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NE 0G U">Z UB 0U 0!/ UNPU<UNUN(U vUNU, 1 72 0c 72, 72^ 1 72BI 08 0 0 0 0u 1mU 0 1e 0 0 0 0C 00 0- 0*) 0'S 0$z 1u! 0" 01# 0L$ 0d% 0;& 0' 0' 0( 0y) 0A* 0+ 0@+ 0, 0, 0- 0y. 0D/ 0 0 00 01 00P2 0<2 02 0>z3 0v3 0`.4 0`4 0`4 0`N5 0`5 086 0F6 027 0J7 0:F8 0Y8 0_8 0 89 0jB: 0; B*0= D/Z= D+= 0= D/8? 0g? 065@ 0k@ 0:sA 0^A 0< BU6GBU*}B\\GSDDPRINT\QMS_000(9 Z6Times New Roman RegularX($USUS.,A6/ b-:i+003|xU2[+[ 0_level1   , 8.` hp x (#823  ..   8.` hp x (#8  \  `&Times New Roman\  `*Times New RomanTT*+ (_2623  ..<T+f :Outline001_6 j   DL 23  ..  2( 4 <DL2 j (hH  Z 6Times New Roman Regular%\  `$Times NewRoman 6Times New Roman Regular(hH  Z 6Times New Roman Regular'\ `(hH  Z6Times New Roman Regular(9 ZTimes (5hCEKQW]cioAutoList11.1.1.1.1.1.1.1.1.(;3$2#  0  .3  0  1i)%(EhCEKQW]cioAutoList21.1.1.1.1.1.1.1.1. 88XXdXXd8<l :Body Text In )   ;1Mi q !y)x (#;  _UX` hp x (#_XXX ) *G+M (_25   /%` ` hp x /23  ..  5+ ` hp x 5  *D+M (_24   ," hp x ,23  ..  5+ ` hp x 5  *A+M (_23  ` ) hp x )23  ..  5+ ` hp x 5  *>+M (_22   &hhp x &23  ..  5+ ` hp x 5   035;AGMSY_11.1.1.1.1.1.1.1.*;+M (_21   #p x #23  ..  5+ ` hp x 5   (35;AGMSY_2a.a.a.a.a.a.a.a.*8+M (_20  h  p x 23  ..  5+ ` hp x 5  *5+M (_19   pp x 23  ..  5+ ` hp x 5  *2+M (_18    x 23  ..  5+ ` hp x 5  * (_1723  Ԁ<c+f :Outline001_1   /%  <DL/23  ..  2( 4 <DL2  <`+f :Outline001_2  ] ,"9 9 <DL,23  ..  2( 4 <DL2  <]+f :Outline001_3 j  ) <DL)23  ..  2( 4 <DL2 j <Z+f :Outline001_4   &DL&23  ..  2( 4 <DL2  <W+f :Outline001_5  e #AADL#23  ..  2( 4 <DL2  3#37=CIQYag1.a.i.(1)(a)(i)1)a)<Q+f :Outline001_7   L23  ..  2( 4 <DL2  <N+f :Outline001_8  m IIL23  ..  2( 4 <DL2  <K+f :Outline001_9 j   L23  ..  2( 4 <DL2 j *GM (_16   /%` ` hp x /23  Ԁ  5+ ` hp x 5  *DM (_15   ," hp x ,23  Ԁ  5+ ` hp x 5  *AM (_14  ` ) hp x )23  Ԁ  5+ ` hp x 5  *>M (_13   &hhp x &23  Ԁ  5+ ` hp x 5  *;M (_12   #p x #23  Ԁ  5+ ` hp x 5  *8M (_11  h  p x 23  Ԁ  5+ ` hp x 5  *5M (_10   pp x 23  Ԁ  5+ ` hp x 5  (2M &_9    x 23  Ԁ  5+ ` hp x 5  ( &_823  (GM &_7   /%` ` hp x /23   5+ ` hp x 5  (DM &_6   ," hp x ,23   5+ ` hp x 5  (AM &_5  ` ) hp x )23   5+ ` hp x 5  (>M &_4   &hhp x &23   5+ ` hp x 5  (;M &_3   #p x #23   5+ ` hp x 5  (8M &_2  h  p x 23   5+ ` hp x 5  (5M &_1   pp x 23   5+ ` hp x 5  &2M $_    x 23   5+ ` hp x 5  0.Normal<:Definition T<AA:Definition L , 5+ ` hp x 5  5+ ` hp x 586Definition(''&H1      (&H2  (&H3  (&H4 XXX (&H5  (&H6  20Address8MM6Blockquote , , 5+ ` hp x 5   5+ ` hp x 5,*CITE,dl*CODEKe<6X9`(Courier NewKS \  `&Times New RomanS42Emphasis64Hyperlink    <:FollowedHype    4go2Keyboard Ke<6X9`(Courier NewKS \  `&Times New RomanS <:Preformatted/%  ,Kk %#/Ke<6X9`(Courier NewKS \  `&Times New RomanS/%  ,Kk %#/<:zBottom of 7[(X7  ?f%2A`Arial?  S \  `&Times New RomanS7\(X7&  d dZ)1dxd'dxd<:zTop of For7^(X7  ?f%2A`Arial?  