What it approves
Installation of Model 2512 weighing system.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
tinitld ,st2ltJ at£Imrrim :ecpertmcntof1:ransportetion-.:federal2l\Jiation2ldministretion ~Upplfmfntel1[~Pf<irrtificetf ~ SH695NW ~~<d-dA/Ik.<krk"'~r~nr/k/~,,?/>~A~d,/k~;'m£d~~nd~~~ ~A4-.yu"#k"M",#~;;;,/kAffl~m,,."JM',~4</fL./ * A/~ Civi1Air ~J'u~~~CAR 10(FAR21.29)andCAR6 dated12/20/56,plusAmendments6-1throu9h6-4 andSpecialrequirementsinlettersdated5/3/60and9/13/61.
~~-.Y~~F~nk. HIIN 7Hl ~: Aerospatiale S.N.I.A.S.
~: SE.3160,SA.316B, SA.318C !i'~~1,6~~ '.~: SA.315B,SA.319B,SA.316C ~ rlnstallationofaModel2512wei9hin9systeminaccordance withOnboardWeighingSystemInstallationInstructionsDrawingNo.2513;or FabricationofDnboardSystemsModelH-48CargoHookLoadCellSysteminaccordance withFAAApprovedOnboardSystemsMasterDrawingListNo.155-007-00,datedJanuary10, 1990,orlaterFAAapprovedrevision;and,Installationofthissysteminaccordance withFAAapprovedOnboardSystemsOwnersManualNo.120-006-00,Revision"C",dated January10,1990,(SeeContinuationSheet) --t;nda~~G;....t:~: Approvalofthischangeintypedesignappliesto the abovemodelhelicoptersonly.Thisapprovalshouldnotbeextendedtohelicoptersof thesemodelsonwhichotherpreviouslyapprovedmodificationsareincorporatedunless itisdeterminedbytheinstallerthattherelationshipbetweenthischangeandanyof thoseotherpreviouslyapprovedmodifications,includingchangesintypedesign,will introducenoadverseeffectupontheairworthinessofthathelicopter(SeeContinuation Sheet).
c;- ./M,-€noI~c.at--,.and/,h,..J~#~~ny~/o-u~~d-.i.1,~._/wiJ~"'~1V--va/~//.Nnuu,"" "'~I-#</-u-"Lt¥..J,u,,- "",nd-r«tf ~nd'«zi, •.•,~ -~ te,,",<'na~~te~~~-<.J/.a//dd -br/k .,u""'';;/M/,'''.,fa..
Y~~J<Um:.u;,kz/u- Y~6 nwnd.,,/' November13,1980 , August2,1990 .'~Y~H.r/'''-n ~I~ .rt/,"~:"44/rah.'" /--r- /--t.r>_, . " 0 /to .• __ v~/;C_ %V'_/P. _ (S'f"ahJ't) AssistantManager,Seattle AircraftCertificationOffice(TItle) Any altaotion of this certificate is punishable ~}/a ,fine of nol txcuding 11,000, or imprisonmml not txcttding 3 yeaTs. 01'both.
This urtifu(J/~ may be 'rQl'Uj"uti in auordn.nu with FAR 2/.n.
~~"~~~4,_:November9,1978 YJ_4,.,t'•••••••~,' December14,1978 fAA foe- 1110-2 (10-611
'linittd .stllltS of9.mnica Bcpartmmtof'[:ransportation-jtdcralalJiationadministration ~upplcmcntel~~pc(icrtifiretc(liontinuetion~h(et) ~~ SH695NW DESCRIPTIONOFTYPEDESIGNCHANGE:(continued) orlaterFAAapprovedrevision.InspectloadcellinaccordancewithSection4.6of OnboardSystemsOwnersManualNo.120-006-00,Revision"C",datedJanuary10,1990,or laterFAAapprovedrevision.
LIMITATIONANDCONDITIONS:(continued) RotorcraftmodifiedinaccordancewiththisSTCmustbeoperatedinaccordancewithan FAAapprovedcopyoftheRotorcraftFlightManualSupplement,revisedAugust2,1990 orlaterFAAapprovedrevision.A copyofthisCertificate,ContinuationSheetNo.
SH695NW,themaintenancemanualandFAAapprovedRotorcraftFlightManualSupplement mustbemaintainedaspartofthepermanentrecordsofthemodifiedhelicopter.
. -1"." •. "'.n'''' .~ .' $I,OOO,or-imprisonment not '.exceedingr3~'yearsJ"QT"bolh.. r'" ,.-'';
FAA FORM al1~2-1 (10-69) : This cerlifi'au may be IrtmJjnwl in tlmJTdance with FAR 21.17.
PAGE 3 OF 3PA.GES
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.