[fltsim.0] title=NAMC YS-11 FC sim=YS11 model= panel= sound= texture= kb_checklists= kb_reference=YS11_ref atc_id= atc_id_color= atc_airline=Air Force atc_flight_number=160 ui_manufacturer=NAMC ui_type=YS-11 ui_variation= JASDF FLIGHT CHECKER 160 visual_damage=1 description=First flown in 1962, the YS-11 is the only Japanese designed airliner to enter production since WW2. A product of the Nihon Aircraft Manufacturing Company (NAMC), it has achieved a degree of success in both the Japanese domestic market and in North America. Initial production was of the YS-11100 while the follow up YS-11A200 was designed for export markets and featured an increased max take off weight. The YS-11A300 was combi version of the 200 series while the YS-11A400 was designed as a pure freighter. the YS-11A500/600 and 700 were the equivalent to the 200/300 and 400 but with a 500kg greater max takeoff weight. The last YS-11 was rolled of the assembly line in 1974 and by 1998, 66 YS-11s remained in service. The largest operators were All Nippon with 6 and Japan Air Commuter with 12. In total 182 Ys-11s were produced including two prototypes. atc_heavy=0 [General] atc_type=NAMC atc_model=YS11 editable=0 performance=Economical cruising speed is 244 KTAS at 20'000 feet. Range with maximum payload 677 miles. Maximum takeoff weight 54013 lbs. Please see "Flying YS-11.txt" for more information. [WEIGHT_AND_BALANCE] max_gross_weight=55111.000 empty_weight=33000.000 reference_datum_position=36.489, 0.000, 0.000 empty_weight_CG_position=-36.750, 0.000, 4.000 max_number_of_stations=50 station_load.0=8500.000, -36.750, 0.000, 4.000 //;Moments of Inertia //empty_weight_pitch_MOI=268022.000 //empty_weight_roll_MOI=227153.000 //empty_weight_yaw_MOI=579108.000 //empty_weight_coupled_MOI=1800.000 //CG_forward_limit=0.000 //CG_aft_limit=1.000 ;Moments of Inertia empty_weight_pitch_MOI=368022.000 empty_weight_roll_MOI=427153.000 empty_weight_yaw_MOI=679108.000 empty_weight_coupled_MOI=1800.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [flight_tuning] cruise_lift_scalar=1.10 parasite_drag_scalar=0.1000 induced_drag_scalar=1.1800 elevator_effectiveness=1.200 aileron_effectiveness=1.000 rudder_effectiveness=1.100 pitch_stability=1.250 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=0.896 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type=5 Engine.0=-25.700, -14.000, 2.500 Engine.1=-25.700, 14.000, 2.500 fuel_flow_scalar=0.385696 [propeller] thrust_scalar=0.475 propeller_type=0 propeller_diameter=14.740 propeller_blades=4 propeller_moi=112.000 beta_max=90 beta_min=14 min_gov_rpm=5000.000 prop_tc=0.0008 rotation=-1,-1 gear_reduction_ratio=12.900 fixed_pitch_beta=1.500 low_speed_theory_limit=80.000 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=10.000 beta_feather=84.000 power_absorbed_cf=1.00 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=0.000 minimum_reverse_beta=22.00 [TurbineEngineData] fuel_flow_gain=0.0035 inlet_area=14.000 rated_N2_rpm=16500.000 static_thrust=637.000 afterburner_available=0 [turboprop_engine] power_scalar=1.100 maximum_torque=10840.0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.0000 idle_rpm_friction_scalar=1.0000 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) max_battery_voltage=36.0 generator_alternator_voltage=42.0 max_generator_alternator_amps=250.0 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, 5, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 5, 17.0 starter2=0, 5, 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 auto_feather=0, 5 , 17.0 standby_vacuum=0, 2 , 5.0 hydraulic_pump=0, 2 , 17.0 fuel_transfer_pump=0, 5 , 17.0 propeller_deice=0, 1 , 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=1.0, -13.579, 0.0, -6.2, 800.0, 0.000, 0.850, 75.000, 0.600, 1.100, 0.900, 3.000, 6.000, 0.000, 200.0, 220.0 point.1=1.0, -42.479, -14.0, -6.2, 1500.0, 1.0, 1.400, 0.000, 0.500, 1.100, 0.800, 3.000, 3.200, 2.000, 200.000, 220.2 point.2=1.0, -42.479, 14.0, -6.2, 1500.0, 2.0, 1.400, 0.000, 0.500, 1.100, 0.800, 3.000, 3.300, 3.000, 200.0, 220.000 point.3=2.000, -36.400, -52.500, 3.000, 1200.0, 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, -36.400, 52.500, 3.000, 1200.0, 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, -72.690, 0.000, 0.000, 1200.