S \  `&Times New RomanS7\(X7Z)2dxd0KS.SampleKe<6X9`(Courier NewKS \  `&Times New RomanS0.Strong 8dl6TypewriterKe<6X9`(Courier NewKS \  `&Times New RomanS42Variable: 8HTML MarkupB      2 0CommentB  <6X9`(Courier New%2A`Arial !USUS.,  _nXXXX   `     h      p      `     h      p   pp4(#BillingCode:351033P  (#(#K(#   `     h      p      x  DEPARTMENTOFCOMMERCE  ` BureauofIndustryandSecurity   15_CFR_ԀParts772and774 p DocketNo. S#X XXXO# X XXX Ԁ030825213321301#X XX X 0# SXXXX Ԁ  p _RIN_Ԁ0694AC76   RevisionstotheExportAdministrationRegulationsbasedonthe2002MissileTechnology  ControlRegimePlenaryAgreements#X XXXݚ#X XXX Ԁ#X XXX #XXXX  X  AGENCY:BureauofIndustryandSecurity,Commerce. $X" ACTION:FinalRule '#&  @-(, n 8 XXdd8   _SUMMARY:#X XXX# TheBureauofIndustryandSecurity(BIS)isamendingtheCommerceControl d List(CCL)toreflectchangestotheMissileTechnologyControlRegime(MTCR)Annexthat < wereagreedtobyMTCRmembercountriesattheSeptember2002PlenaryinWarsaw,Poland.   BISisalsoamendingcertainentriesontheCCLtoclarifythescopeofandjurisdictionfor   controlsonglobalnavigationsatellitereceivingequipment.  ` X XXX EFFECTIVEDATE:Thisruleiseffective:(DATEOFPUBLICATION). t  FORFURTHERINFORMATIONCONTACT:StevenB.Clagett,Director,NuclearandMissile $ TechnologyControlsDivision,BureauofIndustryandSecurity,Telephone:(202)4821641.     `    SUPPLEMENTARYINFORMATION H Background \ #X XXX s#XXXX TheMissileTechnologyControlRegime(MTCR)isanexportcontrolarrangementamong33  " nationsincludingtheworldsmostadvancedsuppliersofballisticmissilesandmissilerelated #  materialsandequipment.Theregimeisdesignedtostemthespreadofrocketsandunmannedair %X" vehiclessystemscapableofdeliveringweaponsofmassdestructionbyestablishingacommon '0!$ exportcontrolpolicy(theGuidelines)andasharedlistofcontrolleditems(theAnnex)thateach l)#& countryimplementswithitsownnationallegislation. D+$(  -&* WhiletheMTCRwasoriginallymeanttopreventthespreadofmissilescapableofcarryinga d nuclearwarhead,itwasexpandedinJanuary1993toalsocoverdeliverysystemsforchemical < andbiologicalweapons.TheonlyabsoluteprohibitionintheregimesGuidelinesisonthe   transferofcomplete productionfacilitiesspeciallydesignedforitemsintheMTCRAnnex.   #X XXXd #ThisruleamendsPart772oftheExportAdministrationRegulationstoaddthedefinitionsfor 8   Range(MTCR)and Payload(MTCR)tothelistoftermsandrevisestheCommerceControl t  List(CCL)toreflectchangestotheMTCRAnnexthatwereagreedtobyMTCRmembersatthe L  September2002PlenaryinWarsaw,Poland.Inaddition,thisruleamendscertainentriesonthe $ CCLtoclarifythescopeofandjurisdictionforcontrolsonglobalnavigationsatellitereceiving  equipment(ExportControlClassificationNumbers(ECCNs)7A005,7A105and7A994). p ThefollowingECCNsareamendedasdescribed:   1C111:MixedOxidesofNitrogenadded(MTCRAnnexchange). 