[fltsim.0] title=F16C BLOCK30 sim=F16C Fighting Falcon model= panel= sound= texture= checklists= atc_id=385 atc_airline=Air Force atc_flight_number=85 atc_heavy=0 ui_manufacturer=Lockheed Martin ui_type=F16C ui_variation=Block30 USAF description=F16C Block30 USAF Fighter atc_id=53 [General] atc_type=LOCKHEED performance=Length: 48ft 5in Wing span: 31ft Power: 1 x 28,810 lb GE F110-GE-100 atc_model=F16 editable=1 [WEIGHT_AND_BALANCE] max_gross_weight=26536 // (pounds) empty_weight=15917 reference_datum_position=0, 0, 0 empty_weight_CG_position=-0.729, 0, 0.300 max_number_of_stations=50 station_load.0=240.0000000,15.837000,0.000000,1.404000 //pilot station_load.1=296.0000000,21.210000,0.000000,-0.098000 //radar station_load.2=841.0000000,5.5690000,0.000000,1.927000 //gun station_load.3=141.0000000,-6.270000,-1.20000,0.000000 //l_pylon station_load.4=141.0000000,6.270000,-1.20000,0.000000 //r_pylon station_load.5=250.0000000,-6.270000,-2.057000,0.000000 //l_tank station_load.6=250.0000000,6.270000,-2.057000,0.000000 //r_tank station_load.7=120.0000000,-1.30000,0.000000,-4.000000 //c_pylon station_load.8=190.0000000,-2.33700,0.090000,-15.7360000 //AIM-9M station_load.9=190.0000000,-2.33700,0.090000,15.7360000 //AIM-9M station_load.10=190.0000000,-1.307000,-1.372000,-12.909000 //AIM-9M station_load.11=190.0000000,-1.307000,-1.372000,12.909000 //AIM-9M station_load.12=100.0000000,-2.852000,-0.852000,-12.916000 //Pylon_L station_load.13=100.0000000,-2.852000,-0.852000,12.916000 //pylon_R station_load.14=461.0000000,-1.30000,0.000000,-5.000000 //alq-184 ;Moments of Inertia empty_weight_roll_MOI=120000 empty_weight_pitch_MOI=300000 empty_weight_yaw_MOI=950000 empty_weight_coupled_MOI=0.000000 [flight_tuning] cruise_lift_scalar=0.55 parasite_drag_scalar=1.8 induced_drag_scalar=1.1 elevator_effectiveness=1.2 aileron_effectiveness=2.5 rudder_effectiveness=1.8 pitch_stability=1.0 roll_stability=2.8 yaw_stability=3.5 elevator_trim_effectiveness=8.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [fuel] Center1=2.00, 0.0, 1.469, 377.99, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2=-6.11, 0.0, 1.469, 330.24, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center3=9.31, 0.0, 2.384, 142.00, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-2.69, -9.4, 0.261, 82.110, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-2.69, 9.4, 0.261, 82.110, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) External1=0.0, -6.270, -2.057, 370.0, 0.0 External2=0.0, 6.270, -2.057, 370.0, 0.0 fuel_type=2 number_of_tank_selectors=2 [airplane_geometry] wing_area=300.0 wing_span=31.0 wing_root_chord=12.376 wing_dihedral=0.0 wing_incidence=0.0 wing_twist=-0.8 oswald_efficiency_factor=0.8 wing_winglets_flag=0 wing_sweep=40.0 wing_pos_apex_lon=5.884 wing_pos_apex_vert=0.55 htail_area=63.70 htail_span=18.31 htail_pos_lon=-10.148 htail_pos_vert=-3.530 htail_incidence=0.0 htail_sweep=38.0 vtail_area=43.10 vtail_span=11.192 vtail_sweep=40.0 vtail_pos_lon=-8.821 vtail_pos_vert=4.103 elevator_area=31.85 aileron_area=47.51 rudder_area=11.65 elevator_up_limit=22.0 elevator_down_limit=20.0 aileron_up_limit=19.0 aileron_down_limit=14.0 rudder_limit=35.0 elevator_trim_limit=40.0 spoiler_limit=60.0 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_flaps_for_spoilerons=0.000000 min_ailerons_for_spoilerons=0 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //1 Longitudinal Position (feet) //2 Lateral Position (feet) main gear 4.80000 //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)1.221440 main gear 0.323441 nose //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) main gear 0.582204 nose 0.573540 //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, 11.90, 0.00, -6.57, 2952.8, 0, 18.000, 90.0, 0.10, 2.5, 0.9900, 5.0, 5.0, 0, 320.0, 305.0 point.1=1, -1.114, -6.12, -6.72, 2952.8, 1, 25.500, 0.0, 0.80, 2.5, 0.9200, 5.0, 5.0, 2, 320.0, 305.0 point.2=1, -1.114, 6.12, -6.72, 2952.8, 2, 25.500, 0.0, 0.80, 2.5, 0.9200, 5.0, 5.0, 3, 320.0, 305.0 point.3=2, -6.914, 0.00, -3.14, 1574.8, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -4.914, 0.00, -2.74, 1574.8, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -18.06, 0.00, -1.54, 1574.8, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 27.37, 0.00, -0.97, 958.8, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 point.7=2, -13.03, 0.00, 4.06, 0.8, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 point.8=2, 15.26, 0.00, 2.57, 0.8, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 point.10=2,-15.49, -4.46, 0.00, 1574.8, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.11=2,-15.49, 4.46, 0.00, 1574.8, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 max_number_of_points=12 static_pitch=1.8 static_cg_height=6.20 [Flaps.0] //Inboard Trailing Edge type=1 span-outboard=0.7 extending-time=3.0 system_type=0 flaps-position.0=0 flaps-position.1=20 damaging-speed=320 // KIAS blowout-speed=350 // KIAS lift_scalar=1.00 drag_scalar=0.02 pitch_scalar=1.35 system_type=1 //Hydraulic [flaps.1] //Leading Edge type=2 // 1 - tail, 2 - lead span-outboard=1.0 // 0.0 .. 1.0 extending-time=.8 // seconds flaps-position.0=22 // degrees flaps-position.1=15 // degrees damaging-speed=500 // KIAS blowout-speed=520 // KIAS lift_scalar=1.00 drag_scalar=0.00 pitch_scalar=3.5 system_type=1 //Hydraulic [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 [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 [GeneralEngineData] engine_type=1 Engine.0=-15.371,0.0,0.097 fuel_flow_scalar=1 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=3.88 rated_N2_rpm=29920 static_thrust=23000 afterburner_available=0 reverser_available=0 [Reference Speeds] flaps_up_stall_speed=118.000000 full_flaps_stall_speed=110.200000 cruise_speed=450 [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 [Views] eyepoint=15.6,0.0,2.7 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=1 pitch_takeoff_ga=8; [direction_indicators] direction_indicator.0=3,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=4,13.0,0.85,4.00,fx_vclighth, light.1=3,12.67,-2.16,-1.63,fx_navredm, light.2=3,12.67,2.16,-1.63,fx_navgrem, light.3=2,-17.90,0.00,11.15,fx_strobeh, light.4=3,-10.49,-3.25,0.85,fx_navwhi, light.5=3,-10.49,3.25,0.85,fx_navwhi, light.6=3,-16.36,0.00,3.05,fx_navwhi, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 contrail=fx_contrail_s
