. ,t. \rrL Drl Y^na. &- 90-09-10 -lr' -t t'lH Jr 90-09-10 TEXAS TNSTRUMENTS: Amendment 39-6565' Docket No.89-ANE-38."l+tii:t:i'llx',[:']ii"'h?[""5:i"'"::]:,u'u't;6'"lio -'o ::; 1-' 1990' ""tliE5tpti"n." i, required no later than November \ unless alreadt "tt:il?'t;:tEnti"t ou".h"ating of the.applicable .i..uft)-u.9li"l!lu';;orh." rexas- rnstru'di';i;!i6i'"li'*l;i r,r6i"Ti-eit6-7's ina -io and t"todels, 6rc2o-7' *ii"::l"i'.hii?^fg"':lo;*!i "J[:::';itH'ln!';:hii3.t3]'lE dite codes "ttf,ltlti!3rlut8f"4n"., installed in' b9i-!9I rimitii'-io, "iiiiiiit-.manufactured"'" bv Boeins cPmTgf:l3l aiipiane' ina r-otIrreeg.n*;B;"";1"]n91orui"'yl.".iuBHl]?]]li ?:3]l:!fi:".':ir:lli'br"ak"rs, (P,r-r1!3ot?1")19 -aie "'.I9ttoti;o,"n",, service-{ated a1 i o,t, n, "i?:i,.,i16'i"nii,*fffi:"tt"il3t:1'e+.Bii:i'^:*3- ro!3TTs"i'lfiq zo?:)i:6ij6o' iil;:i"., :i 6rc6- r0' on servi ce bul I eti n iSitif;lt l8ltrneed -corporati -0e3-24-, l3i6,gB:i3 ,ti*:ii'T:3lin;1'331 7's and 6rc20-10'"ii;u:i,I?i-i:glt"l';il"g"fi ffii3:f:]"";+'rubstantiatins data-bv an-owner or ; Fo^ Ai'"*o,"thin"s''"ilii:i*f;-"+;;;;, "p",""[3] ![il'1iHof compliance with the ;' ;Ti;;;;|" 'eitrod- [;,i:ii;iutri'rt'ih"ii[:l"i:i'lllTlilitiiii::" -nviati.on ni st rati on:riiil:"::' 12 New - certification se rvi c;, rea!1il -ndmi ' H;i#;'EiJ;;;i*!,,,1;tt,:tili:'i3"; nUlAAliSy'B:H,3,"3?i"..i u" on May 30, 1990. Page 1 aP k*-'un- ^' ?*:il[;ft , ::,iili*:,:l$$lif !:iil?ih, s'#;;il. si:Ti;'' illi*t"i'il::' ii:q-'eiii:n*l+ir'li'ii;iIf t"t"985ilot as indicated' unless accomplished I "n.", nequired ? iH : : " r ! :' r ffi *'' "1" "ii' ::::iil:\ilir,ii'sri:" iltii:iffi rnriu;.r"*, inoriE?riiri;itl;fiilffiiiilrlilfu:ii t:i*i-:t3$fl 4iiliiil .^, * Fh ::l iiil,rs, lll:lllF,illii"ru.r*r*o", " . ia:#ii:i.ii;:ii!,li!.liii"i!ul[l't:::l'ft 33t"ln?il;,i'9':"il6li ii;i";;;;;pp;"rc' t!:-nfli;*llii*:i:t' lii,liiliia;lriii*r*r;*ir|i:liilli;;il1$liila:ii;lr tft q[:kiiln*llctifii'ilrdtlifl rl:mllil lfr lieft . "oo ?iffi:irili;;'$Tf li;i;ri"tar *i;il*:'ir;::i;*':*"iro til] 3'i3:"'?'"i91'$X;o o" :lr:lliitk"il!l;i[3'l?".:fiqti*l:'",ilf; in accordance (d) special flight permits qay'be-issued i*.i: i:il:lit*1;3*i:,6ii:i# :ailt{iif;il, tE:fltiliurr il;;iii;;ti;iu:i+i;e't;iii!;;*;*ill$ir:!ii**.,,, . ii?3i13'3;ii;.f i'ti.tl|i:ifi ih'eit;g+Hii:'"fiit;3ttiit.?' .n" l- li', m;"m;fr t*il;qfi i$i' *r$et " i$irl;.Hr?:ir,iii!::r;ril![:,i$iilii;r*i*:,*:gpili,n :*:. !ii;i:,"lli'i"nLl,.Eliil*tt :lf l:"'36''"" :Bi:ti, ct,"::'i'-fiT 1994' ;;;ntil;""in?!'",n"ndr"nt becomes effective on Hovember 25' CONTACT: FOR FURTHER INFORMATION ii'*i*l ;l'1,i;fr [':qi;;t iil#di" ii:li*iinntl;rff Page 1 a t 94-21-06 fax (3L0) 988-521-0. Page 2 rl 2{ u /+ [^.,T t$*6 *{kpa?t l- l'\ ' 87-06-09 87-06-09 MECHANTCAL PRODUCTS. rNC.: Anendment 39-5585. Applies to the following 4001, 4200, 4310, and 8500 series clrcult breakers: uechanical Products Militarv Amoere Date oes ignati on oesi gnati on nati ng code 4001 seri es M52207 3 1 thru 5 8501- thru 8636 4200 seri es M52657 4 7/2 thru 5 8430 thru 8636 4310-001, MS3320 1 thru 5 8605 thru 8636 -019 seri es 8500 seri es (None) l- thru 5 851,4 thru 8636 This AD does not applv to circuit breakers produced or installed prior to tuly'23, L984, (the thirtieth week of 1984), or to circuit breakers which have been insoected bv the manufacturer, found free of defect, marked with a fohite inverted z or ar oainted on the terminal end. and have an additional date code with an "R" prefix. NorE 1: As an aid in identification. the bodies of these circuit breakers are blue or black in color, NoTE 2: The date codes listed above are used to identify the vear and week of manufacture: i.e.. 8430 indicates the thirtieth foeek of 1984. and 8636 indicites the thirtv-sixth-side, week of 1986. These date c6des may be found on the top, or bottom of the ci rcui t breakers. NoTE 3: As an examole. the unit mav have the additional date code of R8642, wheie "R" desiqnateS a retest by tuechanical products, 86 indicates the yeir L986, and 42 ihdicates the 42nd week of 1986. compliance: nequired as indicated after the effective date of thi s AD. To prevent possible loss of essential equipment, electrical fire, or electrical shock hazard on aircraft, accomplish the fo1 | owi ng : (a) within