// VIKING MKIII TURBO BEAVER AMPHIBIAN ver0.8 // FSX update by Chief // COPYRIGHT 2007 Premier Aircraft Design // [fltsim.0] title=TurboBeaver_Mk3 Viking GDTB sim=TurboBeaver_Mk3 model= panel=GDTB sound= texture=GDTB kb_checklists=DHC2_Mk3A_Check kb_reference=DHC2_Mk3A_Ref atc_id=C-GDTB atc_parking_types=RAMP ui_manufacturer=de Havilland ui_type=BEAVER ui_variation=Viking Air Ltd C-GDTB ui_typerole="Single Engine TurboProp" ui_createdby="Premier Aircraft Design" description=Viking Air Limited, located at CYYJ, Victoria International Airport, British Columbia, Canada, is a first tier original equipment manufacturer (OEM) specializing in de Havilland aircraft products. In 2006 Viking proudly accepted the transfer of the type certificates for seven legacy\nde Havilland aircraft.\nvisit Premier Aircraft Design at: www.premaircraft.com visual_damage=0 editable=1 [General] Performance=Engine - P & W Canada PT6A-34 Turbine 680 SHP\nWingspan - 48 ft.\nLength - 35 ft 3 in\nWing area - 250 sq ft\nWeight Empty - 2790 lb.\nMTOW - 6000 lb.\nNormal Cruise Max - 141 kts IAS\nNever Exceed - 160 mph IAS\nRate of Climb - 1200 ft/min\nService Ceiling- 23,000 ft\nFuel Capacity - 186 US gal.\nRange - 550 nm. atc_type=DeHavilland atc_model=DHC2 Category=airplane [CameraDefinition.0] Title = "Right Float" Guid = {B0CA7E72-F3D9-F748-8BF5-108D197B2469} Description = "View from the aft end of the right float looking forward" Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = .5 ShowWeather = Yes InitialXyz = 1.5, .5, -3.9 InitialPbh = 0, 0, 0 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.1] Title = "Right Wing" Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59} Description = View from the right wing looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.0 ShowWeather = Yes InitialXyz = 14.5, 0.6, 0.0 InitialPbh = 8, 0, 270 XyzAdjust = TRUE Category=Aircraft ClipMode=Minimum [CameraDefinition.2] Title = "Left Wing" Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED} Description = View from the left wing looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.0 ShowWeather = Yes InitialXyz = -14.5, 0.6, 0.0 InitialPbh = 8, 0, 90 XyzAdjust = TRUE Category=Aircraft ClipMode=Minimum [CameraDefinition.3] Title = "Side Door" Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051} Description = View of the landing gear and left wing inboard flaps Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = .52 ShowWeather = Yes InitialXyz = -2.0, 0.1, -2.5 InitialPbh = 4, 0, 7 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.001] Title = "Right Seat" Guid = {195EAB58-9E4A-1E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = Yes SnapPbhAdjust = Swivel SnapPbhReturn = False PanPbhAdjust = Swivel PanPbhReturn = False Track = None ShowAxis = YES AllowZoom = TRUE InitialZoom = 0.40 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.65, 0.05, 0.0 InitialPbh=8, 0, 0 [CameraDefinition.002] Title = "Radio Stack" Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.1 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.66, 0.1, 0.05 InitialPbh=33, 0, 0 [CameraDefinition.003] Title = "Engine Controls" Guid = {195EAB58-9E4A-3E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.50 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.15, 0.05, 0.05 InitialPbh=31, 0.0, 0.0 [Views] eyepoint=3.30, -1.00, 2.27 //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 [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, -6.00, 0.00, 3.65, fx_PADbeaconh , light.6 = 4, 4.00, 0.00, 1.50, fx_vclightwhite , light.7 = 4, 4.00, 0.00, 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, 80, 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, -7.83, 1600, 0, 1.40, 45.0, 0.15, 2.5, 0.80, 4.0, 4.0, 0, 175.0, 175.0 point.1 = 1, 13.40, 5.60, -7.83, 1600, 0, 1.40, 45.0, 0.15, 2.5, 0.80, 4.0, 4.0, 1, 175.0, 175.0 point.2 = 1, -2.20, -5.60, -7.985, 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, -7.985, 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 = 0.5 oswald_efficiency_factor = 0.750 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 = 0.01 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 = 26 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 = 10 // 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 = 1.15 drag_scalar = 1.35 pitch_scalar= 0.01 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 = 10 // 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 = 1.15 drag_scalar = 1.35 pitch_scalar= 0.01 system_type = 1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.1 induced_drag_scalar=1.1 elevator_effectiveness=0.8 aileron_effectiveness=0.8 rudder_effectiveness=1.0 pitch_stability=2.0 roll_stability=1.5 yaw_stability=1.0 elevator_trim_effectiveness=1.6 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 [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=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots [GPWS] max_warning_height = 1000 sink_rate_fpm = -1500 excessive_sink_rate_fpm = -2000 climbout_sink_rate_fpm = -100 flap_and_gear_sink_rate_fpm= -100