//Copyright 2003 //Barry Blaisdell //Premair Aircraft Design [fltsim.0] title=PAD_DeHavilland Dash8-200 Horizon Air sim=PAD_DHC8 model= panel= sound= texture= kb_checklists=DASH8_check kb_reference=DASH8_ref atc_id=N356PH ui_manufacturer=DeHavilland ui_type=Dash8 ui_variation=Horizon Air N356PH description=FS2004/2002Pro DeHavilland DHC8-200\nTwin Turboprop Regional Airliner\nVisit the Premier Aircraft Design Web Site\nwww.flightsimnetwork.com\/premaircraft\nAll Files Copyright 2003 atc_heavy=0 atc_airline=Horizon atc_flight_number=356 editable=1 [General] performance=37 Pax Regional Airliner\nLength: 73 ft\nWing Span: 85 ft\nHt: 24 ft-7 in\nWeight:22,100 lb Empty\nMax T\/O Weight:34,500 lb\nPower: 2 x 2150SHP P&W 123C Turboprops\nMax Cruise: 288 Kts TAS\nStall Speed 72 Kts\nCeiling: 25,000 ft\nRange: 935 Naut Miles\nConcept/FD/Cfg Files/Panel: Barry Blaisdell\nRemapping: Udo Lemmob\nMaster Textures & Livery:Bob May atc_type=DEHAVILLAND atc_model=DH8B [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=Landing light.0 = 3, -30.5, -42.3, 4.7, fx_navred , light.1 = 3, -30.5, 42.3, 4.7, fx_navgre , light.2 = 2, -31.0, 42.6, 4.7, fx_strobeh , light.3 = 2, -31.0, -42.6, 4.7, fx_strobeh , light.4 = 1, -65.0, 0.00, 18.3, fx_beacon , light.5 = 3, -68.90, 0.00, 2.30, fx_navwhi , light.6 = 4, -7.91, 0.00, 2.64,fx_vclighth.fx , light.7 = 5, -28.10, -15.00, 4.30, fx_landing , light.8 = 5, -28.10, -16.00, 4.30, fx_landing , light.9 = 5, -28.10, 16.00, 4.30, fx_landing , light.10 = 5, -28.10, 15.00, 4.30, fx_landing , light.11 = 1, -28.0, 0.00, -4.00, fx_beacon , light.12 = 2, -68.90, 0.00, 2.30, fx_strobeh , damage=0 prop_anim_ratio=1.70 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1000.0 autothrottle_available= 0 pitch_takeoff_ga=8.0 use_no_default_bank=1 use_no_default_pitch=1 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 [WEIGHT_AND_BALANCE] max_gross_weight = 34500 // (pounds) empty_weight = 22700 // (pounds) reference_datum_position= 31.0, 0, 0 // (feet) distance from FlightSim Ref position: (1/4 chord,c/l, waterline) empty_weight_CG_position= -26.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "170, -9.8, -1.75, 0.0, Pilot" //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "170, -9.8, 1.75, 0.0, Front Passenger" //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "5000, -27.0, 0.0, 0.0, Payload" //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 111701 empty_weight_roll_MOI = 61201 empty_weight_yaw_MOI = 161691 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=0.8 aileron_effectiveness=1.1 rudder_effectiveness=0.8 pitch_stability=2.0 roll_stability=2.0 yaw_stability=2.0 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -28.4, -13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -28.4, 13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 0.70 //Scalar for fuel flow efficiency min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser [propeller] thrust_scalar = 1.25 //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) [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 = 200 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar = 1.2 //Scalar on Turboprop power maximum_torque = 7878 //Maximum torque available (ft-lbs) [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, 5 , 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 2 , 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 //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, -5.0, 0.00, -7.10, 1500, 0, 1.617, 25.0, 0.500, 2.5, 0.9, 5.0, 6.0, 0, 0.0 , 0.0 point.1 = 1, -29.0, -12.99, -7.30, 3000, 1, 0.633, 0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 0, 0.0 , 0.0 point.2 = 1, -29.0, 12.99, -7.30, 3000, 2, 0.633, 0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 0, 0.0 , 0.0 point.3 = 2, -31.6, -42.50, 5.39, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5 point.4 = 2, -31.6, 42.50, 5.39, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6 point.5 = 2, -68.6, 0.00, 1.22, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9 point.6 = 2, 0.0, 0.00, -3.92, 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 = 7.200 //feet, altitude of CG when at rest on the ground gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 15.0 //Flap angle that activates warning at idle flap_limit_power = 30.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1.06 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint= -8.8, -1.45, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 8 // seconds flaps-position.0 = 0 // degrees, KIAS flaps-position.1 = 5 // degrees, KIAS flaps-position.2 = 15 // degrees, KIAS flaps-position.3 = 30 // degrees, KIAS damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [fuel] LeftMain = -31.1, -9.1, 3.9, 420.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -31.1, 9.1, 3.9, 420.0, 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=1 [airplane_geometry] wing_area = 585.0 //Square feet wing_span = 85.0 //Feet wing_root_chord = 7.0 //Feet wing_dihedral = 2.5 //Degrees wing_incidence = 0.50 //Degrees wing_twist = -3.0 //Degrees oswald_efficiency_factor= 0.7 //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 = -1.50 //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 = 265.0 //Knots True (KTAS) max_mach = 0.58 max_indicated_speed = 240 //Red line (KIAS) [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 [stall_warning] type=1 [direction_indicators] direction_indicator.0=3,0 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [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