WPC@ WyB6 3bA)NB 5.EI^nErÐDtؙ ˜A-pM̀#Ȋt:7Uq4*D`vO:!04+!(_Inn|席fOwЅPTMtHܵLU11^ìWŎҐ3k*TW3}^VEQ}gs p5F Ew<:dDi83̳yqTz%[ _9 t9: V{ U٬ĩv"gU,U> 1  U<UNN1 R3N^  m 0N F XVT  \XnT  ^*ZT 6 PFL T JF 1uF K N[JJ = \MX  b^s` N1`T f333   b^ Jy  ` \3!\!J! 5"I" B_" V"`" W# ^g#Z#Z$ y$ N$J$ !% V1%R% % J%F3& y& `&\&FE' ' T'P'F?(>(R((Z)Jo) \)J*b_*^* b+^+ X+T7,X,L,>/-bm- - P-L/.J{.{.J.^/^m/T/X0Lw0>00>1b?1?1J1^1^I2T2X2LS3P3P3R?4\4>4b+5+5J5^5^56T6X6L?7P7\7R78T88b8JO9^9^9 hU:d: Z!;d{;V;;`5< R<N<T5=T=J=T'>X{>L>`????? d?`?`C@HP LaserJet 4000 Series PCL$,,,,$0(hH  Z 6Times New Roman RegularX($ 6Times New Roman Regular 0 '  _XiXXXfXXiCommerceControlList@BBBSupplementNo.1toPart77466(#Category7"page  1  #C f+##XX CJ#(3$ !  +ON  0Times New Roman Bold F  )  _ C XXExportAdministrationRegulations #XX C.#;(# C XX f CFebruary5,2008#C f##XX C# (3$ !  ZrV8<3|x'ON  Z 6Times New Roman Regular'ON  Z 6Times New Roman Regular1i)(hH  Z 6Times New Roman Regular $Tahoma  x \  `&Times New Roman8 CSY_ekqw}Numbers 2Numbers1.1.1.1.1.1.1.1.7A101%\  `$Times NewRoman(9 Z6Times New Roman Regular7A101 Accelerometers, other than those7A101 Accelerometers, other than those{8s U(O$7E1047A994 Other navigation direction finding7A994 Other navigation direction finding7A1027A102 All types of gyros, other than those7A102 All types of gyros, other than those7A994 Other navigation direction finding7A1037A103 Instrumentation, navigation equipment7A103 Instrumentation, navigation equipment7A994 Other navigation direction finding7A1047A104 Gyro-astro compasses and other7A104 Gyro-astro compasses and other7A9947A994 Other navigation direction finding7E104 Design Technology for the3#37=CIQYag1.a.i.(1)(a)(i)1)a)7E104 Design Technology for the7E9947E994 Technology, n.e.s., for the7E994 Technology, n.e.s., for the7E994 Technology, n.e.s., for the7B0037B003 Equipment specially designed for the7B003 Equipment specially designed for the7A1067A106 Altimeters, other than those controlled7A106 Altimeters, other than those controlledb. Integrated flight instrument systems, which7A105 Receiving equipment for Globalb. Integrated flight instrument systems, which7A994 Other navigation direction finding7A005 Global navigation satellite systems (i.e.7B1017E1027E102 Technology for protection of avionics7E102 Technology for protection of avionics7E994 Technology, n.e.s., for the7E1017E101 Technology, according to the General7E101 Technology, according to the General7E101 Technology, according to the General7E994 Technology, n.e.s., for the7A003.b  | b. Hybrid Inertial Navigation 7B101 Production equipment, and otherb. Integrated flight instrument systems, which7B1027B102 Equipment, other than those controlled7B102 Equipment, other than those controlled7B102 Equipment, other than those controlled7B9947B994 Other equipment for the test,7B994 Other equipment for the test,7D1037D103 Software specially designed for7D103 Software specially designed for7D9947D994 Software, n.e.s., for the7D994 Software, n.e.s., for the7D1027D102 Integration software, as follows (See7D102 Integration software, as follows (See7D994 Software, n.e.s., for the7D1017D101 Software specially designed or7D101 Software specially designed or7D994 Software, n.e.s., for theb. Hybrid Inertial Navigation 7B101 Production equipment, and other7B102 Equipment, other than those controlled7B994 Other equipment for the test,7A117 Guidance sets capable of achieving7A105 Receiving equipment for Global7A005 Global navigation satellite systems (i.e.7A106 Altimeters, other than those controlled7A115 Passive sensors for determining bearing7A115 Passive sensors for determining bearing7A116 Flight control systems (hydraulic,7A116 Flight control systems (hydraulic,7A117 Guidance sets capable of achieving7B103 Specially designed productionb. Hybrid Inertial Navigation 7A005 Global navigation satellite systems (i.e.7B1037B103 Specially designed production7B103 Specially designed production7B994 Other equipment for the test,7A105 Receiving equipment for Global7A106 Altimeters, other than those controlled7A115 Passive sensors for determining bearing7A116 Flight control systems (hydraulic,7A117 Guidance sets capable of achieving7B103 Specially designed productionb. Hybrid Inertial Navigation b. Hybrid Inertial Navigation 7A005 Global navigation satellite systems (i.e.7A105 Receiving equipment for Global7A106 Altimeters, other than those controlled7A115 Passive sensors for determining bearing7A116 Flight control systems (hydraulic,7A117 Guidance sets capable of achieving7B103 Specially designed production7D101 Software specially designed or7D101 Software specially designed or7D103 Software specially designed for7D102 Integration software, as follows (Seeb. Hybrid Inertial Navigation 7A005 Global navigation satellite systems (i.e.7A105 Receiving equipment for Global7A106 Altimeters, other than those controlled7A115 Passive sensors for determining bearing7A116 Flight control systems (hydraulic,7A117 Guidance sets capable of achieving7B103 Specially designed production7D101 Software specially designed or7D102 Integration software, as follows (See7D103 Software specially designed for7A994 Other navigation direction finding7A003.b7A005 Global navigation satellite systems (i.e.7A105 Receiving equipment for Global7A106 Altimeters, other than those controlled7A115 Passive sensors for determining bearingb. Angular or rotational accelerometers specifiedb. Angular or rotational accelerometers specified7A008 Underwater sonar navigation systems,b. Angular or rotational accelerometers specified7A008 Underwater sonar navigation systems,b. Integrated flight instrument systems, which7A004 Gyro-astro compasses, and other7A004 Gyro-astro compasses, and other7A994 Other navigation direction finding7A994 Other navigation direction finding7B994 Other equipment for the test,7A116 Flight control systems (hydraulic,7A117 Guidance sets capable of achieving7B103 Specially designed productionb. Integrated flight instrument systems, whichb. Integrated flight instrument systems, whichb. Integrated flight instrument systems, whichb. Integrated flight instrument systems, which !  _XXXX (X(#(#( ,X    *&%XXQ*CATEGORY7NAVIGATIONAND ( AVIONICS  A.SYSTEMS,EQUIPMENTAND  \ COMPONENTS \ 4    N.B.1: Forautomaticpilotsforunderwater   vehicles,seeCategory8.Forradar,see     Category6. n  #&%%&+#&%%& 7A001Accelerometersasfollows(seeListof   ItemsControlled),andspeciallydesigned   componentstherefor.#&%%&#&%%&     LicenseRequirements  ~V   ReasonforControl:NS,MT,AT . Control(s) 4  `      CountryChart      NSappliestoentireentry   NSColumn1 f MTappliesto#&%%&#&%%&N XOӄ  XԀcommodities 0  MTColumn1> thatmeetorexceedthe 5  parametersof7A101. &      4 ATappliestoentireentry   ATColumn1O# X ӄ#N#{d X X}##&%%&^#&%%&   LicenseExceptions      _LVS_: 4 N/A "Y!   _GBS_: 4 N/A Y#1"   _CIV_: 4 N/A 1$ #  ListofItemsControlled  %%   Unit:$value 'i!' 0  RelatedControls:Seealso%  4 h O  5  7A1016, O@   7 \n % Ԁand4" O  5  7A9946 O   7 . . i(A"( Forangularorrotationalaccelerometers,see A)#) 4 O  5  7A001.b6 O   7 Z1 .MTcontrolsdonotapplyto *#* accelerometersthatarespeciallydesignedand *$+ developedasMeasurementWhileDrilling+%, (_MWD_)sensorsforusein_downhole_Ԁwell (, serviceapplications.