4  7A005:Crossreferenceto7A105and7A994added(clarification). #  7A103:IntegratedNavigationSystemsadded(MTCRAnnexchange). '0!$ 0   7A105:Entryreformattedtoclarifydescriptionofitemscovered(MTCRAnnexchange).Cross D+$( referenceto7A005and7A994added(clarification).-&*(#(# Ї7A994:Relatedcontrolsparagraphdeleted(clarification). d 9A106:FlightControlServovalvesadded(MTCRAnnexchange).    XXXX  SavingClause  ` ShipmentsofitemsremovedfromeligibilityforaLicenseExceptionorexportwithoutalicense t  (NLR)asaresultofthisregulatoryactionthatwereondockforloading,onlighter,ladenaboard L  anexportingcarrier,orenrouteaboardacarriertoaportofexport,on(INSERTDATEOF $ PUBLICATION),pursuanttoactualordersforexporttoaforeigndestination,mayproceedto  thatdestinationunderthepreviouseligibility#X XXX#XXXX ԀforaLicenseExceptionorexportwithoutalicense p (NLR)#X XXX#XXXX ԀsolongastheyhavebeenexportedfromtheUnitedStatesbefore(INSERTDATE30 H DAYSAFTERDATEOFPUBLICATION).Anysuchitemsnotactuallyexportedbefore   midnight,on(INSERTDATE30DAYSAFTERDATEOFPUBLICATION),requirealicense \ inaccordancewiththisregulation.#X XXXw#X XXX   4   #X XXX #XXXX AlthoughtheExportAdministrationActexpiredonAugust20,2001,ExecutiveOrder13222of #  August17,2001(66FR44025,August22,2001),asextendedbytheNoticeofAugust7,2003 %X" (68FR47833,August11,2003),continuestheRegulationsineffectundertheInternational '0!$ EmergencyEconomicPowersAct.#X XXXr#X XXX   l)#&  RulemakingRequirements -&* #X XXX ##XXXX   1.ThisfinalrulehasbeendeterminedtobenotsignificantforpurposesofE.O.12866. d   2.#X XXXݭ#X XXX Notwithstandinganyotherprovisionoflaw,nopersonisrequiredtorespondto,nor   shallanypersonbesubjecttoapenaltyforfailuretocomplywithacollectionofinformation,   subjecttotherequirementsofthePaperworkReductionAct,unlessthatcollectionofinformation  ` displaysacurrentlyvalidOfficeofManagementandBudgetControlNumber.#X XXX z#XXXX ԀThisruleinvolves 8  acollectionofinformationsubjecttothePaperworkReductionActof1980(44U.S.C.3501et t  seq.).ThiscollectionhasbeenapprovedbytheOfficeofManagementandBudgetundercontrol L  number06940088,#X XXXZ#X XXX  MultiPurposeApplication,whichcarriesaburdenhourestimateof45 $ minutesforamanualsubmissionand40minutesforanelectronicsubmission. x   #X XXX #XXXX   3.#X XXX #X XXX Ԁ#X XXX %!#XXXX ThisruledoesnotcontainpolicieswithFederalismimplicationsasthattermisdefined H underE.O.13132.#X XXXh!#XXXX     h      p      #X XXX("#X XXX   4.TheprovisionsoftheAdministrativeProcedureAct(5U.S.C.553)requiringnoticeof 4  proposedrulemaking,theopportunityforpublicparticipation,andadelayineffectivedate,are  " inapplicablebecausethisregulationinvolvesamilitaryandforeignaffairsfunctionoftheUnited #  States(5U.S.C.553(a)(1)).Further,nootherlawrequiresthatanoticeofproposedrulemaking %X" andanopportunityforpubliccommentbegivenforthisinterimrule.Becauseanoticeof '0!