[fltsim.0] title=Fokker F50 THY sim=fok50thy model= panel= sound= texture= kb_checklists= kb_reference= atc_id=TCFOK atc_airline=TACA atc_flight_number=151 ui_manufacturer=Fokker ui_type=F-50 ui_variation=Fokker 50 THY description=Fokker 50 THY suitable as AI aircraft together with THY short range Traffic Routes \nThe aircraft is made in GMax and has a minimum of moving parts to keep framerates up when using it as AI-plane. \nOriginal model by FSRepainter \nRepaint THY colours by Sunuver. [General] atc_type=Fokker atc_model=F27 performance=Powerplants\n Two 1864kW (2500shp) Pratt & Whitney Canada PW125B turboprops driving six blade Dowty propellers. \n\n Performance \n Max cruising speed 287kt, economical cruising speed 245kt. Max operating altitude 25,000ft. Range with 50 passengers and reserves 1110nm, or 1524nm for optional high gross weight version. \n\n Weights\n Operating empty 12,520kg (27,602lb), max takeoff 19,950kg (43,980lb), or optionally 20,820kg (45,900lb).\n\n Dimensions \n Wing span 29.00m (95ft 2in), length 25.25m (82ft 10in), height 8.32m (27ft 4in). Wing area 70.0m2 (753.5sq ft).\n\n Capacity \n Flightcrew of two. Standard seating for 50 at four abreast and 81cm (32in) pitch. Max high density seating for 58. Available with convertible passenger/freight configurations. (airliners.net) [WEIGHT_AND_BALANCE] max_gross_weight=34500 // (pounds) empty_weight=22730 // (pounds) reference_datum_position=31.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, 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 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, -9.8, 1.75, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=5660, -27.0, 0.0, 0.0 //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=1.0 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 [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=1.0 //Scalar for fuel flow efficiency [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) [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=1.0 //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, 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 //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, -6.95, 1500, 0, 1.617, 25.0, 0.500, 2.5, 0.9, 5.0, 6.0, 0 point.1=1, -29.0, -12.99, -7.35, 3000, 1, 0.633, 0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 2 point.2=1, -29.0, 12.99, -7.35, 3000, 2, 0.633, 0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 3 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=-0.5 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=6.84 //feet, altitude of CG when at rest on the ground [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=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 [SMOKESYSTEM] smoke.0=0.00, -0.70, 1.40, fx_smoke_w [fuel] LeftMain=-31.1, -9.1, 3.9, 417.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-31.1, 9.1, 3.9, 417.5, 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 [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=1.0 //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=1.0 //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=265.0 //Knots True (KTAS) full_flaps_stall_speed=73.600000 [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] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 [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=1, -39.2, 0.00, -3.9, fx_beacon , light.1=3, -72.23, 0.05, 2.0, fx_navwhi , light.2=3, -72.23,-0.05, 2.0, fx_navwhi , light.3=3, -24.5, -46.8, 6.5, fx_navred , light.4=3, -24.5, 46.8, 6.5, fx_navgre , light.5=3, -24.5, -46.8, 6.5, fx_navred , light.6=3, -24.5, 46.8, 6.5, fx_navgre , light.7=2, -24.9, 47.1, 6.6, fx_strobe , light.8=2, -24.9, -47.1, 6.6, fx_strobe , light.9=1, -39.2, 0.00, -3.8, fx_beacon , [direction_indicators] direction_indicator.0=3,0