-D(#D(# 0 D RelatedDefinitions:N/A.D(#D(#  D Items: / a.Linearaccelerometershavinganyofthe ` 81 following: 8 2  D a.1.Specifiedtofunctionatlinear  4 accelerationlevelslessthanorequalto15g,and  5 havinganyofthefollowing: p6  D  p a.1.a.  A bias stabilityofless H 8 (better)than130microgwithrespecttoafixed   9 calibrationvalueoveraperiodofoneyear;or  :  D  p a.1.b.A scalefactor stabilityofless  < (better)than130_ppm_Ԁwithrespecttoafixed X= calibrationvalueoveraperiodofoneyear; X0>  D a.2.  Specifiedtofunctionatlinear @ accelerationlevelsexceeding15g,andhavingall A ofthefollowing: B  D  p a.2.a.  A bias repeatabilityofless h@D (better)than5,000microgoveraperiodofone @E year;and F  D  p a.2.b.  A scalefactor repeatabilityof H less(better)than2,500_ppm_Ԁoveraperiodofone xI year;or xPJ  D a.3.  Designedforuseininertialnavigation (!L orguidancesystemsandspecifiedtofunctionat "M linearaccelerationlevelsexceeding100g.#&%%&*#&%%& "N %  b. D Angularorrotationalaccelerometersspecified $`P tofunctionatlinearaccelerationlevelsexceeding `%8Q 100g.#&%%&#&%%& 8& R %M#&%%&#&%%&#&%%&#&%%&   ,%Y #&%%&#&%%&1XX 17A002Gyrosorangularratesensors,having ( anyofthefollowingcharacteristics(seeListof  ItemsControlled),andspeciallydesigned  componentstherefor. #&%%&'#&%%&    LicenseRequirements  ` 8   ReasonforControl:NS,MT,AT   Control(s) 4  `      CountryChart      NSappliestoentireentry   NSColumn1 pH  MTappliesto#&%%&v#&%%& `    0  MTColumn1   #&%%&@#&%%&commoditiesthatmeet   Ѐorexceedtheparameters   Ѐof7A102.   ATappliestoentireentry   ATColumn1#&%%&#&%%&O  X{dNӄ   X0   LicenseRequirementNote: Forthepurpose ! ofMTcontrolsonly,the#&%%&#&%%&termstabilityisdefined  asameasureoftheabilityofaspecific  mechanismorperformancecoefficienttoremain  invariantwhencontinuouslyexposedtoafixed ] operatingcondition.(Thisdefinitiondoesnot ]5 refertodynamicorservostability.)(IEEESTD 5  528-2001paragraph2.247)N#  ӄ#O#{d X ##&%%&#&%%&    LicenseExceptions     _LVS_: 4 N/A m E   _GBS_: 4 N/A E!    _CIV_: 4 N/A "! #&%%&# &%%&ListofItemsControlled  ##   Unit:$value }%U% 0  RelatedControls:Seealso% # 4% h O  5  7A1026F OZ   7 \ %#9 Ԁand4& O  5  7A9946!O!   7H!. U&- & Forangularorrotationalaccelerometers,see -'!' 4 O  5  7A001.b6 "O"   7ZK".#&%%&#&%%&(!(   RelatedDefinitions:N/A (")   Items: )#* #&%%&"#&%%&a.A driftrate stability,whenmeasuredina e+=%, 1genvironmentoveraperiodofonemonth,and =,&- withrespecttoafixedcalibrationvalue,ofless (- (better)than0.5degreeperhourwhenspecifiedto . functionatlinearaccelerationlevelsuptoand / including100g;   0 b. D An anglerandomwalkofless(better)than ` 82 orequalto0.0035degreepersquareroothour;or 8 3  D Note:   7A002.bdoesnotcontrolspinning  5 massgyros(spinningmassgyrosaregyroswhich  6 useacontinuallyrotatingmasstosenseangular r7 motion). rJ 8 c. D Araterangegreaterthanorequalto500 " : degreespersecondandhavinganyofthe  ; following:  <  D c.1.  A driftrate stability,when Z> measuredina1genvironmentoveraperiodof Z2? threeminutes,andwithrespecttoafixed 2 @ calibrationvalueofless(better)than40degrees  A perhour;or B  D c.2  An anglerandomwalkofless jD (better)thanorequalto0.2degreepersquareroot jBE hour;or BF  D d.Specifiedtofunctionatlinearacceleration H levelsexceeding100g.#&%%&##&%%& I #&%%&^*#&%%&#&%%&*# D  p     &%%& 7A003 InertialSystemsandspeciallydesigned R *L componentstherefor.#&%%&(+#&%%&  .!M #&%%&+#&%%& LicenseRequirements  "O  D ReasonforControl:NS,MT,AT $fQ Control(s)         L  x CountryChart >& S  D NSappliestoentireentry L  x NSColumn1 '!U MTappliestocommodities L 0 x MTColumn1)v#Wx(#x(# thatmeetorexceedthe v*N$X parametersof7A103. N+&%Y  D  &,%Z ЇATappliestoentireentry   ATColumn1#&%%&$,#&%%& (  LicenseExceptions     _LVS_: 4 N/A  `   _GBS_: 4 N/A ` 8   _CIV_: 4 N/A 8   ListofItemsControlled      Unit:$value p  0  RelatedControls:Seealso% ' 4)bh O  5  7A10360O0  7b\1%'0Ԁand4*bO  5  7A99461O1  7b1. pH  InertialNavigationSystems(INS)andinertial H  equipment,andspeciallydesigned    componentsthereforspecificallydesigned,   modifiedorconfiguredformilitaryuseare   subjecttotheexportlicensingauthorityofthe   U.S.DepartmentofState,Directorateof X DefenseTradeControls.(See22_CFR_Ԁpart X0 121.)#&%%&.#&%%&0 0  RelatedDefinitions:#&%%&Y4#&%%&UKUS., DataBasedReferenced  Navigation( _DBRN_)systemsaresystems  whichusevarioussourcesofpreviously  measuredgeomappingdataintegratedto h provideaccuratenavigationinformationunder h@ dynamicconditions.Datasourcesinclude @ bathymetricmaps,stellarmaps,gravitymaps,  magneticmapsor3Ddigitalterrainmaps.#&%%&4#US.,UK.,5&%%&   Items:  #&%%&H7#&%%&#&%%&7#&%%&a.InertialNavigationSystems(INS)(_gimballed_ xP or_strapdown_)andinertialequipmentdesigned for P (  aircraft,landvehicles,vessels(surfaceor ,!  underwater) or spacecraft forattitude,guidance "! orcontrol,havinganyofthefollowing "" characteristics,andspeciallydesigned ## componentstherefor: $h$   a.1. 4 Navigationerror(freeinertial) @& & subsequenttonormalalignmentof0.8nautical ' ' mileperhour(_nm_/hr)CircularErrorProbable '!( (_CEP_)orless(better);or (")   a.2. 4 Specifiedtofunctionatlinear x*P$+ accelerationlevelsexceeding10g. P+(%,  (,&- % R b.HybridInertialNavigation%R=<Systemsembedded (- withGlobalNavigationSatelliteSystem(s) . (_GNSS_)orwith DataBasedReferenced / Navigation( _DBRN_)System(s)forattitude, 0 guidanceorcontrol,subsequenttonormal  `1 alignment,havinganINSnavigationposition ` 82 accuracy,afterlossof_GNSS_Ԁor _DBRN_fora 8 3 periodofupto4minutes,ofless(better)than10  4 metersCircularErrorProbable(_CEP_).  5 #&%%&8#&%%&c. D InertialEquipmentforAzimuth,Heading,or p7 NorthPointinghavinganyofthefollowing pH 8 characteristics,andspeciallydesigned H 9 componentstherefor:   :  D c.1.  DesignedtohaveanAzimuth,  < Heading,orNorthPointingaccuracyequalto,or  = less(better)than6arcminutesRMSat45degrees X> latitude;or X0?  D c.2.  Designedtohaveanon-operating A shocklevelof900gorgreateratadurationof B 1-msec,orgreater. C d. D Inertialmeasurementequipmentincluding h@E InertialMeasurementUnits(_IMU_)andInertial @F ReferenceSystems(IRS),incorporating G accelerometersorgyroscontrolledby7A001or H 7A002,andspeciallydesignedcomponents I therefor.#&%%&o?#&%%& xJ  D Note1 :Theparametersof7A003.aand P (L 7A003.bareapplicablewithanyofthefollowing *!M environmentalconditions: "N  D  p 1.Inputrandomvibrationwithanoverall #P magnitudeof7.7g_rms_Ԁinthefirsthalfhourand $bQ atotaltestdurationofoneandonehalfhourper b%:R axisineachofthethreeperpendicularaxes,when :& S therandomvibrationmeetsthefollowing: ' T  D  p   a.Aconstantpowerspectraldensity ("V (PSD)valueof0.04g2/Hzoverafrequency )r#W intervalof15to1,000Hz;and r*J$X  D  p   b.ThePSDattenuateswithfrequency ",%Z from0.04g2/Hzto0.01g2/Hzoverafrequency ( intervalfrom1,000to2,000Hz;      2.Arollandyawrateofequaltoormore  than+2.62rad/s(150deg/s);or  `     3.Accordingtonationalstandards 8  equivalentto1.or2.ofthisnote.      