[fltsim.0] title=DeHavilland Dash8Q-400 DETA sim=d84mst22 model= panel= sound= texture= kb_checklists=dh84_check kb_reference=dh84_ref atc_id=C2-GLA ui_manufacturer=DeHavilland ui_type=Dash8-400 ui_variation=DETA Regional description=FS2002 Dehavilland Dash8-Q400\nTwin Turboprop Regional Airliner\nAll Files Copyright 2002\nPremier Aircraft Design\nhttp:\/\/www.flightsimnetwork.com\/premaircraft\nPaint by Mario Coelho atc_heavy=0 atc_airline=DETA atc_flight_number=411 [General] performance=72\/78 Pax Regional Airliner\nLength:107.8 Ft\nWing Span: 93 Ft\nHeight: 27.5 Ft\nWeight:36,458 lbs\n63,250 lbs MTOW\nFuel: 1,772 USG\nPower:2 x PW 150A@2535 shp\n13.5 Ft Dia 6 Blade Composite Props\nMax Cruise: 350 Kts TAS\nROC 1900 fpm\nCeiling:25,000ft \/ Range:1,296 nm\nStall: 102\/90\nDate: Jan 2002\nDesign: Barry Blaisdell\nPAD atc_type=DEHAVILLAND atc_model=DH8D [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1600.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=1 autothrottle_max_rpm=150.000000 pitch_takeoff_ga=8.000000 use_no_default_bank=1 use_no_default_pitch=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -0.55, -46.00, 3.60, fx_navred , light.1=3, -0.55, 46.00, 3.60, fx_navgre , light.2=2, -0.75, 46.10, 3.60, fx_strobe , light.3=2, -0.75, -46.10, 3.60, fx_strobe , light.4=1, -52.50, 0.00, 19.45, fx_beacon , light.5=1, 24.24, 0.00, -6.10, fx_beacon , light.6=1, 14.24, 0.00, 3.50, fx_beacon , light.7=5, 1.50, -17.7, 2.75, fx_landing , light.8=5, 1.50, 17.7, 2.75, fx_landing, light.9=5, 1.50, -16.90, 2.75, fx_landing , light.10=5, 1.50, 16.90, 2.75, fx_landing, light.11=3, -61.50, 0.00, 18.40, fx_navwhi , light.12=2, -61.50, 0.00, 18.40, fx_strobeh , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=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 [Views] eyepoint=40.498835,-1.207210,0.999631 [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 , 1 [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=36450.000 empty_weight_roll_MOI=596125.000 empty_weight_pitch_MOI=348919.000 empty_weight_yaw_MOI=418449.000 empty_weight_coupled_MOI=1300.000 max_gross_weight=63250.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [fuel] LeftMain=0.000, -14.500, -1.000, 765.000, 0.000 //Long (feet), Lat (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=0.000, 14.500, -1.000, 765.000, 0.000 //Long (feet), Lat (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2.000000 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area=847.000 //Square feet wing_span=91.667 //Feet wing_root_chord=7.917 //Feet wing_dihedral=2.197 //Degrees wing_incidence=0.000 //Degrees wing_twist=-2.796 //Degrees oswald_efficiency_factor=1.635 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=0.000 //Degrees, wing leading edge wing_pos_apex_lon=0.000 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.000 //Feet, vertical distance from reference point, positive going up htail_area=201.000 //Square feet htail_span=41.667 //Feet htail_pos_lon=-45.833 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.000 //Feet, vertical distance from reference point, positive going up htail_incidence=0.500 //Degrees htail_sweep=0.000 //Degrees vtail_area=310.000 //Square feet vtail_span=20.075 //Feet, tip to body vtail_sweep=0.000 //Degrees, vertical tail leading edge vtail_pos_lon=-34.167 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=5.833 //Feet, vertical distance from reference point, positive going up elevator_area=40.000 //Square feet aileron_area=29.880 //Square feet rudder_area=27.200 //Square feet elevator_up_limit=27.502 //Degrees elevator_down_limit=20.626 //Degrees aileron_up_limit=19.481 //Degrees aileron_down_limit=14.897 //Degrees rudder_limit=23.491 //Degrees elevator_trim_limit=19.481 //Degrees spoiler_limit=59.989 //Degrees spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=0 //Aileron to spoileron gain min_ailerons_for_spoilerons=0 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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) [contact_points] point.0=1.000, 40.50, 0.000, -8.733, 1574.803, 0.000, 0.726, 46.740, 0.546, 3.500, 0.756, 5.000, 5.000, 0.000, 0.000, 0.000 point.1=1.000, -4.417, -13.750, -8.933, 1574.803, 1.000, 0.726, 0.000, 0.257, 3.000, 0.664, 8.000, 8.000, 2.000, 0.000, 0.000 point.2=1.000, -4.417, 13.750, -8.933, 1574.803, 2.000, 0.726, 0.000, 0.257, 3.000, 0.664, 8.000, 8.000, 3.000, 0.000, 0.000 point.3=2.000, -1.583, -40.917, 3.167, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4=2.000, -1.583, 40.917, 3.167, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5=2.000, -21.500, 0.000, -6.083, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6=2.000, 29.167, 0.000, -6.083, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=-0.500 static_cg_height=7.918 [GeneralEngineData] engine_type=5 Engine.0=9.583333,-16.500000,0.416667 Engine.1=9.583333,16.500000,0.416667 fuel_flow_scalar=0.34000 [TurbineEngineData] fuel_flow_gain=0.000100 inlet_area=3.000000 rated_N2_rpm=29920.000000 static_thrust=2950.000000 [turboprop_engine] power_scalar=1.74 maximum_torque=5000.000 [propeller] propeller_type=0 propeller_diameter=13.750000 propeller_blades=4 propeller_moi=120.000000 beta_max=45.000000 beta_min=12.000000 min_gov_rpm=25520.000000 prop_tc=0.004000 gear_reduction_ratio=17.600000 fixed_pitch_beta=0.000000 low_speed_theory_limit=80.000000 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=700.000000 beta_feather=79.300000 power_absorbed_cf=0.900000 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=1.00000 minimum_reverse_beta=-14.000000 [Reference Speeds] flaps_up_stall_speed=112.000000 //Knots True (KTAS) full_flaps_stall_speed=90.000000 //Knots True (KTAS) cruise_speed=350.000 //Knots True (KTAS) [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [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 [Flaps.0] type=1 span-outboard=0.500 extending-time=8.000 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=6.998, 0.000 flaps-position.2=11.996, 0.000 flaps-position.3=16.994, 0.000 flaps-position.4=36.992, 0.000
