[fltsim.0] title=Northrop/McDonnell Douglas YF-23A "Black Widow" II PAV-1 87800 sim=PAV-1 model=800 panel= sound= texture=800 panel_alias= sound_alias= kb_checklists=YF-23A_Check kb_reference=YF-23A_Ref atc_id=PAV1 atc_airline=Air Force atc_flight_number=87800 ui_manufacturer=Northrop/McDonnell Douglas ui_type=YF-23A "Black Widow" II ui_variation=PAV-1 87800 atc_parking_types=MIL_COMBAT atc_parking_codes=F23 description=Northrop/McDonnel Douglas competitor aircraft for the Advanced Tactical Fighter Program to replace the F-15C Eagle with a new technology air superiority fighter. Two prototypes were built. The roll-out was on 22nd June 1990. This is the YF-23A "Black Widow" II Prototype Air Vehicle (PAV) 1, serial number 87800 equipped whit two Pratt & Whitney YF-119-PW-100 engines. Its first flight was on 27th August 1990 on Edwards Air Force Base and its last flight was on 18th December 1990. The flight program lasted 65 hours divided in 50 flights. On 23 April 1991, the US Department of Defense announced that the Lockheed/Boeing/General Dynamics team had won the ATF competition whit the YF-22A "Lighting" II. The PAV-1, known as "Grey Ghost", is now stored at Edwards AFB. atc_heavy=0 editable=0 [fltsim.1] title=Northrop/McDonnell Douglas YF-23A "Black Widow" II PAV-2 87801 sim=PAV-2 model=801 panel= sound= texture=801 panel_alias= sound_alias= kb_checklists=YF-23A_Check kb_reference=YF-23A_Ref atc_id=PAV2 atc_airline=Air Force atc_flight_number=87801 ui_manufacturer=Northrop/McDonnell Douglas ui_type=YF-23A "Black Widow" II ui_variation=PAV-2 87801 atc_parking_types=MIL_COMBAT atc_parking_codes=F23 description=Northrop/McDonnel Douglas competitor aircraft for the Advanced Tactical Fighter Program to replace the F-15C Eagle with a new technology air superiority fighter. Two prototypes were built. The roll-out was on 22nd June 1990. This is the YF-23A "Black Widow" II Prototype Air Vehicle (PAV) 2, serial number 87801 equipped whit two General Electric YF-120-GE-100 engines. Its first flight was on 26th October 1990 on Edwards Air Force Base and its last flight was on 18th December 1990. The flight program lasted 65 hours divided in 50 flights. On 23 April 1991, the US Department of Defense announced that the Lockheed/Boeing/General Dynamics team had won the ATF competition whit the YF-22A "Lighting" II. The PAV-2, known as "Spider", is now stored at The Western Museum Of Flight. atc_heavy=0 editable=0 [forcefeedback] gear_bump_nose_magnitude=3000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=2700 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=2700 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=1300 ground_bumps_angle1=08900 ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ground_bumps_angle2=09100 ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [General] atc_type= atc_model= editable=0 performance=Specifications\nPrime Contractor: Northrop Corp.\nSubcontractor: McDonnell Douglas Corp.\nType: YF-23A "Black Widow" II\nYear: 1990\nCrew: 1\nNumber Built: 2 (PAV-1 (87-800), PAV-2 (87-801))\nEngines: 2 YF-119-PW-100 (PAV-1) or 2 YF-120-GE-100 (PAV-2)\nMaximum Speed: 1.6M (No AB), 2.0M (AB)\nCruise Speed: 1.45M at 36000Ft\nService Ceiling: 65000Ft\nTake Off Lenght: 3500Ft\nMaximum G-Loads: +9/-4 Clean at High Altitude\nCombat Radius: 750Nm\nEmpty Weight: 29000Lb\nNormal Weight: 54000Lb\nCombat Weight: 62000Lb\nFuel Load: 2400Gal\nWingspan: 43.7Ft\nLenght: 67.5Ft\nHeight: 13.11Ft\nWing Area: 900sqFT\nWeapons Load (Planned): 8+ Short/Mid Range AAM + 1 Vulcan Cannon\nRemarks: Lost ATF Program to YF-22A [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=41000.000000 empty_weight_roll_MOI=225000.000000 empty_weight_pitch_MOI=250000.000000 empty_weight_yaw_MOI=275000.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=58000.000 [fuel] LeftMain=0.000000,-4.800000,0.000000,1200.000000,0.000000 RightMain=0.000000,4.800000,0.000000,1200.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=600.000000 wing_span=40.000000 wing_root_chord=10.833333 wing_dihedral=2.142334 wing_incidence=0 wing_twist=0.351563 oswald_efficiency_factor=3.0000 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=230.000000 htail_span=22.500000 htail_pos_lon=-21.250000 htail_pos_vert=0.000000 htail_incidence=0 htail_sweep=0.000000 vtail_area=270.000000 vtail_span=18.734994 vtail_sweep=0.000000 vtail_pos_lon=-13.333333 vtail_pos_vert=8.333333 elevator_area=50.000000 aileron_area=16.080000 rudder_area=34.000000 elevator_up_limit=30 elevator_down_limit=20 aileron_up_limit=20 aileron_down_limit=20 rudder_limit=25 elevator_trim_limit=15 spoiler_limit=60 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1.000, 18.39, 0.000, -6.970, 