Note2: 7A003doesnotcontrolinertial    navigationsystemsthatarecertifiedforuseon r   civilaircraftbycivilauthoritiesofa rJ  _Wassenaar_ԀArrangementParticipatingState,see J"  SupplementNo.1toPart743foralistofthese "  countries.#&%%&C#&%%&     Note3:  ` 7A003.c.1doesnotcontrol   theodolitesystemsincorporatinginertial \ equipmentspeciallydesignedforcivilsurveying \4 purposes. 4  #&%%&J#&%%&  TechnicalNotes:       1.7A003.breferstosystemsinwhichan j INSandotherindependentnavigationaidsare jB builtintoasingleunit(embedded)inorderto B achieveimprovedperformance.      2. CircularErrorProbable( _CEP_)  Inacircularnormaldistribution,theradiusofthe z circlecontaining50percentoftheindividual zR measurementsbeingmade,ortheradiusofthe R * circlewithinwhichthereisa50percent *!  probabilityofbeinglocated.#&%%&5L#&%%& "! #&%%&jO#&%%& %  7A004Gyro-_astro_Ԁcompasses,andother $b$ deviceswhichderivepositionororientationby b%:% meansofautomaticallytrackingcelestial :& & bodiesorsatellites,withanazimuthaccuracy ' ' ofequaltoorless(better)than5secondsof '!( arc.  (") %O LicenseRequirements  r*J$+   ReasonforControl:NS,MT,AT ",%- ЇControl(s)         L  x CountryChart (- NSappliestoentireentry L  x NSColumn1 /  D  p MTappliestoentireentry L  x MTColumn1  `1 ATappliestoentireentry L  x ATColumn1 8 3  LicenseExceptions   5  D _LVS_:  N/A p7  D _GBS_:  N/A pH 8  D _CIV_:  N/A H 9  ListofItemsControlled   ;  D Unit:$value  =  D RelatedControls:Seealso% + 4-hO  5  7A1046aUOuUea  7hU%+TUԀand% . 4/O8!O  5  7A9946.VOBVN  7,#pV%.!V X>  D RelatedDefinitions:N/A X0?  D Items: 0@ Thelistofitemscontrollediscontainedinthe B _ECCN_Ԁheading. C  % C 7A005Globalnavigationsatellitesystems(i.e. @F _GPS_Ԁor_GLONASS_)receivingequipment,and G speciallydesignedcomponentstherefor.(These H itemsaresubjecttotheexportlicensing I authorityoftheU.S.DepartmentofState, xJ DirectorateofDefenseTradeControls.See22 xPK _CFR_Ԁpart121.)%CW  P (L  D Noteto7A005 :Seealso7A105and7A994. "N  7A006Airbornealtimetersoperatingat $bQ frequenciesotherthan4.2to4.4_GHz_Ԁinclusive, b%:R havinganyofthefollowingcharacteristics(see :& S ListofItemsControlled).  ' T  LicenseRequirements  ("V  D ReasonforControl:NS,MT,AT r*J$X Control(s)         L  x CountryChart ",%Z ЇNSappliestoentireentry   NSColumn1 (     MTappliestoentireentry   MTColumn1  ATappliestoentireentry   ATColumn1  `     0 4  44  LicenseExceptions  8    _LVS_: 4 N/A     _GBS_: 4 N/A      _CIV_: 4 N/A p   ListofItemsControlled  H    Unit:$value   0  RelatedControls:Seealso% : 4<cfO  5  7A1066_O_trol  7cZ_%:_,4AcO  5  7A9946e`Oy`trol  7c`   andCategory6forcontrolsonradar.    RelatedDefinitions:N/A X   Items: X0 a. Powermanagement;or  b.Usingphaseshiftkeymodulation.   #&%%&O#%  7A008Underwatersonarnavigationsystems, @ usingDopplervelocityorcorrelationvelocity  logsintegratedwithaheadingsource,havinga  positioningaccuracyofequaltoorless(better)  than3%ofdistancetraveledCircularError x Probable(_CEP_),andspeciallydesigned xP componentstherefore.  P ( %ub LicenseRequirements  "!   ReasonforControl:NS,AT ## Control(s) 4  `   0 0  CountryChart`%8% NSappliestoentireentry   NSColumn2 ' ' ATappliestoentireentry 0  ATColumn1(")  LicenseExceptions  p*H$+   _CIV_: 4 N/A  ,%-  D TSR:  N/A (-  ListofItemsControlled  /  D Unit:$value  `1 0 D RelatedControls:4leO  5  7A0086`gOtgList  7gԀdoesnotcontrol ` 82 systemsspeciallydesignedforinstallationon 8 3 surfacevesselsorsystemsrequiringacoustic  4 beaconsorbuoystoprovidepositioningdata.  5 See6A001.aforacousticsystems,and  6 6A001.bforcorrelationvelocitysonarlog p7 equipment.See8A002forothermarine pH 8 systems.H 9D(#D(#  D RelatedDefinitions:N/A   :  D Items:  ; Thelistofitemscontrollediscontainedinthe  = _ECCN_Ԁheading.&%%& X>  %  7A101Accelerometers,otherthanthose A controlledby7A001(seeListofItems B Controlled),andspeciallydesigned C componentstherefor.%j#&%%&j#&%%&  hD  LicenseRequirements  @F  D ReasonforControl:MT,AT H Control(s)         L  x CountryChart xJ MTappliestoentireentry L  x MTColumn1 P (L  D  p ATappliestoentireentry L  x ATColumn1 "N  LicenseExceptions  #P  D _LVS_:  N/A `%8R  D _GBS_:  N/A 8& S  D _CIV_:  N/A ' T  ListofItemsControlled  ("V  D Unit:$value p*H$X 0 D RelatedControls:Thisentrydoesnotcontrol H+ %Y accelerometerswhicharespeciallydesigned  ,%ZD(#D(# * x   anddevelopedas_MWD_Ԁ(MeasurementWhile ( Drilling)sensorsforusein_downhole_Ԁwell  serviceoperations. 0  RelatedDefinitions:N/A   Items:  ` #&%%&k#&%%&a.Linearaccelerometersdesignedforusein 8  inertialnavigationsystemsoringuidancesystems   ofalltypes,usablein missileshavingallofthe   followingcharacteristics,andspeciallydesigned    componentstherefore:#&%%&q#&%%& p  #&%%&^s#&%%& 1(#331, @ 1.Scalefactor repeatabilityless H  (better)than1250_ppm_;and     @ 2.Bias repeatabilityless(better)than   1250microg.    1(#331s ,Vt򀀀 Note: Themeasurementofbiasandscale X0 factorreferstoonesigmastandarddeviation 2  withrespecttoafixedcalibrationoveraperiodof   oneyear.#&%%&s#&%%&  b.Continuousoutputaccelerometersofanytype, j specifiedtofunctionataccelerationlevelsgreater jB than100g,andspeciallydesignedcomponents B therefor.#&%%&^w#&%%&   #&%%&x#&%%&% $ 7A102Alltypesofgyros,otherthanthose z controlledby7A002,usablein rockets, zR missiles,orunmannedaerialvehiclescapable R * ofachievinga rangeequaltoorgreaterthan *!  300km,witharated driftrate stabilityof "! lessthan0.5 degrees(1sigmaor_rms_)perhour "" ina1genvironmentandspeciallydesigned ## componentstherefor.%$yԀ#&%%&x#&%%&  $b$  LicenseRequirements  :& &   ReasonforControl:MT,AT '!( Control(s) 4  `      CountryChart )r#*   MTappliestoentireentry   MTColumn1 J+"%,     0 4 ",%-44 ATappliestoentireentry L  x ATColumn1 (-  LicenseExceptions  /  D _LVS_:  N/A  `1  D _GBS_:  N/A ` 82  D _CIV_:  N/A 8 3  ListofItemsControlled   5  D Unit:$value p7 0 D RelatedControls:N/ApH 8D(#D(# 0 D RelatedDefinitions:1.)Driftrateisdefined H 9 asthetimerateofoutputdeviationfromthe   : desiredoutput.Itconsistsofrandomand  ; systematiccomponentsandisexpressedasan  < equivalentangulardisplacementperunittime  = withrespecttoinertialspace.2.)Stabilityis X> definedasstandarddeviation(1sigma)ofthe X0? variationofaparticularparameterfromits 0@ calibratedvaluemeasuredunderstable A temperatureconditions.Thiscanbe B expressedasafunctionoftime.CD(#D(#  D Items: hD Thelistofitemscontrollediscontainedinthe @F _ECCN_Ԁheading.#&%%&{#&%%& G   D TechnicalNote: Inthisentry,theterm I stabilityisdefinedasameasureoftheabilityof zJ aspecificmechanismorperformancecoefficient zRK toremaininvariantwhencontinuouslyexposedto R *L afixedoperatingcondition.(Thisdefinitiondoes *!M notrefertodynamicorservostability.)(IEEE "N STD528-2001paragraph2.247)#&%%&#&%%& "O  % ( 7A103Instrumentation,navigationequipment b%:R andsystems,otherthanthosecontrolledby :& S 7A003,andspeciallydesignedcomponents ' T therefor.%(  '!U  LicenseRequirements  )r#W  D ReasonforControl:MT,AT J+"%Y  ",%Z Control(s) 4  `      CountryChart (   MTappliestoentireentry   MTColumn1  ATappliestoentireentry   ATColumn1  `  LicenseExceptions  8    _LVS_: 4 N/A     _GBS_: 4 N/A      _CIV_: 4 N/A p   ListofItemsControlled  H    Unit:$value   0  RelatedControls:1.)Forrockets,missiles,or   unmannedaerialvehiclescontrolledunderthe   U.S.MunitionsList(22_CFR_Ԁpart121),items X describedin4teo O  5  7A103.b6֊OCon  7te Ԁaresubjecttotheexport X0 licensingauthorityoftheU.S.Departmentof 0 State,DirectorateofDefenseTradeControls  (See22_CFR_Ԁpart121).