$ proposedrulemakingandanopportunityforpubliccommentarenotrequiredtobegivenforthis l)#& ruleundertheAdministrativeProcedureActorbyanyotherlaw,theanalyticalrequirements D+$( oftheRegulatoryFlexibilityAct(5U.S.C.601etseq.)arenotapplicable.Therefore,this -&* regulationisissuedinfinalform.Althoughthereisnoformalcommentperiod,publiccomments d onthisregulationarewelcomeonacontinuingbasis.Commentsshouldbesubmittedto < MatthewBlaskovich,OfficeofExporterServices,BureauofIndustryandSecurity,Department   ofCommerce,P.O.Box273,Washington,D.C.20044.    ListofSubjects  8  15CFRParts772and774 L    Exports,Foreigntrade.#X XXX "#X XXX  $   Accordingly,parts772and774oftheExportAdministrationRegulations(15CFRparts p 730799)areamendedasfollows: H #X XXX (# Part772[AMENDED] \   % (031  1. X XXX  Theauthoritycitationsfor15CFRpart772isrevisedtoreadasfollows: #X XXX *#X XXX   "   Authority: 50U.S.C.app.2401etseq.;50U.S.C.1701etseq.;#X XXX ++#XXXX ԀE.O.13222,66FR %X" 44025,#X XXX+#Ԁ3CFR,2001Comp.,p.783;NoticeofAugust7,2003,68FR47833,X XXX August11,2003.#X XXX ,# '8!$   2.Section772.1isamendedbyaddingdefinitionsfor Payloadand Range(MTCR) L+$( inalphabeticalorderasfollows: $-&* 772.1DefinitionsofTermsasUsedintheExportAdministrationRegulations(EAR). d    ` *****     XXXX  Payload(MTCR).Thetotalmassthatcanbecarriedordeliveredbythespecified  ` rocketsystemorunmannedaerialvehicle(UAV)systemthatisnotusedtomaintainflight.#X XXX_.# 8   Note :Theparticularequipment,subsystems,orcomponentstobeincludedinthepayload L  dependsonthetypeandconfigurationofthevehicleunderconsideration. X XXX  ,  TechnicalNotes: x  a.#X XX X C0#Ԁ0  BallisticMissilesP(#(#   1.0 ` Payloadforsystemswithseparatingreentry vehicles(RVs)includes:(` (#` (#    ` i.0 TheRVs,including:l (# (# 0  0` (#(#0 ` (#` (#A.Dedicatedguidance,navigation,andcontrolequipment;D  (# (# 0  0` (#(#0 ` (#` (#B.Dedicatedcountermeasuresequipment;" (# (#    ` ii.0 Munitionsofanytype(e.g.,explosiveornonexplosive);#  (# (#    ` iii.0 Supportingstructuresanddeploymentmechanismsforthemunitions(e.g. %h" hardwareusedtoattachto,orseparatetheRVfrom,thebus/postboost '@!$ vehicle)thatcanberemovedwithoutviolatingthestructuralintegrityof |)#& thevehicle;T+$( (# (#    ` iv.0 Mechanismsanddevicesforsafing,arming,fuzing,orfiring;,-&* (# (#    ` v.0 Anyothercountermeasuresequipment(e.g.,decoys,jammers,orchaff d dispensers)thatseparatefromtheRVbus/postboostvehicle;< (# (#    ` vi.0 Thebus/postboostvehicleorattitudecontrol/velocitytrimmodulenot   includingsystems/subsystemsessentialtotheoperationofotherstages.  (# (#  X XXX   2.