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.6=2.000, -1.990, 0.000, -2.000, 1200.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 max_number_of_points=21 static_pitch=0.000 static_cg_height=6.300 [Views] eyepoint=-8.0, -1.82, 5.4 //(feet) longitudinal, lateral, vertical distance from reference datum [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -38.489, 52.30, 4.50, fx_navgrem , light.1=3, -38.489, -52.30, 4.50, fx_navredm , light.2=4, -10.589, 0.00, 4.50, fx_vclighth , light.3=1, -38.389, 0.00, 8.60, fx_beaconh , light.4=1, -60.289, 0.00, -1.6, fx_beaconb , light.5=3, -84.989, 0.00, 5.72, fx_navwhih , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_YS11, 1 [SMOKESYSTEM] smoke.0=2.70,-35.4,-15.3, fx_smoke_ys11 smoke.1=2.70,-35.4,15.3, fx_smoke_ys11 [fuel] Center1=-35.750, 0.000, 0.000, 228.000, 3.000 Center2=-35.750, 0.000, 0.000, 357.000, 3.000 LeftMain=-35.750, -9.600, 0.000, 662.500, 3.000 RightMain=-35.750, 9.600, 0.000, 662.500, 3.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area=1020.420 wing_span=105.000 wing_root_chord=13.800 wing_dihedral=6.320 wing_incidence=3.000 wing_twist=-3.000 oswald_efficiency_factor=0.820 wing_winglets_flag=0 wing_sweep=3.000 wing_pos_apex_lon=-32.000 wing_pos_apex_vert=0.000 htail_area=238.000 htail_span=39.880 htail_pos_lon=-74.250 htail_pos_vert=7.040 htail_incidence=0.000 htail_sweep=15.640 vtail_area=156.076 vtail_span=18.800 vtail_sweep=38.000 vtail_pos_lon=68.500 vtail_pos_vert=8.960 elevator_area=57.400 aileron_area=31.900 rudder_area=51.100 elevator_up_limit=27.000 // 20 elevator_down_limit=13.000 // 20 aileron_up_limit=24.000 // 25 aileron_down_limit=15.000 // 25 rudder_limit=22.000 elevator_trim_limit=15.000 spoiler_limit=95.000 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 [Reference Speeds] flaps_up_stall_speed=100.000 full_flaps_stall_speed=85.000 cruise_speed=240.000 [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=500.0 autothrottle_available=0 autothrottle_arming_required=1 autothrottle_max_rpm=90 autothrottle_takeoff_ga=0 pitch_takeoff_ga=8; [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 [exits] number_of_exits=2 exit_rate.0=0.15 ;Percent per second exit_rate.1=0.15 ;Percent per second [forcefeedback] 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=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 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 [direction_indicators] direction_indicator.0=3,0 [Flaps.0] type=1 span-outboard=0.280 extending-time=27.000 system_type=1 damaging-speed=200.000 blowout-speed=220.000 lift_scalar=1.10 drag_scalar=0.530 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=10.000, 200.000 flaps-position.2=15.000, 180.000 flaps-position.3=20.000, 165.000 flaps-position.4=25.000, 150.000 flaps-position.5=35.000, 136.000 [Flaps.1] type=1 span-outboard=0.280 extending-time=27.000 system_type=1 damaging-speed=200.000 blowout-speed=220.000 lift_scalar=1.10 drag_scalar=0.530 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=10.000, 200.000 flaps-position.2=15.000, 180.000 flaps-position.3=20.000, 165.000 flaps-position.4=25.000, 150.000 flaps-position.5=35.000, 136.000