#&%%&I#&%%&Ԁ2.)Inertialnavigation  systemsandinertialequipment,andspecially  designedcomponentsthereforspecifically h designed,modifiedorconfiguredformilitary h@ usearesubjecttotheexportlicensing @ authorityoftheU.S.DepartmentofState,  DirectorateofDefenseTradeControls.(See  22_CFR_Ԁpart121.)   RelatedDefinitions:N/A x   Items: xP #&%%&#&%%&a.Inertialorotherequipmentusing (!  accelerometersorgyroscontrolledby7A001, "! 7A002,7A101or7A102andsystems "" incorporatingsuchequipment; ##   #&%%&?# &%%&Note#&%%&w# &%%&:7A103.adoesnotcontrolequipment `%8% containingaccelerometersspeciallydesigned :& & anddevelopedas_MWD_Ԁ(MeasurementWhile ' ' Drilling)sensorsforuseindownholewell '!( servicesoperations. (") #&%%&#&%%&%  b.Integratedflightinstrumentsystems,which r*J$+ include_gyrostabilizers_Ԁorautomaticpilots, J+"%, designedormodifiedforusein rockets,missiles, ",%- orunmannedaerialvehiclescapableofachieving (- a rangeequaltoorgreaterthan300km.%g#&%%&H#&%%& .  D #&%%&#&%%&c.IntegratedNavigationSystems,designedor 0 modifiedforusein rockets,missiles,orunmanned  `1 aerialvehiclescapableofachievinga range ` 82 equaltoorgreaterthan300kmandcapableof 8 3 providinganavigationalaccuracyof200m  4 CircularErrorProbable(_CEP_)orless.#&%%&y#&%%&  5  D #&%%&[# &%%&TechnicalNote:#&%%&Ŗ# &%%&ԀAnintegratednavigation p7 systemtypicallyincorporatesthefollowing rJ 8 components: J" 9 1.Aninertialmeasurementdevice(e.g.,an  ; attitudeandheadingreferencesystem,inertial  < referenceunit,orinertialnavigationsystem);  = 2.Oneormoreexternalsensorsusedtoupdate Z> thepositionand/orvelocity,eitherperiodically Z2? orcontinuouslythroughouttheflight(e.g., 2 @ satellitenavigationreceiver,radaraltimeter,  A and/orDopplerradar);and B 3.Integrationhardwareandsoftware.#&%%&#&%%& C  D  p     #&%%&%#&%%& % , 7A104Gyro-_astro_Ԁcompassesandother BF devices,otherthanthosecontrolledby7A004, G whichderivepositionororientationbymeans H ofautomaticallytrackingcelestialbodiesor I satellitesandspeciallydesignedcomponents zJ therefor.%,К  zRK  LicenseRequirements  *!M  D ReasonforControl:MT,AT "O Control(s)         L  x CountryChart $bQ  D MTappliestoentireentry L  x MTColumn1 :& S ATappliestoentireentry L  x ATColumn1 '!U  LicenseExceptions  )r#W  D _LVS_:  N/A J+"%Y  D _GBS_:  N/A ",%Z   _CIV_: 4 N/A (      4 ListofItemsControlled     Unit:$value  ` 0  RelatedControls:Thisentrycontrols ` 8 speciallydesignedcomponentsforgyro_astro_ 8  compassesandotherdevicescontrolledby   4leO  5  7A0046OР   7ry.  0  RelatedDefinitions:N/A     Items: p  Thelistofitemscontrollediscontainedinthe H  _ECCN_Ԁheading.     % > 7A105ReceivingequipmentforGlobal   NavigationSatelliteSystems(_GNNS_)(e.g._GPS_, X _GLONASS_,orGalileo)havinganyofthe X0 followingcharacteristics,andspecially 0 designedcomponentstherefor.(Theseitems  aresubjecttotheexportlicensingauthorityof  theU.S.DepartmentofState,Directorateof  DefenseTradeControls.See22_CFR_Ԁpart121.)%>  h   #&%%&#1.Designedormodifiedforusein missiles;or @ 2.Designedormodifiedforairborneapplications  andhavinganyofthefollowing:    a.Capableofprovidingnavigation xP informationatspeedsinexcessof600m/s(1,165 P ( nauticalmph); (!    b.Employingdecryption,designedor "" modifiedformilitaryorgovernmentalservices,to ## gainaccessto_GNSS_Ԁsecuredsignal/data;or $`$   c.Beingspeciallydesignedtoemployanti 8& & jamfeatures(e.g.nullsteeringantennaor ' ' electronicallysteerableantenna)tofunctioninan '!( environmentofactiveorpassivecountermeasures. (")  Noteto7A105: Seealso7A005and7A994 p*H$+  ",%-  % ; 7A106Altimeters,otherthanthosecontrolled (- by7A006,ofradarorlaserradartype, . designedormodifiedforusein missiles. / (Theseitemsaresubjecttotheexportlicensing 0 authorityoftheU.S.DepartmentofState,  `1 DirectorateofDefenseTradeControls.See22 ` 82 _CFR_Ԁpart121.)%;8  8 3  &%%&7A107Threeaxismagneticheadingsensors  6 havingallofthefollowingcharacteristics,and p7 speciallydesignedcomponentstherefor.  pH 8  LicenseRequirements    :  D ReasonforControl:󀀀MT,AT   <  Control(s)        CountryChart  X>  MTappliestoentireentry L  x MTColumn1 0@  D  p ATappliestoentireentry L  x ATColumn1 B  LicenseExceptions  hD   D _LVS_:  N/A @F  D _GBS_:  N/A G  D _CIV_:  N/A H  ListofItemsControlled  xJ  D Unit:$value P (L  D RelatedControls:N/A (!M  D RelatedDefinitions:N/A "N  D Items:  "O  a.Internaltiltcompensationinpitch(+/-90 $`Q degrees)androll(+/-180degrees)axes; `%8R b.Capableofprovidingazimuthalaccuracybetter ' T (less)than0.5degrees_rms_Ԁatlatitudesof+/-80 '!U degrees,referencedtolocalmagneticfield;and  ("V  c.Designedormodifiedtobeintegratedwith p*H$X flightcontrolandnavigationsystems. H+ %Y   ,%Z    Note: Flightcontrolandnavigationsystems ( in7A107include_gyrostabilizers_,automaticpilots  andinertialnavigationsystems.#&%%&,#    % s 7A115Passivesensorsfordeterminingbearing b : tospecificelectromagneticsource(direction :  findingequipment)orterraincharacteristics%sD,   designedormodifiedforusein missiles.   (Theseitemsaresubjecttotheexportlicensing    authorityoftheU.S.DepartmentofState, r  DirectorateofDefenseTradeControls.See22 rJ  _CFR_Ԁpart121.)  J"   % u 7A116Flightcontrolsystems(hydraulic,   mechanical,electro-optical,or   electro-mechanicalflightcontrolsystems Z (includingfly-by-wiresystems)andattitude Z2 controlequipment)designedormodifiedfor 2   missiles%u.(Theseitemsaresubjecttothe   exportlicensingauthorityoftheU.S.  DepartmentofState,DirectorateofDefense  TradeControls.See22_CFR_Ԁpart121.)  j  % o 7A117 Guidancesetscapableofachieving  systemaccuracyof3.33%orlessoftherange  (e.g.,a _CEP_of10kmorlessatarangeof  300km)%o.(Theseitemsaresubjecttotheexport z licensingauthorityoftheU.S.Departmentof zR State,DirectorateofDefenseTradeControls. R * See22_CFR_Ԁpart121.)  *!   % ! 7A994Othernavigationdirectionfinding ## equipment,airbornecommunication $b$ equipment,allaircraftinertialnavigation b%:% systemsnotcontrolledunder7A003or7A103, :& & andotheravionicequipment,includingparts ' ' andcomponents,n.e.s.%!  '!(  LicenseRequirements  )r#*   ReasonforControl:RS,AT J+"%,  ",%- Control(s)         L  x CountryChart (-  D RSappliesto0  0(#(#0 (#(#0L (# (#0xL(#L(#RSColumn1/x(#x(# QRS11-00100-100/101and 0 QRS1100050443/569  `1 _Micromachined_ԀAngular ` 82 RateSensors.SeeRelated 8 3 Controls.  4 ATappliestoentireentry L  x ATColumn1  6  D LicenseRequirementNotes: &%%&Thereisnode pH 8 _minimis_levelforforeign-madecommercial L$ 9 primaryorstandbyinstrumentsystemsthat $ : integrateQRS11-00100-100/101orcommercial  ; automaticflightcontrolsystemsthatintegrate  < QRS11-00050-443/569_Micromachined_ԀAngular  = RateSensors(see734.4(a)oftheEAR).