#X XX X :7# Payload X XXX Ԁforsystemswithnonseparatingreentryvehiclesincludes: 8  0   ` i.0 (#(#Munitionsofanytype(e.g.,explosiveornonexplosive);t  (# (#    ` ii.0 Supportingstructuresanddeploymentmechanismsforthemunitionsthat L  canberemovedwithoutviolatingthestructuralintegrityofthevehicle;$ (# (# 0   ` iii.0 (#(#Mechanismsanddevicesforsafing,arming,fuzingorfiring; (# (# 0   ` iv.0 (#(#Anycountermeasuresequipment#X XX X 7#(e.g.,decoys,jammers,orchaff p dispensers)thatcanberemovedwithoutviolatingthestructuralintegrity H ofthevehicle. X XXX   (# (# b.SpaceLaunchVehicles Payloadincludes: \   1.0 ` Satellites(singleormultiple);4 ` (#` (#   2.0 ` Satellitetolaunchvehicleadaptersincluding,ifapplicable,apogee/perigeekick  " motorsorsimilarmaneuveringsystems;# ` (#` (# c.SoundingRockets Payloadincludes: %X"   1.0 ` Equipmentrequiredforamission,suchasdatagathering,recordingor '0!$ transmittingdevicesformissionspecificdata;l)#&` (#` (#   2.0 ` Recoveryequipment(e.g.,parachutes)thatcanberemovedwithoutviolatingthe D+$( structuralintegrityofthevehicle.-&*` (#` (# d.CruiseMissiles Payloadincludes: d   1.0 ` Munitionsofanytype(e.g.,explosiveornonexplosive);<` (#` (# 0  2.0` (#(#Supportingstructuresandmechanismsforthemunitionsthatcanberemoved   withoutviolatingthestructuralintegrityofthevehicle; ` (#` (#   3.0 ` Mechanismsanddevicesforsafing,arming,fuzingorfiring; `` (#` (# 0  4.0` (#(#Countermeasuresequipment(e.g.,decoys,jammersorchaffdispensers)thatcan 8  beremovedwithoutviolatingthestructuralintegrityofthevehicle;t ` (#` (# 0  5.0` (#(#Signaturealterationequipmentthatcanberemovedwithoutviolatingthe L  structuralintegrityofthevehicle;$` (#` (# e.OtherUAVs Payloadincludes:    1.0 ` Munitionsofanytype(e.g.,explosiveornonexplosive);p` (#` (# 0  2.0` (#(#Mechanismsanddevicesforsafing,arming,fuzingorfiring;H` (#` (# 0  3.0` (#(#Countermeasuresequipment(e.g.,decoys,jammersorchaffdispensers)thatcan   beremovedwithoutviolatingthestructuralintegrityofthevehicle;\` (#` (# 0  4.0` (#(#Signaturealterationequipmentthatcanberemovedwithoutviolatingthe 4  structuralintegrityofthevehicle; "` (#` (# 0  5.0` (#(#Equipmentrequiredforamissionsuchasdatagathering,recordingortransmitting #  devicesformissionspecificdata;%X"` (#` (# 0  6.0` (#(#Recoveryequipment(e.g.,parachutes)thatcanberemovedwithoutviolatingthe '0!$ structuralintegrityofthevehicle.l)#&` (#` (# ***** D+$(  -&* Ї (Eh80% ! !#X XX X ;# X XXX  Range(Cat8)***    h  d  Range(MTCR).Themaximumdistancethatthespecifiedrocketsystemorunmannedaerial   vehicle(UAV)systemiscapableoftravelinginthemodeofstableflightasmeasuredbythe   projectionofitstrajectoryoverthesurfaceoftheEarth.  `  TechnicalNotes:  t  a.0  Themaximumcapabilitybasedonthedesigncharacteristicsofthesystem,whenfully $ loadedwithfuelorpropellant,willbetakenintoconsiderationindeterminingrange.