1500.000, 0.000, 0.890, 34.100, 0.420, 2.262, 0.750, 3.000, 3.000, 0.000, 255.000, 300.000 point.1=1.000, -5.840, -6.260, -7.740, 2000.000, 1.000, 1.330, 0.000, 0.940, 1.894, 0.750, 3.100, 3.100, 2.000, 255.000, 300.000 point.2=1.000, -5.840, 6.260, -7.740, 2000.000, 2.000, 1.330, 0.000, 0.940, 1.894, 0.750, 3.000, 3.000, 3.000, 255.000, 300.000 point.3=2.000, -6.000, -21.700, 0.600, 500.000, 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, -6.000, 21.700, 0.600, 500.000, 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, -33.000, 0.000, 0.300, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6=2.000, 30.000, 0.000, -0.900, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.7=2.000, 33.000, -6.667, 0.300, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.8=2.000, 33.000, 6.667, 0.300, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.9=2.000, -19.204, -6.672, -0.884, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.10=2.000, -19.204, 6.672, -0.884, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.11=2.000, 2.031, -7.240, -1.826, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.12=2.000, 2.031, 7.240, -1.826, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.13=2.000, 21.045, 0.000, 4.455, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.14=2.000, -26.168, -16.434, 7.464, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.15=2.000, -26.168, 16.434, 7.464, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0.000000 static_cg_height=6.853791 gear_system_type=0 [exits] number_of_exits = 2 exit_rate.0 = 0.5 exit_rate.1 = 0.4 [SMOKESYSTEM] smoke.0=0.0, -24.3, 3.80, fx_YF-23ABurner smoke.1=0.0, -24.3, -3.80, fx_YF-23ABurner smoke.2=0.0, -24.3, 3.80, fx_YF-23AFlame smoke.3=0.0, -24.3, -3.80, fx_YF-23AFlame [Flaps.0] type=2 span-outboard=0.500 extending-time=2.500 system_type=0 damaging-speed=300.000 blowout-speed=400.000 lift_scalar=0.500 drag_scalar=1.000 pitch_scalar=0.000 flaps-position.0=0.000, 0.000 flaps-position.1=5.000, 0.000 flaps-position.2=15.000, 0.000 flaps-position.3=30.000, 0.000 [Flaps.1] type=1 span-outboard=0.300 extending-time=2.500 system_type=0 damaging-speed=300.000 blowout-speed=400.000 lift_scalar=0.500 drag_scalar=1.000 pitch_scalar=0.000 flaps-position.0=0.000, 0.000 flaps-position.1=5.000, 0.000 flaps-position.2=15.000, 0.000 flaps-position.3=30.000, 0.000 [Flaps.2] type=1 span-outboard=0.200 extending-time=2.500 system_type=0 damaging-speed=300.000 blowout-speed=400.000 lift_scalar=0.500 drag_scalar=1.000 pitch_scalar=0.000 flaps-position.0=0.000, 0.000 flaps-position.1=5.000, 0.000 flaps-position.2=5.000, 0.000 flaps-position.3=10.000, 0.000 flaps-position.4=20.000, 0.000 [flight_tuning] cruise_lift_scalar = 1.00 parasite_drag_scalar = 1.10 induced_drag_scalar = 1.10 elevator_effectiveness = 1.00 aileron_effectiveness = 1.00 rudder_effectiveness = 1.00 pitch_stability = 1.10 roll_stability = 1.00 yaw_stability = 1.10 elevator_trim_effectiveness = 1.30 aileron_trim_effectiveness = 1.00 rudder_trim_effectiveness = 1.00 [GeneralEngineData] engine_type=1 Engine.0=-20.333333,-3.8,1.6 Engine.1=-20.333333,3.8,1.6 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [TurbineEngineData] fuel_flow_gain=0.002500 inlet_area=17.5000 rated_N2_rpm=29920.000000 static_thrust=25000.000000 afterburner_available=1 reverser_available=0 [jet_engine] thrust_scalar = 0.920 [Reference Speeds] flaps_up_stall_speed=150.000000 full_flaps_stall_speed=120.000000 cruise_speed=1000.00000 max_indicated_speed=1353.000000 max_mach=2.100000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=20.0,0.000000,4.11 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=2000.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 use_no_default_bank=1 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 [direction_indicators] direction_indicator.0=3,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [LIGHTS] light.0=3, 20.000, 0.00, 2.600, fx_vclighth light.1=3, 20.000, 0.00, 3.900, fx_vclighth light.2=2, -9.00, -22.00, 1.00, fx_YF-23AWingtip light.3=2, -9.00, 22.00, 1.00, fx_YF-23AWingtip light.4=9, -12.50, -13.5, 1.00, fx_YF-23AFlaptip light.5=9, -12.50, 13.5, 1.00, fx_YF-23AFlaptip light.6=6, 10.0, -4.5, 1.00, fx_YF-23AStrake light.7=6, 10.0, 4.5, 1.00, fx_YF-23AStrake light.8=3, 2.3, 0, 3.72, fx_navgrem light.9=3, -3.696, 4.64, 2.624, fx_navredm light.10=3, 16.570, 0, -1.516, fx_navwhi light.11=3, 16.570, 0, -1.516, fx_navredm [Radios] 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 light_panel=0, 5 , 17.0 [brakes] toe_brakes_scale=0.915555 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=29.220848 flap_limit_idle=5.042029 [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