#&%%&#Ԁ \>  LicenseExceptions  4 @  D _LVS_:  N/A B  D _GBS_:  N/A C  D _CIV_:  N/A lD  D  p   ListofItemsControlled  DF  D  p        D Unit:$value H 0 D RelatedControls:&%%&QRS11_Micromachined_ I AngularRateSensorsaresubjecttothe |J exportlicensingjurisdictionoftheU.S. |TK DepartmentofState,DirectorateofDefense T ,L TradeControls,unlessthe ,!M QRS11-00100-100/101isintegratedintoand "N includedasanintegralpartofacommercial "O primaryorstandbyinstrumentsystemofthe #P typedescribedin_ECCN_Ԁ4 PO  5  7A9946?OS   7'D,oraircraftof $dQ thetypedescribedin_ECCN_Ԁ9A991that d%<R incorporatessuchsystems,orisexported <& S solelyforintegrationintosuchasystem;or ' T theQRS11-00050-443/569isintegratedinto '!U anautomaticflightcontrolsystemofthetype ("V describedin_ECCN_Ԁ4 O  5  7A9946O   7' ,oraircraftofthe )t#W typedescribedin_ECCN_Ԁ9A991that t*L$X incorporatessuchsystems,orareexported L+$%Y solelyforintegrationintosuchasystem. $,%ZD(#D(# (SeeCommodityJurisdictionrequirementsin ( 22_CFR_ԀParts121;CategoryVIII(e),Note(1))  Inthelattercase,suchitemsaresubjecttothe  licensingjurisdictionoftheDepartmentof  Commerce.Technologyspecifictothe  ` developmentandproductionofQRS11 ` 8 sensorsremainssubjecttothelicensing 8  jurisdictionoftheDepartmentofState.#&%%&#    &%%&RelatedDefinitions:N/A     Items:    Thelistofitemscontrollediscontainedinthe pH  _ECCN_Ԁheading. H    B.TEST,INSPECTIONAND   PRODUCTIONEQUIPMENT     7B001Test,calibrationoralignment 0 equipmentspeciallydesignedforequipment  controlledby7A(except7A994).    LicenseRequirements  h   ReasonforControl:NS,MT,AT @ Control(s) 4  `      CountryChart    NSappliestoentireentry   NSColumn1 x MTappliestoentireentry   MTColumn1 P ( ATappliestoentireentry   ATColumn1 "!  LicenseExceptions  ##   _LVS_: 4 N/A `%8%   _GBS_: 4 N/A 8& &   _CIV_: 4 N/A ' '  ListofItemsControlled  (")   Unit:$value p*H$+ 0  RelatedControls:1.)Seealso4kR)O  5  % F 7B1016O#  7R)%F,% U 4X1O  5  7B1026qO  71%Ud H+ %, and4',O  5  7B9946EOY   7' .2.)Thisentrydoesnotcontrol ,%- test,calibrationoralignmentequipmentfor (- MaintenancelevelI.#&%%&#&%%&.D(#D(# 0 D RelatedDefinition:1.)MaintenanceLevelI: / Thefailureofaninertialnavigationunitis 0 detectedontheaircraftbyindicationsfrom  `1 theControlandDisplayUnit(_CDU_)orbythe ` 82 statusmessagefromthecorresponding 8 3 sub-system.Byfollowingthemanufacturers  4 manual,thecauseofthefailuremaybe  5 localizedatthelevelofthemalfunctioning  6 linereplaceableunit(_LRU_).Theoperator p7 thenremovesthe_LRU_Ԁandreplacesitwitha pH 8 spare.2.)MaintenanceLevelII:The H 9 defective_LRU_Ԁissenttothemaintenance   : workshop(themanufacturersorthatofthe  ; operatorresponsibleforlevelIImaintenance).  < Atthemaintenanceworkshop,the  = malfunctioning_LRU_Ԁistestedbyvarious X> appropriatemeanstoverifyandlocalizethe X0? defectiveshopreplaceableassembly(_SRA_) 0@ moduleresponsibleforthefailure.This_SRA_ A isremovedandreplacedbyanoperative B spare.Thedefective_SRA_Ԁ(orpossiblythe C complete_LRU_)isthenshippedtothe hD manufacturer.MaintenanceLevelIIdoesnot h@E includetheremovalofcontrolled @F accelerometersorgyrosensorsfromthe_SRA_.GD(#D(#  D Items: H Thelistofitemscontrollediscontainedinthe xJ _ECCN_Ԁheading. xPK  D 7B002Equipment,asfollows(seeListofItems "N Controlled),speciallydesignedtocharacterize "O mirrorsforring lasergyros.  #P  LicenseRequirements  `%8R  D ReasonforControl:NS,MT,AT ' T Control(s)         L  x CountryChart )p#W  D NSappliestoentireentry L  x NSColumn1 H+ %Y   ,%Z _MTappliestoentireentry   MTColumn1 ( ATappliestoentireentry   ATColumn1   LicenseExceptions   `   _LVS_: 4 N/A 8    _GBS_: 4 N/A     _CIV_: 4 N/A        4 ListofItemsControlled  p    Unit:$value H    RelatedControls:Seealso4W1 O  5  7B1026O  71~5Ԁand% Y 4[1O  5  7B9946O  71%Y      RelatedDefinitions:N/A     Items:   a._Scatterometers_Ԁhavingameasurementaccuracy X of10_ppm_Ԁorless(better); X0 b._Profilometers_Ԁhavingameasurementaccuracy  of0.5_nm_Ԁ(5angstrom)orless(better).   % 8 7B003Equipmentspeciallydesignedforthe h@  productionofequipmentcontrolledby7A @ (except7A994).%8h    LicenseRequirements     ReasonforControl:NS,MT,AT xP Control(s) 4  `      CountryChart (!    NSappliestoentireentry   NSColumn1 "" MTappliestoentireentry   MTColumn1 $`$ ATappliestoentireentry   ATColumn1 8& &  LicenseExceptions  '!(   _LVS_: 4 N/A )p#*   _GBS_: 4 N/A p*H$+   _CIV_: 4 N/A H+ %,     ,%-  ListofItemsControlled  (-  D Unit:$value / 0 D RelatedControls:#&%%&#&%%&Ԁ#&%%&+#&%%&1.)Seealso% { 4}ԐO  5  7B1036O_  7z!%{,#&%%&n#&%%&(this 0 entryissubjecttothelicensingauthorityof  `1 theU.S.DepartmentofState,Directorateof ` 82 DefenseTradeControls(see22_CFR_Ԁpart 8 3 121)#&%%&#&%%&)and4~ԌO  5  7B9946O_  7v/#&%%&#&%%&.2.)Thisentryincludes:  4 InertialMeasurementUnit(_IMU_Ԁmodule)#&%%&#&%%&  5 tester;_IMU_Ԁplatformtester;_IMU_Ԁstable  6 elementhandlingfixture;_IMU_Ԁplatform p7 balancefixture;gyrotuningteststation;gyro pH 8 dynamicbalancestation;gyrorun-in/motor H 9 teststation;gyroevacuationandfillstation;   : centrifugefixturesforgyrobearings;  ; accelerometeraxisalignstations;  < accelerometerteststation;andfiberoptic  = gyrocoilwindingmachines.#&%%&q#&%%&X>D(#D(# 򀀀RelatedDefinitions:N/A X0?  D Items: 0@ Thelistofitemscontrollediscontainedinthe B _ECCN_Ԁheading.#&%%&3#&%%& C #&%%&n# &%%&% S 7B101#&%%&#&%%& Productionequipment,andother @F test,calibration,andalignmentequipment, G otherthanthatdescribedin2B119to2B122,#&%%& #&%%& H 7B003,and7B102,designedormodifiedtobe I usedwithequipmentcontrolledby7A001to xJ 7A004or7A101to7A104.%S#&%%& #&%%&  xPK  LicenseRequirements  (!M  D ReasonforControl:MT,AT "O Control(s)         L  x CountryChart $`Q MTappliestoentireentry L  x MTColumn1 8& S ATappliestoentireentry L  x ATColumn1 '!U  LicenseExceptions  )p#W  D _LVS_:N/A H+ %Y  D _GBS_:N/A  ,%Z   _CIV_:N/A (  ListofItemsControlled     Unit:$value  ` 0  RelatedControls:#&%%& #&%%&1.)Seealso2B119to ` 8 2B122#&%%&#&%%&,% 7 49FR1O  5  7B0036-OA  7U. o%7 ,4mU. O  5  7B1026Oprod  7 p ,,and4n "O  5  7B9946Oprod  7 .2.)This 8  entryincludes:inertialmeasurementunit   (_IMU_Ԁmodule)tester#&%%&#&%%&;_IMU_Ԁplatformtester;   _IMU_Ԁstableelementhandlingfixture;_IMU_    platformbalancefixture;gyrotuningtest p  station;gyrodynamicbalancestations;gyro pH  run-in/motorteststations;gyroevacuation H  andfillingstations;centrifugefixturesfor    gyrobearings;accelerometeraxisalign   stations;andaccelerometerteststations.#&%%&#&%%&    RelatedDefinitions:N/A     Items: X Thelistofitemscontrollediscontainedinthe 0 _ECCN_Ԁheading.#&%%&i#&E%%&  #&%%&E#&%%& % V 7B102Equipment,otherthanthosecontrolled h by7B002,designedormodifiedtocharacterize h@ mirrors,forlasergyroequipment,asfollows @ (seeListofItemsControlled).%V%    LicenseRequirements     ReasonforControl:MT,AT xP      4  `      Control(s) 4  `      CountryChart (!    MTappliestoentireentry   MTColumn1 "" ATappliestoentireentry   ATColumn1 $`$  LicenseExceptions  8& &   _LVS_: 4 N/A '!(   _GBS_: 4 N/A (")   _CIV_: 4 N/A )p#*  ListofItemsControlled  H+ %,   ,%-  D Unit:$value (-  D RelatedControls:N/A .  D RelatedDefinitions:N/A /  D Items: 0 a.0 D _Scatterometers_Ԁhavingathresholdaccuracyof ` 82 10_ppm_Ԁorless(better).8 3D(#D(# b.0 D Reflectometershavingathresholdaccuracyof  5 50_ppm_Ԁorless(better). 6D(#D(# c.0 D _Prolifometers_Ԁhavingathresholdaccuracyof pH 8 0.5nm(5angstrom)orless(better).