(#(# b.0  TherangeforbothrocketsystemsandUAVsystemswillbedeterminedindependentlyof p anyexternalfactorssuchasoperationalrestrictions,limitationsimposedbytelemetry, H datalinksorotherexternalconstraints. (#(# c.0  Forrocketsystems,therangewillbedeterminedusingthetrajectorythatmaximizes \ range,assumingICAOstandardatmospherewithzerowind.4 (#(# d.0  ForUAVsystems,therangewillbedeterminedforaonewaydistanceusingthemost  " fuelefficientflightprofile(e.g.,cruisespeedandaltitude),assumingICAOstandard #  atmospherewithzerowind.%X"(#(# #X XX X G#***** '0!$  Part774[AMENDED]  D+$(  -&*   3. X XXX  Theauthoritycitationfor15CFRpart774isrevisedtoreadasfollows:  d   Authority: #X XXX N#XXXX Ԁ50U.S.C.app.2401etseq.;#X XXXN#XXXX Ԁ50U.S.C.1701etseq.;10U.S.C.7420;10   U.S.C.7430(e);18U.S.C.2510etseq.;22U.S.C.287c,22U.S.C.3201etseq.,22U.S.C.6004;   30U.S.C.185(s),185(u);42U.S.C.2139a;42U.S.C.6212;43U.S.C.1354;46U.S.C.app.  h 466c;50U.S.C.app.5#X XXXAO#X XXX ;Sec.901911,Pub.L.106387;Sec.221,Pub.L.10756#X XXX P#XXXX ;E.O.13026,61 @  FR58767,3CFR,1996Comp.,p.228;#X XXXZ#X XXX  4    a.2.Metalfuels,otherthanthatcontrolledbytheU.S.MunitionsList,inparticlesizesof #  lessthan#X XXX k]#X XXX z60x106m(60micrometers)#X XXX L^#X XXX ,whetherspherical,atomized,spheroidal,flakedor %X" ground,consisting97%byweight#X XXX ^#X XXX ormore#X XXX ^_#X XXX Ԁofanyofthefollowing: '0!$ #X XXX _#X XXX    ` a.2.a Zirconium; D+$(    ` a.2.b Beryllium; -&*    ` a.2.c Magnesium;or d    ` a.2.d Alloysofthemetalsspecifiedbya.2.atoa.2.cabove.#X XXX `#X XXX  <    ` TechnicalNote:Thenaturalcontentofhafniuminthezirconium(typically2%to   7%)iscountedwiththezirconium.#X XXX a#X XXX      a.3.Liquidoxidizers,asfollows: 8     ` a.3.a.Dinitrogentrioxide; L     ` a.3.b.Nitrogendioxide/dinitrogentetroxide;     ` a.3.c.Dinitrogenpentoxide; H      ` a.3.d.#X XXX b#.MixedOxidesofNitrogen(MON) p    \  X XXX   TechnicalNote:#X XX X d# X XXX ԀMixedOxidesofNitrogen(MON)aresolutionsofNitricOxide(NO)in  " DinitrogenTetroxide/NitrogenDioxide(N#X XX X e# X XhX 2#X XX X e# X XXX O#X XX X f# X XhX 4#X XX X Zf# X XXX /NO#X XX X f# X XhX 2#X XX X f# X XXX )thatcanbeusedinmissilesystems.There #  arearangeofcompositionsthatcanbedenotedasMONiorMONij,whereiandjareintegers %X" representingthepercentageofNitricOxideinthemixture(e.g.,MON3contains3%Nitric '0!$ Oxide,MON2525%NitricOxide.AnupperlimitisMON40,40%byweight).#X XX X /g#X XXX  x  l)#& b.Polymericsubstances: -&* Ї  b.1.Carboxy-terminatedpolybutadiene(CTPB); d   b.2.Hydroxy-terminatedpolybutadiene(HTPB),otherthanthatcontrolledbytheU.S.   MunitionsList;     b.3.Polybutadiene-acrylicacid(PBAA); 8    b.4.Polybutadiene-acrylicacid-acrylonitrile(PBAN); L  c.Otherpropellantadditivesandagents:    c.1.Butacene; H   c.2.Triethyleneglycoldinitrate(TEGDN); \   c.3.2-Nitrodiphenylamine;  "   c.4.Trimethylolethanetrinitrate(TMETN); %X"   c.5.Diethyleneglycoldinitrate(DEGDN).#X XXX h#XXXX  l)#& #X XXXyl#   `  X XXX #X XX X l#X XXX &u%XX   #X X%&uJm#5.