[fltsim.0] title=Dreamwings Dash 8 -Q400 Tyrolean sim=Dash8Q400 model= panel= sound= texture=ty checklists= ui_manufacturer=Bombardier/Dreamwings ui_type=Dash 8 Q400 ui_variation=Tyrolean description=Dreamwings Dash8 Q400 atc_id= atc_heavy=0 atc_airline=Tyrolean atc_flight_number= [General] Tyrolean painted by Steve Drabek. performance=Model Designer: Tommy Hansson\nFDE: John Cillis\n\nFlightcrew:\t2 Pilots and 2-3 Cabin Crew\nPax:\t70\nMax cruising speed:\t360kts\nMax certificated ceiling:\t25,000ft\nMax range with 70 passengers and reserves:\t1362nm\n\nWing span\t28.42m (93ft 3in)\nLength\t32.84m (107ft 9in)\nHeight\t8.38m (27ft 5in)\nWing area\t63.1m2 (679.0sq ft). atc_type=Bombardier atc_model=DHC84 editable=0 [WEIGHT_AND_BALANCE] max_gross_weight=64,500 // (pounds) empty_weight=37,888 // (pounds) 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=8 //Cabin station_load.0=2400,15.000000,-3.000000,4.000000 //FWD Left station_load.1=2400,15.000000,3.000000,4.000000 //FWD Right station_load.2=2100,0.000000,-3.000000,4.000000 //Center Left station_load.3=2100,0.000000,3.000000,4.000000 //Center Right station_load.4=2100,-15.000000,-3.000000,4.000000 //Rear Left station_load.5=2100.000000,-15.000000,3.000000,4.000000 //Rear Right //Baggage Cmpt station_load.6=1110.000000,20.000000,0.000000,-2.000000 //FWD station_load.7=1110.000000,-15.000000,0.000000,-2.000000 //Rear ;Moments of Inertia empty_weight_pitch_MOI=311701 empty_weight_roll_MOI=361201 empty_weight_yaw_MOI=361691 empty_weight_coupled_MOI=0 //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, 47.7, 0.00, -6.8, 1500.00, 0.000, 1.161, 60.000, 0.075, 2.500, 0.987, 5.000, 5.000, 0.000, 0.000, 0.000 point.1=1, -2.0, -12.99, -7.3, 1574.803, 1.000, 1.161, 0.000, 0.215, 2.500, 0.642, 5.000, 5.000, 2.000, 0.000, 0.000 point.2=1, -2.0, 12.99, -7.3, 1574.803, 2.000, 1.161, 0.000, 0.215, 2.500, 0.642, 5.000, 5.000, 3.000, 0.000, 0.000 point.3=2, 5.0, -47.8, 6.3, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5 point.4=2, 5.0, 47.8, 6.3, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6 point.5=2, -33.6, 0.00, 1.22, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9 point.6=2, 40.0, 0.00, 1.22, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4 max_number_of_points=21 static_pitch=-0.4 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=7.1 //feet, altitude of CG when at rest on the ground gear_system_type=0 [Views] eyepoint=43.400, 0, 1.7 //(feet) longitudinal, lateral, vertical distance from reference datum [GeneralEngineData] engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=0, -13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=0, 13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.5 min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.011000 inlet_area=.25 rated_N2_rpm=29920.000000 static_thrust=200.000000 afterburner_available=0 [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=13.5 //Propeller Diameter, (feet) propeller_blades=6 //Number of propeller blades propeller_moi=77 //Propeller moment of inertia beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=12 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=25520 //Miminum governed RPM prop_tc=0.0025 //Prop time-constant gear_reduction_ratio=17.0 //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=1 //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=79.3 //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) rotation=1,1 [turboprop_engine] power_scalar=1.66 //Scalar on Turboprop power maximum_torque=4500 //Maximum torque available (ft-lbs) [fuel] LeftMain=0, -9.1, 3.9, 886.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=0, 9.1, 3.9, 886.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=.88 induced_drag_scalar=.88 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=3.0 roll_stability=2.0 yaw_stability=2.0 elevator_trim_effectiveness=3.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [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 , 17.0 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=10 // degrees, KIAS flaps-position.2=30 // degrees, KIAS flaps-position.3=40 // degrees, KIAS damaging-speed=250 // KIAS blowout-speed=300 // KIAS [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [airplane_geometry] wing_area=679.0 //Square feet wing_span=93.25 //Feet wing_root_chord=7.25 //Feet wing_dihedral=2.5 //Degrees wing_incidence=-2.5 //Degrees wing_twist=2.5 //Degrees oswald_efficiency_factor=.7 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=3.0 //Degrees, wing leading edge wing_pos_apex_lon=-25.0 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_area=180.0 //Square feet htail_span=26.0 //Feet htail_pos_lon=-58.9 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=1.0 //Degrees htail_sweep=8.0 //Degrees, horizontal tail leading edge vtail_area=152.0 //Square feet vtail_span=11.7 //Feet, tip to body vtail_sweep=30.0 //Degrees, vertical tail leading edge vtail_pos_lon=-54.9 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=3.4 //Feet, vertical distance from reference point, positive going up elevator_area=53.5 //Square feet aileron_area=12.1 //Square feet rudder_area=46.4 //Square feet elevator_up_limit=17.0 //Degrees elevator_down_limit=15.5 //Degrees aileron_up_limit=18.0 //Degrees aileron_down_limit=18.0 //Degrees rudder_limit=30.0 //Degrees elevator_trim_limit=15.0 //Degrees spoiler_limit=60.0 //Degrees spoiler_limit= 60.000 spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=3.000 //Aileron to spoileron gain min_ailerons_for_spoilerons=9.969 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=92.0 //Knots True (KTAS) full_flaps_stall_speed=72.0 //Knots True (KTAS) cruise_speed=350.0 //Knots True (KTAS) max_indicated_speed=265.000000 max_mach=0.60 [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=150.0, 250.0 aileron=150.0, 250.0 rudder=150.0, 250.0 [autopilot] use_no_default_pitch=1 use_no_default_bank=1 autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 default_pitch_mode=0 default_bank_mode=0 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 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 5.0, -47.8, 6.3, fx_navred , light.1=3, 5.0, 47.8, 6.3, fx_navgre , light.2=2, 5.3, 47.8, 6.3, fx_strobe , light.3=2, 5.3, -47.8, 6.3, fx_strobe , light.4 = 3, -50.069, -0.016, 19.965, fx_strobeh , light.5 = 1, 17.875, -0.007, 4.644, fx_beacon , light.6 = 2, -59.003, 0, 18.829, fx_navwhih , light.7=4, -7.91, 0.00, 2.64, fx_vclight, [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=1.062532 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [exits] number_of_exits=3 exit_rate.0=0.25 ;Percent per second exit_rate.1=0.35 ;Percent per second exit_rate.2=0.30 ;Percent per second [TailHook] tailhook_length=1 ;(feet) tailhook_position = 0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.05,0.05 ;Percent per second cable_force_adjust = 1.0
