[FLTSIM.0] title = YS11A AI ; sim = YS11A AI ; model = ; panel = ; sound = ; texture = Piedmont_old ; kb_checklists = ; prop_anim_ratio = -1.76 ; description = YS11A for AI traffic.\nFSDS2 model by Dee Waldron. ; ui_manufacturer = Nippon ; ui_type = YS11A ; ui_variation = Basic ATC model ; cruise_speed = 315.0 ; ui_typerole = "Aircraft" ; isAirTraffic = 1 isUserSelectable = 0 icao_airline = "PDT" [GENERAL] atc_type = NAMC ; atc_model = YS11 ; editable = 1 ; performance = \n\n ; [WEIGHT_AND_BALANCE] max_gross_weight = 15000 ; (pounds) empty_weight = 9090 ; (pounds) reference_datum_position = 0.0000, 0.0000, 0.0000 ; (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_cg_position = 0.0, 0, 0 ; (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 ; station_load.0 = 170, 5.0, -2.0, 0.0 ; Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 170, 5.0, 2.0, 0.0 ; Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = 170, -2.1, -2.0, 0.0 ; Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = 170, -2.1, 2.0, 0.0 ; Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = 170, -5.3, -2.0, 0.0 ; Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = 170, -5.3, 2.0, 0.0 ; Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ; Moments of Inertia empty_weight_pitch_moi = 30000 ; empty_weight_roll_moi = 18200 ; empty_weight_yaw_moi = 36500 ; empty_weight_coupled_moi = 0.0 ; [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 = -8.3, -4.8, 0.5 ; (feet) longitudinal, lateral, vertical distance from reference datum engine.1 = -8.3, 4.8, 0.5 ; (feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 1.0 ; Scalar for fuel flow efficiency master_ignition_switch = 0 ; starter_type = 0 ; thrustanglespitchheading.0 = 0,0 ; thrustanglespitchheading.1 = 0,0 ; [PROPELLER] thrust_scalar = 1.0 ; Propeller thrust scalar propeller_type = 0 ; 0=Constant Speed, 1=Fixed Pitch propeller_diameter = 8.8 ; Propeller Diameter, (feet) propeller_blades = 4 ; Number of propeller blades propeller_moi = 24 ; Propeller moment of inertia beta_max = 45 ; Maximum blade pitch angle for constant speed prop, (degrees) beta_min = 15.2 ; 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 = 17.6 ; 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 = 158 ; Lbs, max rated static thrust at Sea Level low_idle_n1 = 20 ; low_idle_n2 = 60 ; high_n1 = 100 ; high_n2 = 100 ; [TURBOPROP_ENGINE] power_scalar = 1.0 ; Scalar on Turboprop power maximum_torque = 3270 ; 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, 29.50, 0.00, -5.80, 1181, 0, 0.596, 45.0, 0.296, 2.5, 0.9516, 4.8, 4.8, 0, 0.0, 0.0 ; point.1 = 1, -0.50, -14.00, -6.00, 1574, 1, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.5, 5.2, 2, 0.0, 0.0 ; point.2 = 1, -0.50, 14.00, -6.00, 1574, 2, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.8, 4.9, 3, 0.0, 0.0 ; point.3 = 2, -3.33, -23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 ; point.4 = 2, -3.33, 23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 ; point.5 = 2, -22.67, 0.00, 0.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 ; point.6 = 2, 23.08, 0.00, -1.50, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 ; static_pitch = 0.0000 ; degrees (pitch when loaded on ground) static_cg_height = 5.900 ; feet, altitude of CG when at rest on the ground [VIEWS] eyepoint = 31.00, -1.50, 5.80 ; (feet) longitudinal, lateral, vertical distance from reference datum [FLAPS.0] type = 1 ; 1 - tail, 2 - lead span-outboard = 0.5 ; 0.0 .. 