#&%%&#&%%&H 9D(#D(#  % | 7B103Speciallydesigned production  < facilitiesforequipmentcontrolledby7A117.  = (Theseitemsaresubjecttotheexportlicensing X> authorityoftheU.S.DepartmentofState, X0? DirectorateofDefenseTradeControls.See22 0@ _CFR_Ԁpart121.)%|  A #&%%&#&%%& % Z 7B994Otherequipmentforthetest, hD inspection,or productionofnavigationand h@E avionicsequipment.%Z   @F  LicenseRequirements  H  D ReasonforControl:AT xJ Control(s)         L  x CountryChart P (L  D ATappliestoentireentry L  x ATColumn1 "N  LicenseExceptions  #P  D _LVS_:  N/A `%8R  D _GBS_:  N/A 8& S  D _CIV_:  N/A ' T  ListofItemsControlled  ("V  D Unit:$value p*H$X  D RelatedControls:N/A H+ %Y  D RelatedDefinitions:N/A  ,%Z   Items: ( Thelistofitemscontrollediscontainedinthe  _ECCN_Ԁheading.     C.MATERIALS 8  [RESERVED]       D.SOFTWARE     C 7D001 Softwarespeciallydesignedor H  modifiedforthe developmentor     productionofequipmentcontrolledby7A   (except7A994)or7B(except7B994).     LicenseRequirements  X   ReasonforControl:NS,MT,RS,AT 0 Control(s) 4  `      CountryChart  NSappliesto software   NSColumn1 h forequipmentcontrolled h@ by7A001to7A004,7A006, @ 7A008,7B001,7B002or  7B003  MTappliesto"software"for0  MTColumn1#&%%& #&%%&N X X{dOӄ  Xx equipmentcontrolledfor xP MTreasons.MTdoesnotapply i A to"software"forequipment Z!2  controlledby7A008.O# X ӄ#N#{d X X##&%%&##XX%&#&%XX&%%& K"#! RSappliesto software   RSColumn1 $# forinertialnavigation $$ systemsinertialequipment, %% andspeciallydesigned &t & componentstherefor,for t'L!'  civilaircraft. L($"( ATappliestoentireentry   ATColumn1#&%%&#&%%& )#*  LicenseExceptions  +%,  ,\&-  D _CIV_:  N/A (-  D TSR:  N/A .  ListofItemsControlled  0  D Unit:$value ` 82 0 D RelatedControls:1.)Seealso% f 4henO  5  7D1016O/ng  7en!]%fԀand 8 3 4ienDO  5  7D9946Ong  7en81.2.)The softwarerelatedto  4 % P 4j(DO  5  7A003.b6Oled  7tr#%P,4qld;O  5  7A0056Occur  7ld/,7A007,4O  5  7A103.b6SOgԀ  7 ,4ptt !O  5  7A1056O).  7tt#C,  5 4rDO  5  7A1066O  78,4tO  5  7A1156mO   7Є,4v[O  5  7A1166O-led  7tr[,4w(O  5  7A1176ON/A  74,or4x47 O  5  7B1036tON/A  74!"Ԁare  6 subjecttotheexportlicensingauthorityofthe p7 U.S.DepartmentofState,Directorateof pH 8 DefenseTradeControls.(See22_CFR_Ԁpart H 9 121.)3.) Softwareforinertialnavigation   : systemsandinertialequipment,andspecially  ; designedcomponentstherefor,notforuseon  < civilaircraftaresubjecttotheexport  = licensingauthorityoftheU.S.Departmentof X> State,DirectorateofDefenseTradeControls. X0? (See22_CFR_Ԁpart121.)0@D(#D(#  D RelatedDefinitions:N/A A  D Items: B Thelistofitemscontrollediscontainedinthe hD _ECCN_Ԁheading. h@E @  <  D  p   7D002 Sourcecodeforthe useofany H inertialnavigationequipmentincluding I inertialequipmentnotcontrolledby7A003or xJ 7A004, orAttitudeandHeadingReference xPK Systems(_AHRS_)(except_gimballed_Ԁ_AHRS_)#&%%&t#&%%&.#&%%&%#&%%&  T ,L  D  p          L LicenseRequirements  "N  D ReasonforControl:NS,MT,AT #P Control(s)         L  x CountryChart d%<R  D NSappliestoentireentry L  x NSColumn1 ' T MTappliestoentireentry L  x MTColumn1 ("V ATappliestoentireentry L  x ATColumn1 t*L$X  LicenseExceptions  $,%Z Ї  _CIV_: 4 N/A (   TSR: 4 N/A   ListofItemsControlled     Unit:$value ` 8 0  RelatedControls:1.)Seealso% b 4denoO  5  7D1026 *O*ng  7encL*%b)Ԁand 8  4eenO  5  7D9946*O*ng  7en +.2.)Thisentrydoesnotcontrol    sourcecodeforthe useof_gimballed_   _AHRS_.   0  RelatedDefinition:_AHRS_Ԁgenerallydiffer p  frominertialnavigationsystems(INS)inthat pH  an_AHRS_Ԁprovidesattitudeandheading H  informationandnormallydoesnotprovide    theacceleration,velocityandposition   informationassociatedwithanINS.    Items:   Thelistofitemscontrollediscontainedinthe X0 _ECCN_Ԁheading. 0  7D003Other software,asfollows(seeListof  ItemsControlled).  h  LicenseRequirements  @   ReasonforControl:NS,MT,AT  Control(s) 4  `      CountryChart x   NSappliestoentireentry   NSColumn1 P ( MTappliesto"software"for0  MTColumn1#&%%&!&#&%%&N X X{dOӄ  X"! equipmentcontrolledfor "" MTreasons.MTdoesnotapply ## to"software"forequipment $$ controlledby7A008.O# X ӄW1#N#{d X X81##&%%&1#&%%&#XX%&#&%XX %% ATappliestoentireentry   ATColumn1#&%%&2#&%%& t'L!'  LicenseExceptions  $)")   _CIV_: 4 N/A *$+   TSR: 4 N/A +%,  ,\&-  ListofItemsControlled  (-  D Unit:$value /  D RelatedControls:Seealso% \ 4^enO  5  7D10365O25  7`5%\5Ԁand% _ 4aen8!O  5  7D99465O5  7,#-6%_5 0 0 D RelatedDefinitions:#&%%&|3#&%%&UKUS.,DataBasedReferenced  `1 Navigation(_DBRN_)systemsaresystems ` 82 whichusevarioussourcesofpreviously 8 3 measuredgeomappingdataintegratedto  4 provideaccuratenavigationinformationunder  5 dynamicconditions.Datasourcesinclude  6 bathymetricmaps,stellarmaps,gravitymaps, p7 magneticmapsor3Ddigitalterrainmaps.#&%%&7#US.,UK.,$7&%%&pH 8D(#D(#  D Items: H 9 #&%%&k9#&E%%&a. Softwarespeciallydesignedormodifiedto  ; improvetheoperationalperformanceorreduce  < thenavigationalerrorofsystemstothelevels  = controlledby7A003,7A004or7A008; X> b. Sourcecodeforhybridintegratedsystems 0@ thatimprovestheoperationalperformanceor A reducesthenavigationalerrorofsystemstothe B levelcontrolledby7A003or7A008by C continuouslycombiningheadingdatawithanyof hD thefollowing: h@E  D b.1.Dopplerradarorsonarvelocitydata; G  D b.2.Globalnavigationsatellitesystems(i.e., I _GPS_Ԁor_GLONASS_)referencedata;or xJ  D b.3.DatafromDataBasedReferenced P (L Navigation(_DBRN_)systems;#&%%&E9#&E%%& (!M #&%%&Ee>#&E%%&c. Sourcecodeforintegratedavionicsor "O missionsystemsthatcombinesensordataand #P employ expertsystems; $`Q d. Sourcecodeforthe developmentofanyof 8& S thefollowing: ' T  D d.1.Digitalflightmanagementsystemsfor ("V  totalcontrolofflight; )p#W  D d.2.Integratedpropulsionandflightcontrol H+ %Y systems;  ,%Z Q* Q|x Q    d.3.Fly-by-wireorfly-by-lightcontrol  systems;    d.4.Fault-tolerantorself-reconfiguring  `  activeflightcontrolsystems; ` 8   d.5.Airborneautomaticdirectionfinding   equipment;     d.6.Airdatasystemsbasedonsurfacestatic p  data;or pH    d.7.Raster-typehead-updisplaysorthree    dimensionaldisplays;   e.Computer-aided-design(CAD) software   speciallydesignedforthe developmentof X  activeflightcontrolsystems,helicopter X0 multi-axisfly-by-wireorfly-by-lightcontrollers 0 orhelicopter circulationcontrolledanti-torqueor  circulation-controlleddirectioncontrolsystems  whose technologyiscontrolledby7E004.b,  7E004.c.1or7E004.c.2. h #&%%&E>#&%%&     4  ` % g 7D101 Softwarespeciallydesignedor  modifiedforthe useofequipmentcontrolled  by7A001to7A006,7A101to 7A107,7A115,  7A116,7B001,7B002,7B003,7B101,7B102,or x 7B103.%gF#&%%&E#&%%&  xP  LicenseRequirements  (!    ReasonforControl:MT,AT "" Control(s) 4  `      CountryChart $`$   MTappliestoentireentry   MTColumn1 8& & ATappliestoentireentry   ATColumn1 '!(  LicenseExceptions  )p#*   _CIV_: 4 N/A H+ %,   TSR: 4 N/A  ,%- Ї ListofItemsControlled  (-  D Unit:$value . 0 D RelatedControls:1.)The softwarerelated / to4yO  5  7A003.b6JOJmput  7qK,4zO  5  7A0056{KOKmput  7K,4@O  5  7A103.b6'LO;Lt  7@|iL,4 O  5  7A1056LOLght  7y- M,4 !O  5  7A1066MOMght  7y-"M, 0 4 DO  5  7A1156ANOUNght  7y-8N,4y-O  5  7A1166NOOght  7y-/O,4 O  5  7A1176OOOght  7y-O,or4 O  5  7B1036HPO\Pght  7y-PԀaresubject  `1 totheexportlicensingauthorityoftheU.S. ` 82 DepartmentofState,DirectorateofDefense 8 3 TradeControls.