170, 3.08, -1.1, -0.5 station_load.1 = 170, 3.08, 1.1, -0.5 station_load.2 = 360, 0.75, 0.0, 0.0 station_load.3 = 455, -2.40, 0.0, 0.0 station_load.4 = 100, -5.16, 0.0, 0.0 station_load.5 = 100, -6.40, 0.0, 1.0 station_load.6 = 000, -7.80, 0.0, 1.0 [SMOKESYSTEM] smoke.0=0.00, 10.00, 6.00,fx_PADwater2, smoke.1=0.00, 10.00, -6.00, fx_PADwater2, [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 0.20, -24.10, 3.72, fx_PADnavred , light.1 = 3, 0.20, 24.10, 3.72, fx_PADnavgre , light.2 = 3, -22.60, 0.00, 1.30, fx_PADnavwhi , light.3 = 2, -0.20, -24.10, 3.75, fx_PADstrobeh , light.4 = 2, -0.20, 24.10, 3.75, fx_PADstrobeh , light.5 = 1, -6.20, 0.00, 3.60, fx_PADbeaconh , light.6 = 4, 4.00, -1.00, 1.50, fx_vclightwhite , light.7 = 4, 4.00, 1.00, 1.50, fx_vclightwhite , light.8 = 4, -1.50, 0.00, 1.50, fx_vclightwhite , light.9 = 4, -5.00, 0.00, 1.50, fx_vclightwhite , [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 5 fuel_flow_scalar = 1.12 engine.0 = 10.0, 0.0, 0.0 min_throttle_limit=-0.250000 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 Center1 = 0, 0, -1.5, 80, 1 LeftMain = 1.5, 0, -1.5, 80,1 RightMain = -1.5, 0, -1.5, 23, 1 electric_pump=1 [contact_points] //Classes...What type of point 0=Unused or Ignore // 1=Wheel // 2=Scrape point // 4=Float // 5=Float Rudder //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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal //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) point.0 = 1, 13.40, -5.60, -8.00, 1600, 0, 1.40, 45.0, 0.3, 2.5, 0.80, 4.0, 4.0, 0, 175.0, 175.0 point.1 = 1, 13.40, 5.60, -8.00, 1600, 0, 1.40, 45.0, 0.3, 2.5, 0.80, 4.0, 4.0, 1, 175.0, 175.0 point.2 = 1, -2.20, -5.60, -7.900, 1600, 1, 1.50, 0.0, 0.4, 2.5, 0.80, 4.0, 4.0, 2, 175.0, 175.0 point.3 = 1, -2.20, 5.60, -7.900, 1600, 2, 1.50, 0.0, 0.4, 2.5, 0.80, 4.0, 4.0, 3, 175.0, 175.0 point.4 = 4, 12.60, -5.60, -6.500, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 0, 0.0, 0.0 point.5 = 4, 12.60, 5.60, -6.500, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 1, 0.0, 0.0 point.6 = 4, -12.80, -5.60, -6.000, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 2, 0.0, 0.0 point.7 = 4, -12.80, 5.60, -6.000, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 3, 0.0, 0.0 point.8 = 2, 0.00, -24.00, 3.50, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.9 = 2, 0.00, 24.00, 3.50, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.10 = 2, -22.60, 0.00, 1.20, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.11 = 2, 11.00, 0.00, 0.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 point.12 = 5, -13.60, -5.60, -6.00, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.0, 1.2, 0.0, 0.0, 0.0 point.13 = 5, -13.60, 5.60, -6.00, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.1, 1.5, 0.0, 0.0, 0.0 static_pitch = 1.000 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height = 7.900 //feet, altitude of CG when at rest on the ground max_number_of_points = 13 gear_system_type=1 //Hydraulic [keyboard_response] elevator = 100, 180 aileron = 200, 1000 rudder = 200, 1000 [forcefeedback] gear_bump_nose_magnitude = 3000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2700 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2700 gear_bump_right_direction = 00500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1300 ground_bumps_angle1 = 08900 ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.20 ground_bumps_magnitude2 = 200 ground_bumps_angle2 = 09100 ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [airplane_geometry] wing_area = 249.0 wing_span = 48.0 wing_root_chord = 5.8 wing_dihedral = 2.0 wing_incidence = 1.5 wing_twist = -1.7 oswald_efficiency_factor = 0.700 wing_winglets_flag = 0 wing_sweep = 0.00 wing_pos_apex_lon = 1.50 wing_pos_apex_vert = 2.9 htail_area = 40.0 htail_span = 16.00 htail_pos_lon = -17.8 htail_pos_vert = 1.3 htail_incidence = 0.0 htail_sweep = 5.0 vtail_area = 25.0 vtail_span = 6.6 vtail_sweep = 28.0 vtail_pos_lon = -17.8 vtail_pos_vert = 2.0 elevator_area = 16.6 aileron_area = 18.3 rudder_area = 6.7 elevator_up_limit = 28.0 elevator_down_limit = 21.0 aileron_up_limit = 20.0 aileron_down_limit = 15.0 rudder_limit = 24.0 elevator_trim_limit = 19.5 spoiler_limit = 20.0 aileron_to_spoileron_gain = 1 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 1 auto_spoiler_available=0 spoiler_extension_time=0.200000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-1.500000 negative_g_limit_flaps_down=-1.500000 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 electric_always_available = 0 flap_motor = 0, 5, 12 gear_motor = 0, 5, 12 autopilot = 0, 5, 12 avionics_bus = 0, 5, 12 avionics = 1, 5, 12 pitot_heat = 0, 2, 12 additional_system = 0, 2, 12 marker_beacon = 1, 2, 12 gear_warning = 0, 2, 12 fuel_pump = 0, 5, 12 starter1 = 0, 20, 12 light_nav = 0, 5, 12 light_beacon = 0, 5, 12 light_landing = 0, 5, 12 light_taxi = 0, 5, 12 light_strobe = 0, 5, 12 light_panel = 0, 5, 12 [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.6 // 0.0 .. 1.0 extending-time = 5 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 15 // degrees flaps-position.2 = 35 // degrees flaps-position.3 = 50 // degrees flaps-position.4 = 58 // degrees damaging-speed = 200 // KIAS blowout-speed = 250 // KIAS lift_scalar = 1.00 drag_scalar = 1.12 pitch_scalar= -0.5 system_type = 1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [flaps.1] type = 1 // 1 - tail, 2 - lead span-outboard = 0.4 // 0.0 .. 1.0 extending-time = 5 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 0 // degrees flaps-position.2 = 15 // degrees flaps-position.3 = 15 // degrees flaps-position.4 = 30 // degrees damaging-speed = 200 // KIAS blowout-speed = 250 // KIAS lift_scalar = 1.00 drag_scalar = 1.12 pitch_scalar= -0.10 system_type = 1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [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 [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=8.5 //Propeller Diameter, (feet) propeller_blades=3 //Number of propeller blades propeller_moi=19 //Propeller moment of inertia beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=15.6 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=25520 //Miminum governed RPM prop_tc=0.004 //Prop time-constant gear_reduction_ratio=17.4 //Propeller gear reduction ratio fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=700 //Minimum RPM for prop feathering beta_feather=88.0 //Feathering pitch angle (degrees) power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain=0.011 //Gain on fuel flow inlet_area=1.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=33000 //RPM, second stage compressor rated value static_thrust=140 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar=1.0 //Scalar on Turboprop power maximum_torque=1865 //Maximum torque available (ft-lbs) [gear_warning_system] gear_warning_available = 2 //Amphib pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 20.1 //Flap angle that activates warning at idle flap_limit_power = 13.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.68 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,0,0,0 //pump on Eng1 [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 [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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=1,0 [airspeed_indicators] airspeed_indicator.0 = 1.16, -22.0 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [Reference Speeds] flaps_up_stall_speed=65.0 //Knots True (KTAS) full_flaps_stall_speed=51.0 //Knots True (KTAS) cruise_speed=141.0 //Knots True (KTAS) max_mach=0.35 max_indicated_speed = 160 //Red line (KIAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1200.0 autothrottle_available=0 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 0.0 use_no_default_bank=1 use_no_default_pitch=1 default_pitch_mode=0 default_bank_mode=0 [stall_warning] type=2 stick_shaker=0 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=0.150000 [deice_system] structural_deice_type=0