1.0 extending-time = 5 ; seconds flaps-position.0 = 0 ; degrees flaps-position.1 = 20 ; degrees flaps-position.2 = 40 ; degrees damaging-speed = 250 ; KIAS blowout-speed = 300 ; KIAS [RADIOS] ; Radio Type=availiable, standby frequency, has glide slope audio.1 = 1 ; com.1 = 1, 0 ; com.2 = 1, 0 ; nav.1 = 1, 0, 1 ; nav.2 = 1, 0, 0 ; adf.1 = 1 ; transponder.1 = 1 ; marker.1 = 1 ; [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, 250 ; aileron = 150, 250 ; rudder = 150, 250 ; [DIRECTION_INDICATORS] ; 1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another ; 2 Indicator number of slaving indicator if Type=4 direction_indicator.0 = 3,0 ; [LIGHTS] ; Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit ;-light.0 = 3, -0.25, -52.50, 5.25, fx_navred , ; ;-light.1 = 3, -0.25, 52.50, 5.25, fx_navgre , ; ;-light.2 = 3, -47.55, 0.00, 6.30, fx_navwhi , ; ;-light.3 = 1, -4.60, 0.00, 8.65, fx_beacon , ; ;-light.4 = 4, 31.0, 0.00, 5.80, fx_vclight, ; lightdef.0 = Type:3#Index:0#LocalPosition:-0.25,-52.50,5.25#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_NavigationRed#Node:#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_NavigationRed ; lightdef.1 = Type:3#Index:0#LocalPosition:-0.25,52.50,5.25#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_NavigationGreen#Node:#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_NavigationGreen ; lightdef.2 = Type:3#Index:0#LocalPosition:-47.55,0.00,6.30#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_NavigationWhite#Node:#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_NavigationWhite ; lightdef.3 = Type:1#Index:0#LocalPosition:-4.60,0.00,8.65#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_BeaconTop#Node:#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_BeaconTop ; lightdef.4 = Type:4#Index:0#LocalPosition:31.0,0.00,5.80#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_CabinBounce#Node:#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_CabinBounce ; lightdef.100 = Type:6#Index:0#LocalPosition:30.5,0,-3.8#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_Taxi#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_Taxi ; lightdef.101 = Type:6#Index:0#LocalPosition:0.5,-14,-4#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_Taxi#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_Taxi ; lightdef.102 = Type:6#Index:0#LocalPosition:0.5,14,-4#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_Taxi#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_Taxi ; [EFFECTS] wake = fx_wake ; water = fx_spray ; dirt = fx_tchdrt ; concrete = fx_sparks ; touchdown = fx_tchdwn_s, 1 ; [FUEL] leftmain = 0.0, -14.5, -1.0, 190.0, 0.0 ; Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) leftaux = 0.0, -6.0, -1.5, 79.5, 0.0 ; Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) rightmain = 0.0, 14.5, -1.0, 190.0, 0.0 ; Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) rightaux = 0.0, 6.0, -1.5, 79.5, 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 = 310.0 ; Square feet wing_span = 57.2 ; Feet wing_root_chord = 5.4 ; Feet wing_dihedral = 6.0 ; Degrees wing_incidence = 1.0 ; Degrees wing_twist = -1.5 ; Degrees oswald_efficiency_factor = 0.7 ; Measure of lift effeciency of wing wing_winglets_flag = 1 ; Are winglets available? wing_sweep = 1.0 ; Degrees, wing leading edge wing_pos_apex_lon = 2.1 ; 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 = 67.0 ; Square feet htail_span = 17.2 ; Feet htail_pos_lon = -22.6 ; 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 = 0.5 ; Degrees htail_sweep = 20.0 ; Degrees, horizontal tail leading edge vtail_area = 42.0 ; Square feet vtail_span = 7.4 ; Feet, tip to body vtail_sweep = 40.0 ; Degrees, vertical tail leading edge vtail_pos_lon = -20.5 ; Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 4.1 ; Feet, vertical distance from reference point, positive going up elevator_area = 17.0 ; Square feet aileron_area = 13.5 ; Square feet rudder_area = 7.3 ; 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 = 96.0 ; Knots True (KTAS) full_flaps_stall_speed = 76.8 ; Knots True (KTAS) cruise_speed = 315.0 ; Knots True (KTAS) [AUTOPILOT] autopilot_available = 1 ; flight_director_available = 1 ; default_vertical_speed = 1800.0 ; 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 ; NAMC YS11A ; Copyright 2004, D.E. Waldron. All rights reserved.