(See22_CFR_Ԁpart121.)2.)  4  Softwareforinertialnavigationsystemsand  5 inertialequipment,andspeciallydesigned  6 componentstherefor,notdesignedforuseon p7 civilaircraftbycivilaviationauthoritiesofa pH 8 countrylistedinCountryGroupA:1issubject H 9 totheexportlicensingauthorityoftheU.S.   : DepartmentofState,DirectorateofDefense  ; TradeControls.(See22_CFR_Ԁpart121.) <D(#D(#  D RelatedDefinitions:N/A  =  D Items: X> Thelistofitemscontrollediscontainedinthe 0@ _ECCN_Ԁheading. A  D  p % c 7D102Integration software,asfollows(See hD ListofItemsControlled). %cAU#&%%&sG#&%%&  h@E  LicenseRequirements  G  D  p ReasonforControl:MT,AT I Control(s)         L  x CountryChart |TK  D MTappliestoentireentry L  x MTColumn1 ,!M ATappliestoentireentry L  x ATColumn1 "O  LicenseExceptions  $dQ  D _CIV_:  N/A <& S  D TSR:  N/A ' T  ListofItemsControlled  ("V  D Unit:$value t*L$X 0 D RelatedControls:The softwarerelatedto L+$%Y 4HDO  5  7A003.b6MYOaYatio  7rcYԀor4O  5  7A103.b6YOZ   7+?ZԀaresubjecttotheexport $,%ZD(#D(# licensingauthorityoftheU.S.Departmentof ( State,DirectorateofDefenseTradeControls.  (See22_CFR_Ԁpart121.)   RelatedDefinitions:N/A    Items:  ` a.Integration softwarefortheequipment 8  controlledby7A103.b.   b.Integration softwarespeciallydesignedfor    theequipmentcontrolledby7A003or7A103.a. p  #&%%&U#&%%&  % ] 7D103 Softwarespeciallydesignedfor    _modelling_Ԁorsimulationofthe guidancesets   controlledby7A117orfortheirdesign   integrationwith missiles.(Thisentryis   subjecttotheexportlicensingauthorityofthe X U.S.DepartmentofState,Directorateof X0 DefenseTradeControls.See22_CFR_Ԁpart121.)%]}]  0  % ` 7D994 Software,n.e.s.,forthe   development, production,or useof h navigation,airbornecommunicationandother h@ avionics.%`_  @  LicenseRequirements     ReasonforControl:AT x Control(s) 4  `      CountryChart P (   ATappliestoentireentry   ATColumn1 "!  LicenseExceptions  ##   _CIV_: 4 N/A `%8%   TSR: 4 N/A 8& &  ListofItemsControlled  '!(   Unit:$value )p#*   RelatedControls:N/A p*H$+   RelatedDefinitions:N/A H+ %,   Items:  ,%- ЇThelistofitemscontrollediscontainedinthe (- _ECCN_Ԁheading. .  D   E.TECHNOLOGY  8 3 rd D 7E001 TechnologyaccordingtotheGeneral  6 TechnologyNoteforthe developmentof p7 equipmentor softwarecontrolledby7A pH 8 (except7A994),7B(except7B994)or7D H 9 (except7D994).    : #&%%&M]#&%%& LicenseRequirements   <  D ReasonforControl:NS,MT,#&%%&f#&%%&ԀRS,AT#&%%&f#&%%& X> Control(s)         L  x CountryChart 0@ NSappliesto technology x NSColumn1 B foritemscontrolledby C 7A001to7A004,7A006, hD 7A008,7B001to7B003, h@E 7D001to7D003 @F  D  p MTappliesto"technology"0 x MTColumn1#&%%&g#&%%&N X X{dOӄ  XHx(#x(# forO# X ӄ_i#Oӄ  XN#  ӄ@i#Nӄ  #&%%&!i#&%%&#XX%&2#&%XXԀequipmentcontrolledfor I MTreasons.MTdoesnotapply J to"technology"forequipment oK controlledby7A008.O# X ӄi#N#{d X Xj##&%%&Gj##XX%&j#&%XX&%%& o GL  D RSappliesto technology L  x RSColumn1 "N forinertialnavigation "O systems,inertialequipment #P andspeciallydesigned $Q componentstherefor,for %WR civilaircraft W&/ S ATappliestoentireentry L  x ATColumn1#&%%&k#&%%& (!U  LicenseExceptions  )#W  D _CIV_:  N/A g+?%Y  D TSR:  N/A ?,&Z Ї ListofItemsControlled  (   Unit:N/A  0  RelatedControls:1.)Seealso% K 4NO  5  7E1016_oOsoN/  7do%KRoԀand  4O7O  5  7E99463pOGp02,  77up.2.)The technologyrelatedto  ` 4rcO  5  7A003.b6qO.qЇTh  7 Z\q,4 O  5  7A0056qOqЇTh  7 r,7A007,4=  O  5  7A103.b6{rOrevel  7 +r,4 O  5  7A1056)sO=sЇTh  7 ks, ` 8 4 O  5  7A1066sOsЇTh  7 +t,4 rO  5  7A1156tOtЇTh  7 f t,4  O  5  7A1166AuOUuЇTh  7 u,4 O  5  7A1176uOvЇTh  7 /v,4 O  5  7B1036vOvЇTh  7 v, 8  softwarein4 s O  5  7D1016gwO{wЇTh  7 g wԀspecifiedintheRelated   Controlsparagraphof_ECCN_Ԁ4 O  5  7D1016zxOxЇTh  7 x,   4 O  5  7D1026:yONyЇTh  7 |y.a,or4 O  5  7D1036yOyЇTh  7 v -zԀaresubjecttotheexport    licensingauthorityoftheU.S.Departmentof p  State,DirectorateofDefenseTradeControls pH  (see22_CFR_Ԁpart121).#&%%&m#&%%&H    RelatedDefinitions:N/A      Items:   Thelistofitemscontrollediscontainedinthe   _ECCN_Ԁheading. X  7E002 TechnologyaccordingtotheGeneral  TechnologyNoteforthe productionof  equipmentcontrolledby7A(except7A994)or  7B(except7B994).  h  LicenseRequirements  @   ReasonforControl:NS,MT,RS,AT  Control(s) 4  `      CountryChart x NSappliesto technology 0  NSColumn1P ( forequipmentcontrolledby (!  7A001to7A004,7A006, "! 7A008or7B001to7B003 "" MTappliesto"technology"0  MTColumn1#&%%&{#&%%&N X X{dOӄ  X$`$ forO# X ӄK#Oӄ  XN#  ӄ,#Nӄ  #&%%& #&%%&#XX%&k#&%XXԀequipmentcontrolledfor `%8% MTreasons.MTdoesnotapply W&/ & to"technology"forequipment /'!' controlledby7A008.O# X ӄ#N#{d X X##&%%&3#&%%&#XX%&u#&%XX (!( RSappliesto technology   RSColumn1 )#* forinertialnavigation *g$+ systems,inertialequipment g+?%, andspeciallydesigned ?,&- componentstherefor,for (- civilaircraft . ATappliestoentireentry L  x ATColumn1#&%%&#&%%& 0  LicenseExceptions  ` 82  D _CIV_:  N/A  4  D TSR:  N/A  5  ListofItemsControlled  pH 8  D Unit:N/A   : 0 D RelatedControls:1.)Seealso% G 4I7O  5  7E1026?OS02,  77!%G2Ԁand  ; 4J7DO  5  7E9946O'02,  77$U.2.)The technologyrelatedto  < 4DO  5  7A003.b6O for  7;,4;O  5  7A0056Ofor  7/,7A007,4TO  5  7A103.b6ZOnfor  7 ,4 !O  5  7A1056Ofor  7#J,  = 4DO  5  7A1066ȊO܊for  78 ,4O  5  7A1156tOfor  7,4O  5  7A1166 O4for  7b,4(O  5  7A1176̌OThe  7 ,or47 O  5  7B1036{OThe  7 !"Ԁare X> subjecttotheexportlicensingauthorityofthe X0? U.S.DepartmentofState,Directorateof 0@ DefenseTradeControls(see22_CFR_Ԁpart A 121).BD(#D(#  D RelatedDefinitions:N/A C  D Items: hD Thelistofitemscontrollediscontainedinthe @F _ECCN_Ԁheading. G  7E003 TechnologyaccordingtotheGeneral xJ TechnologyNotefortherepair,refurbishingor xPK overhaulofequipmentcontrolledby7A001to P (L 7A004.  (!M  LicenseRequirements  "O  D ReasonforControl:NS,MT,AT $`Q Control(s)         L  x CountryChart 8& S NSappliestoentireentry L  x NSColumn1 '!U MTappliestoentireentry L  x MTColumn1 )p#W ATappliestoentireentry L  x ATColumn1 H+ %Y   ,%Z  LicenseExceptions  (   _CIV_: 4 N/A    TSR: 4 N/A   ListofItemsControlled  ` 8 0  Unit:N/A  0  RelatedControls:Seealso46 O  5  7E9946O X  7jĔ.Thisentry   doesnotcontrolmaintenance technology    directlyassociatedwithcalibration,removal p  orreplacementofdamagedorunserviceable pH  _LRUs_Ԁand_SRAs_Ԁofa civilaircraftas H  describedinMaintenanceLevelIor    MaintenanceLevelII.  0  RelatedDefinition:RefertotheRelated   Definitionsfor7B001.    Items: X Thelistofitemscontrollediscontainedinthe 0 _ECCN_Ԁheading.       4 7E004Other technology,asfollows(seeList h ofItemsControlled).  h@  LicenseRequirements     ReasonforControl:NS,MT,AT  Control(s) 4  `      CountryChart xP   NSappliestoentireentry   NSColumn1 (!  