[fltsim.0] title=Dreamwings Dash 8 -Q400 JAC/JAL scheme sim=Dash8Q400 model= panel= sound= texture=JAC checklists= ui_manufacturer=Bombardier/Dreamwings ui_type=Dash 8 Q400 ui_variation=Japan Air Commuter JA843C description=Dreamwings Dash8 Q400 JAL/JAC atc_id=Commuter atc_heavy=0 atc_airline= atc_flight_number= [General] 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=DH8C editable=0 [WEIGHT_AND_BALANCE] empty_weight = 37717 // (pounds) max_gross_weight=64500 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 =6 CG_forward_limit=0.25 CG_aft_limit=0.5 station_load.0 = "500, 60.0, 0.0, 0.0, Flight Crew" station_load.1 = "500, -10.0, 0.0, 0.0, Galleys" station_load.2 = "2000, -15.0, 0.0, 0.0, Baggage" station_load.3 = "2500, 40.0, 0.0, 0.0, Cargo" station_load.4 = "2500, 60.0, 0.0, 0.0, Front Pax Cabin" station_load.5 = "2500, 50.0, 0.0, 0.0, Rear Pax Cabin" empty_weight_pitch_MOI=311701 empty_weight_roll_MOI=361201 empty_weight_yaw_MOI=361691 empty_weight_coupled_MOI = 1300 max_gross_weight=64500.000000 //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 fuel_flow_scalar=0.9 min_throttle_limit=-0.250000 [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 = 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 = 00000 //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) [TurbineEngineData] fuel_flow_gain=0.025 //Gain on fuel flow inlet_area=2.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=200 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar = 1.5 //Scalar on Turboprop power maximum_torque = 7500 //Maximum torque available (ft-lbs) max_rpm_mechanical_efficiency_scalar=0.960 idle_rpm_mechanical_efficiency_scalar=0.975 [fuel] LeftMain= -10.000000,-14.500000,0.00000,862.00000,0.000000 RightMain= -10.000000,14.500000,0.00000,862.00000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=1 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=0.9 induced_drag_scalar=0.9 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 [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 = 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= 2.0 //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=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 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=800.000000 autothrottle_available=1 pitch_takeoff_ga=8.000000 use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode. autothrottle_arming_required=0 autothrottle_takeoff_ga=8 autothrottle_max_rpm=18000 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=1.000000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 5.0, -47.2, 6.2, fx_navred , light.1=3, 5.0, 47.2, 6.2, 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=0.75 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 = 0.15,0.15 ;Percent per second cable_force_adjust = 1.0