six months after the effective date of this AD, accompl i sh the following: (l-) visually inspect for installation in aircraft of any of the applicable circuit breakers and prior to further flight remove all units from service. or (2) visually inspect fo|installation in aircraft of any of the aoolicable circuit breakers in accordance with the instructibns contained in uechanical Products service rnstruction (identification on the back page with the date 10/86) and, prior to further flight, remove all units from service, or (3) oetermine that none of the applicable circuit breakers are installed in aircraft by an examination of mai ntenance and/or purchasing records. NorE: Return of all affected ci rcuit breakers to Mechanical products, rnc., 1824 River street, P.o. Box 729, Jackson, Michiqan 49204, is recommend and may enhance replacement part availibilitv. (b) Aircraft may be flown in accordance with FAR 21,.L97 to a location where the no may be accomplished, Page 1 87-06-09 .A (c) nn adjustment to the comp'liance time or an equ'iva'lent \ means of compliance with this AD may be used if approved by the Manager, Chicago Rircraft Certification Office, ACE-115C, 2300 EastDeVonAvefrue,Desplaines,Illinois60018 nll persons affected by this directive may obtain cop'ies of the docuinent(s) referred t6 herein upon reque-st to lvtechahical products, Inc., 1824 River Street, P.O. eox 729, Jackson, Michiqan 49204; or may examine the document(s) referred to herein at FAA, office of the- Regional counsel, Room 1558, 601 East 12th street, Kansas c'ity, lrti ssouri 64106. this amendment becomes effective on lpril 27, 1987. Page 2 03-04-06 2003-04-06 VARIOUS AIRCMFT: Amendment 39-13054. Docket 2003-NM-41-AD APPLICABILITY: Ai rcraft, certificated in any cateqory, equipped with a Honevwell primus rr RNz-850/-851 rnteqrated r.rivioation- unit havino a Dart numbi:r identified in Table L of this io; includiiq, but not limit6d to BAE Systems (operations) Limited (:etstream) r'aodel 410i ai rplanes; gombardier (c1415 ? BD-700-1A10 series ai rplanes; eombardier cL-215-6811 variant) series ai rplanes; cessna Model 560, 560xL, and 650 airplanes; Dassault tvtodel [4vstere-Falcon 50 series airp]anes: oornier rvlodel 328-L00 and -300 series airplanes; Empresa grasileira de Aeronautica S,A, (EI4BRAER) Model EMB-135 and -145 series airolanes: Leariet Model 45 airolanes: Ravtheon l,todel ttawker 800xp and Hawkei L000 airpllnes; and sikorsky uodei s-261, s -76g. and s-76c aircraft. rable 1 of this AD follows; TABLE 1.-Integrated t'tavigation Unit part Numbers PART NUMBERS 7510100-811 through 7510100-814 ncl usive 7510100-83L throuqh 7510100-834 ncl usi ve 7510100-901 throuoh 75101-00-904 ncl usi ve 7510100-911 throulh 7510100-914 ncl usi ve 75101-00-921- throuqh 7 5t0t00-924 ncl usi ve 7510100-931 through 751-0100-934 nclusive NoTE 1: This AD appl ies to Honevwell Primus rr RNz-850/-851 rnteqrated Naviqation units ihitalled on anv aircraft. reqardless'or of whethei tne ai rciaft has been otherwi se modi fi ed. al tered. reoai red i n the area subiect to the requirements of this AD. For aircraft that have been modified, altered, dr repaired so that the performance of the requi rements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (e) of this AD, The reouest should include an assessment of the effect of the modification, alteration, or repai r on the unsafe condition addressed by this AD; and, if the unsafe condition has not been elininated, the request should include specific proposed actions to address it. coMPLTANcE: nequi red as i ndi cated , unl ess accompl i shed previ ous1y. To ensure that the flightcrew has an accurate glideslope deviation indication, accompl ish the'fol lowing: COI4PLIANCE TIME FOR ACTION (a)- within 5 days after the effective date of this ao, accomplish the requirements of either paragraph (b) or (c) of this no. INSPECTION TO DETERI4INE PART NUMBER (b)- perform a one-time general visual inspection of the modification plate for the ttoneywell Frimus rr ruv-850 i'tavigation Receiver l,todule; part number 7 5Loi34-8L'J,, -831, -901, or -9ff; which is part of the ttoneywell primus rr RNz-850/-851 rntegrated tlavigation unit; to deteimine if uod "1" has beeh installed.