MTappliestoentireentry, 0  MTColumn1"" except7E004.a.7. ## ATappliestoentireentry   ATColumn1#&%%&#&%%& `%8%  LicenseExceptions  ' '   _CIV_: 4 N/A (")   TSR: 4 N/A )p#*  ListofItemsControlled  H+ %,   ,%-  D Unit:N/A (- 0 D RelatedControls:Seealso%  42 O  5  7E1046O͜Rel  7% Ԁand% 3 45K!O  5  7E9946O X  7+#ȝ%3y.D(#D(# 0 D RelatedDefinitions:#&%%&#&E%%& Primaryflightcontrol / meansan aircraftstabilityormaneuvering 0 controlusingforce/momentgenerators,i.e.,  `1 aerodynamiccontrolsurfacesorpropulsive ` 82 thrustvectoring.#&%%&E#&%%&8 3D(#D(#  D Items:  4 a. Technologyforthe developmentor  6  productionof: p7  D a.1.Airborneautomaticdirectionfinding H 9 equipmentoperatingatfrequenciesexceeding5   : MHz;  ;  D a.2.Airdatasystemsbasedonsurfacestatic  = dataonly,i.e.,thatdispensewithconventionalair X> dataprobes; X0?  D a.3.Raster-typehead-updisplaysorthree A dimensionaldisplaysfor aircraft; B  D a.4.Inertialnavigationsystemsorgyro-_astro_ hD compassescontainingaccelerometersorgyros h@E controlledby7A001or7A002; @F  D a.5.Electricactuators(i.e.,_electromechanical_, H _electrohydrostatic_Ԁandintegratedactuator I package)speciallydesignedfor primaryflight xJ control; xPK  D a.6. Flightcontrolopticalsensorarray (!M speciallydesignedforimplementing activeflight "N controlsystems; "O  D a.7. _DBRN_systemsdesignedtonavigate $`Q underwaterusingsonarorgravitydatabasesthat `%8R provideapositioningaccuracyequaltoorless 8& S (better)than0.4nauticalmiles.#&%%&#&%%& ' T b. Development technology,asfollows,for ("V  activeflightcontrolsystems(including )p#W fly-by-wireorfly-by-light): p*H$X  D b.1.Configurationdesignforinterconnecting  ,%Z multiplemicroelectronicprocessingelements ( (on-boardcomputers)toachieve realtime  processingforcontrollawimplementation;    b.2.Controllawcompensationforsensor  ` locationordynamicairframeloads,i.e., ` 8 compensationforsensorvibrationenvironmentor 8  forvariationofsensorlocationfromthecenterof   gravity;     b.3.Electronicmanagementofdata p  redundancyorsystemsredundancyforfault pH  detection,faulttolerance,faultisolationor H  reconfiguration;      Note :7E004.b.3.doesnotcontrol    technologyforthedesignofphysical   redundancy. Z   b.4.Flightcontrolsthatpermit_inflight_ 2  reconfigurationofforceandmomentcontrolsfor   realtimeautonomousairvehiclecontrol;    b.5.Integrationofdigitalflightcontrol, j navigationandpropulsioncontroldataintoa jB digitalflightmanagementsystemfor total B controlofflight;    Note :7E004.b.5doesnotcontrol:      1. Development technologyfor |T integrationofdigitalflightcontrol,navigation T , andpropulsioncontroldataintoadigitalflight ,!  managementsystemfor flightpath "! optimization; ""     2. Development technologyfor $d$  aircraftflightinstrumentsystemsintegrated d%<% solelyfor_VOR_,_DME_,ILSorMLSnavigationor <& & approaches. ' '   b.6.Fullauthoritydigitalflightcontrolor (") _multisensor_Ԁmissionmanagementsystems )t#* employing expertsystems; t*L$+   N.B.: For technologyforFullAuthority $,%- DigitalEngineControl( _FADEC_),see (- 9E003.a.9. . c. Technologyforthe developmentof 0 helicoptersystems,asfollows:  `1  D c.1.Multi-axisfly-by-wireorfly-by-light 8 3 controllersthatcombinethefunctionsofatleast  4 twoofthefollowingintoonecontrollingelement:  5  D  p c.1.a.Collectivecontrols; p7  D  p c.1.b.Cycliccontrols; H 9  D  p c.1.c.Yawcontrols;  ;  D c.2. Circulation-controlledanti-torqueor  = circulation-controlleddirectionalcontrol X> systems; X0?  D c.3.Rotorbladesincorporating variable A geometryairfoilsforuseinsystemsusing B individualbladecontrol. C  D  p       4M7O  5  65OIN/  7w% L 7E101 Technology,accordingtotheGeneral @F TechnologyNoteforthe useofequipment G controlledby7A001to7A006,7A101to 7A107, H 7A115to7A117,7B001,7B002,7B003,7B101, I 7B102,7B103,or7D101to7D103.%Lڶ#&%%&#&%%&  xJ  LicenseRequirements  P (L  D ReasonforControl:MT,RS,AT "N Control(s)         L  x CountryChart #P MTappliestoentireentry L  x MTColumn1 `%8R  D  p RSappliesto use     L  x RSColumn1 ' T ofinertialnavigation '!U systems,inertial ("V equipmentandspecially )p#W designedcomponentstherefor, p*H$X forcivilaircraft. H+ %Y   ,%Z ATappliestoentireentry   ATColumn1 ( 0    04 44  LicenseExceptions     _CIV_: 4 N/A  `   TSR: 4 N/A ` 8  ListofItemsControlled      Unit:N/A    0  RelatedControls:1.)The technology p  relatedto4 O  5  7A003.b6SOgcial  7s/ ,4s O  5  7A0056Ocial  7sw C,4?  O  5  7A103.b6O{  7I,4sO  5  7A1056[Oocial  7s, pH  4sO  5  7A1066O/cial  7s],4sO  5  7A1156Ocial  7s ,4sE O  5  7A1166sOcial  7s9 ,4s O  5  7A1176O3cial  7sa,4sO  5  7B1036Ocial  7s , H  softwarespecifiedintheRelatedControls    paragraphof_ECCN_Ԁ4s O  5  7D1016Ocial  7s>,#&%%&P#&%%&Ԁ4sO  5  7D1026Ocial  7s,.a,or   4sO  5  7D1036Ocial  7sԀaresubjecttotheexportlicensing   authorityoftheU.S.DepartmentofState,   DirectorateofDefenseTradeControls.(See X 22_CFR_Ԁpart121.)2.) Technologyfor X0 inertialnavigationsystemsandinertial 0 equipment,andspeciallydesigned  componentstherefor,notforuseoncivil  aircraftaresubjecttotheexportlicensing  authorityoftheU.S.DepartmentofState, h DirectorateofDefenseTradeControls.(See h@ 22_CFR_Ԁpart121.)#&%%&#&%%&@   RelatedDefinitions:N/A    Items:  Thelistofitemscontrollediscontainedinthe x _ECCN_Ԁheading. xP  % H 7E102 Technologyforprotectionofavionics "! andelectricalsubsystemsagainst "" electromagneticpulse(_EMP_)and ## electromagneticinterference(EMI)hazards, $`$ fromexternalsources,asfollows(seeListof `%8% ItemsControlled).%Ht  8& &  LicenseRequirements  '!(   ReasonforControl:MT,AT )p#* Control(s) 4  `      CountryChart H+ %,     ,%- MTappliestoentireentry L  x MTColumn1 (- ATappliestoentireentry L  x ATColumn1 /  LicenseExceptions   `1  D _CIV_:  N/A 8 3  D TSR:  N/A  4  ListofItemsControlled   6  D Unit:N/A pH 8  D RelatedControls:N/A H 9  D RelatedDefinitions:N/A   :  D Items:  ; a.Design technologyforshieldingsystems;  = b.Design technologyfortheconfigurationof X0? hardenedelectricalcircuitsandsubsystems; 0@ c.Design technologyforthedeterminationof B hardeningcriteriaof.aand.bofthisentry. C  % 0 7E104Design Technologyforthe @F integrationoftheflightcontrol,guidance,and G propulsiondataintoaflightmanagement H system,designedormodifiedfor missiles,for I optimizationofrocketsystemtrajectory.(This xJ entryissubjecttotheexportlicensing xPK authorityoftheU.S.DepartmentofState, P (L DirectorateofDefenseTradeControls.See22 (!M _CFR_Ԁpart121.)%0#&%%&<#  "N  % 4 7E994 Technology,n.e.s.,forthe $`Q  development, production,or useof `%8R navigation,airbornecommunication,andother 8& S avionicsequipment.%4  ' T  LicenseRequirements  ("V  D ReasonforControl:AT p*H$X Control(s)         L  x CountryChart  ,%Z ЇATappliestoentireentry   ATColumn1 (     LicenseExceptions     _CIV_: 4 N/A  `   TSR: 4 N/A ` 8  ListofItemsControlled        Unit:N/A    0  RelatedControls:Technologyspecifictothe p  developmentandproductionofQRS11 pH  sensorsremainssubjecttothelicensing H  jurisdictionoftheDepartmentofState(see    _ECCN_Ԁ4sO  5  7A9946aOucial  7s ,RelatedControls&%%&).#&%%&#  0  RelatedDefinitions:N/A&%%&    Items:    X Thelistofitemscontrollediscontainedinthe ( _ECCN_Ԁheading.  @  <  EAR99ItemssubjecttotheEARthatarenot 8  elsewherespecifiedinthisCCLCategoryorin   anyothercategoryintheCCLaredesignated   bythenumberEAR99.      !      4  `       <  h   #XX%&##XXXX#