[fltsim.0] title=FLY BE Dash 8Q400 sim=dhc84 model= panel= sound= texture=be checklists= ui_manufacturer=Bombardier ui_type=Dash 8Q400 ui_variation=FLY BE atc_airline=JERSEY atc_flight_number=201 description=Bombardier Dash 8Q400\FLY BE atc_id=G-JEDI [General] performance=Max Cruise Speed\t350kts\nMaximum Range\t1,362 nm\nService Ceiling\t27,000 ft\nMax Gross Weight\t64,500 lb\nSeating\t\tUp to 70 atc_type=Bombardier atc_model=DHC84 editable=0 [WEIGHT_AND_BALANCE] empty_weight = 37717 // (pounds) reference_datum_position = 0.000000,0.000000,0.000000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0.000000,0.000000,0.000000 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations =50 station_load.0 = 15400, 0, 0, 0.0 //Payload ;Moments of Inertia empty_weight_roll_MOI = 205716 empty_weight_pitch_MOI = 231761 empty_weight_yaw_MOI = 330944 empty_weight_coupled_MOI = 1300 max_gross_weight=64500.000000 [fuel] LeftMain=0.000000,-14.500000,0.00000,862.00000,0.000000 RightMain=0.000000,14.500000,0.00000,862.00000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=1 [contact_points] //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) point.0=1, 35.72, 0.00, -5.259, 1500, 0, 1.671, 80, 0.250, 0.572, 0.9, 7.0, 5.0, 0, 120, 250 point.1=1, -0.917, -5.604, -5.696, 1574.803, 1.000, 1.014, 0.000, 0.272, 2.500, 0.9, 5.000, 5.000, 2.000, 0.000, 0.000 point.2=1, -0.917, 5.604, -5.696, 1574.803, 2.000, 1.014, 0.000, 0.272, 2.500, 0.9, 5.000, 5.000, 3.000, 0.000, 0.000 point.3=2.000, -0.500, -42.667, 3.833, 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, -0.500, 42.667, 3.833, 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, -20.333, 0.000, 0.000, 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, 24.083, 0.000, 0.000, 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=0.000000 static_cg_height=5.506865 gear_system_type=0 [forcefeedback] gear_bump_nose_magnitude=3000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=2800 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=3100 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=1450 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [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 rocognition=0, 2 , 0 light_wing=0, 2 , 0 light_logo=0, 2 , 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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1700.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=100000.000000 use_no_default_pitch=1 use_no_default_bank=1 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 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, -3.379, -46.32, 6.716, fx_navred , light.1 = 3, -3.379, 46.32, 6.716, fx_navgre , light.2 = 2, -3.379, 46.32, 6.716, fx_strobe , light.3 = 2, -3.379, -46.32, 6.716, fx_strobe , light.4 = 1, -3.737, 0.00, 6.811, fx_beacon , // Boven light.5 = 1, 0.000, 0.00, -2.369, fx_beacon , // Onder light.6 = 1, -54.31, 0.00, 5.249, fx_strobeh , // Achter electric_pump=0 [airplane_geometry] wing_area = 1179.0 //Square feet wing_span = 93.3 //Feet wing_root_chord = 7.0 //Feet wing_dihedral = 2.5 //Degrees wing_incidence = 1.0 //Degrees wing_twist = -3.0 //Degrees oswald_efficiency_factor= 1.7 //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 = 97.0 //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 = 106.0 //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 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 [Reference Speeds] flaps_up_stall_speed = 92.0 //Knots True (KTAS) full_flaps_stall_speed = 72.0 //Knots True (KTAS) cruise_speed = 330.0 //Knots True (KTAS) max_mach = 0.62 max_indicated_speed = 300 //Red line (KIAS) [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.7 // 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 [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=2.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=2.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [GeneralEngineData] engine_type=5 Engine.0=9.500000,-8.500000,2.333333 Engine.1=9.500000,8.500000,2.333333 fuel_flow_scalar=0.9 min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.011 //Gain on fuel flow inlet_area=1.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=465 //Lbs, max rated static thrust at Sea Level [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter = 13.0 //Propeller Diameter, (feet) propeller_blades = 4 //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 = 0.004 //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) [turboprop_engine] maximum_torque=12198 //Maximum torque available (ft-lbs) [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=1.03, -1.8, 3.26 [direction_indicators] direction_indicator.0=3,0 [SmokeSystem] smoke.0=-0.5,-2.333,-4.833, fx_smoke_rx smoke.1=-0.5,-2.333,4.833, fx_smoke_rx [brakes] toe_brakes_scale=0.495224 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= 2 exit_rate.0= 0.25 ;Percent per second exit_rate.1= 0.35 ;Percent per second