#X XXX +m#SupplementNo.1toPart774(theCommerceControlList),Category7Navigation -&* andAvionics,ECCN7A005isamended X XXX byaddingaNotetoreadasfollows:#X XX X Hn#X XXX  d  7A005Globalnavigationsatellitesystems(i.e.GPSorGLONASS)receivingequipment,   andspeciallydesignedcomponentstherefor.(Theseitemsaresubjecttotheexport   licensingauthorityoftheU.S.DepartmentofState,OfficeofDefenseTradeControls.See  ` 22CFRpart121.)  8  Noteto7A005:Seealso7A105and7A994. L  #X XXX n#0  6.SupplementNo.1toPart774(theCommerceControlList),Category7Navigation(#(# andAvionics,ECCN7A103,ListofItemsControlledSection,isamended X XXX byrevisingthe p  Itemsparagraphtoreadasasfollows:#X XX X yq#X XXX &u%XX  H  #X X%&u,r#7A103Instrumentation,navigationequipmentandsystems,otherthanthosecontrolledby 4 7A003,andspeciallydesignedcomponentstherefor.     *****  #X   ListofItemsControlled&u%XX   l'!$   #X X%&us#Unit:*** *$( 0  RelatedControls:***,h&*(#(#   RelatedDefinitions:*** d   Items: < a.Inertialorotherequipmentusingaccelerometersorgyroscontrolledby7A001,7A002,7A101   or7A102andsystemsincorporatingsuchequipment;  `   Note :7A103.adoesnotcontrolequipmentcontainingaccelerometersspeciallydesigned t  anddevelopedasMWD(MeasurementWhileDrilling)sensorsforuseindown-holewell L  servicesoperations. $   b.Integratedflightinstrumentsystems,whichincludegyrostabilizersorautomaticpilots, p designedormodifiedforusein missiles. H #X XXX r# c.IntegratedNavigationSystems,designedormodifiedforusein missilesandcapableof \ providinganavigationalaccuracyof200mCircularErrorProbable(CEP)orless. 4    TechnicalNote:Anintegratednavigationsystemtypicallyincorporatesthefollowing #  components: %X" 1.0  Aninertialmeasurementdevice(e.g.,anattitudeandheadingreferencesystem,inertial l)#& referenceunit,orinertialnavigationsystem);D+$((#(# 2.0  Oneormoreexternalsensorsusedtoupdatethepositionand/orvelocity,either -&* periodicallyorcontinuouslythroughouttheflight(e.g.,satellitenavigationreceiver,radar d altimeter,and/or&u%XX ԀDopplerradar);and<(#(# #X X%&uz#3.0  Integrationhardwareandsoftware.  (#(#  0  7.SupplementNo.1toPart774(theCommerceControlList),Category7Navigation `(#(# andAvionics,ECCN7A105isrevised X XXX toreadasfollows:UKUS.,#X XX X 7|# X XXX   8     7A105#X XX X |#X XXX &u%XX US.,UK.,i|Ԁ#&u%%&u}##X X%&u=}# X XXX UKUS.,ԀReceivingequipmentforGlobalNavigationSatelliteSystems(GNSS)(e.g.GPS, L  GLONASS,orGalileo)havinganyofthefollowingcharacteristics,andspeciallydesigned $ componentstherefor.(TheseitemsaresubjecttotheexportlicensingauthorityoftheU.S.  DepartmentofState,OfficeofDefenseTradeControls.See22CFRpart121.)  p #X XX X }#US.,UK.,}  1.Designedormodifiedforusein missiles;or   2.Designedormodifiedforairborneapplicationsandhavinganyofthefollowing: \ 'SXX'  a.Capableofprovidingnavigationinformationatspeedsinexcessof600m/s(1,165nautical 4  mph).  " b.Employingdecryption,designedormodifiedformilitaryorgovernmentalservices,togain #  accesstoGNSSsecuredsignal/data;or %X" c.Beingspeciallydesignedtoemployantijamfeatures(e.g.nullsteeringantennaor '0!$ electronicallysteerableantenna)tofunctioninanenvironmentofactiveorpassive l)#& countermeasures. D+$(  -&* Noteto7A105:Seealso7A005and7A994 d   8.SupplementNo.1toPart774(theCommerceControlList),Category7Navigation   andAvionics,ECCN7A994,ListofItemsControlledSectionisamended X XXX byrevisingthe    RelatedControlsparagraphtoreadasfollows:#X XX X # X XXX UKUS.,   ` 7A994Othernavigationdirectionfindingequipment,airbornecommunicationequipment, t  allaircraftinertialnavigationsystemsnotcontrolledunder7A003or7A103,andother L  avionicequipment,includingpartsandcomponents,n.e.s. $ #X XX X #X XXX US.,UK.,ń*****  p   ListofItemsControlled#X XXX >#UKUS., X XXX    Unit:*** \ RelatedControls: N/A #X XX X #US.,UK., X XXX UKUS., 4   RelatedDefinitions:*** " Items:***  #  #X XX X #X XXX US.,UK.,Ӈ*****#X XXX u#UKUS., X XXX  '8!$  US.,UK.,#X XX X #0  9.SupplementNo.1toPart774(theCommerceControlList),Category9PropulsionD+$((#(# Systems,SpaceVehicles,andRelatedEquipment,ECCN9A106,ListofItemsControlled -&* Sectionisamended X XXX byrevisingthe Itemsparagraphtoreadasfollows:#X XX X n# d  X XXX 0XXSX09A106Systemsorcomponents,otherthanthosecontrolledby9A006,usablein missiles,   asfollows(seeListofItemsControlled),#X XXX #X XXX Ԁandspeciallydesignedforliquidrocketpropulsion   systems#X XXX #.  ` X XXX  ****#X XXX #X XXX Ԁ* 8   ListofItemsControlled  L  0  Unit:***(#(# 0  RelatedControls:***p(#(# 0  RelatedDefinitions:***H(#(#   Items:   a.Ablativelinersforthrustorcombustionchambers; 4  b.Rocketnozzles;  " c.Thrustvectorcontrolsub-systems; #  Ѐ %X"   TechnicalNote: Examplesofmethodsofachievingthrustvectorcontrolcontrolledby9A106.c '0!$ includes: l)#&     1.Flexiblenozzle; -&*     2.Fluidorsecondarygasinjection; d     3.Movableengineornozzle; <     4.Deflectionofexhaustgassteam(jetvanesorprobes);or       5.Thrusttabs.&u%XX    #X X%&uT#d.Liquidandslurrypropellant(includingoxidizers)controlsystems,andspeciallydesigned t  componentstherefor,designedormodifiedtooperateinvibrationenvironmentsofmorethan10 L  grmsbetween20Hzand2000Hz. $  ̀  Note: Theonlyservovalvesandpumpscontrolledby9A106.d,arethefollowing: p     a.Servovalvesdesignedforflowratesof24litersperminuteorgreater,atanabsolute   pressureof7Mpaorgreater,thathaveanactuatorresponsetimeoflessthan100ms; \     b.Pumps,forliquidpropellants,withshaftspeedsequaltoorgreaterthan8,000rpmor 4 withdischargepressuresequaltoorgreaterthan7Mpa.        ,&* e.Flightcontrolservovalvesdesignedormodifiedforusein missilesanddesignedor d modifiedtooperateinavibrationenvironmentofmorethan10gRMSovertheentirerange < between20Hzand2KHz.   #X XXX #X XXX #X XXX w#DATED: t  MatthewBorman p ActingAssistantSecretary H forExportAdministration