Document 6BXa1YQdvRX8v7e9d9oE8rap3
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< of
The
Boeing
ARR2G
Company
_
0943
Washington, DC
FACSIMILE LEAD SHEET
Please Check One:
Destroy Copy
_X Sender Will Pick Up
Date:O1 ctob0 er .2000
No. of Pages LEAD +4.
`Time Sent
ToCh Auea r rlesM
CompanyUSEnvironmentalProtectionAgency
Bldg
Dept
Oo Se
Phone No.
Fax Phone No. (202) 260-8168
Check Phone No.
Special Instructions:
From:MathewC.Frank
Company: TC heo Boeinm g pany
Bldg
Dep.
oe
wwe
Phone No._703/465-3243
Fax Phone No. _703/465.3034
Check Phone No. _703/465-36 3
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Matt Frank
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T1h2e00BWasiiengn Cio.mpany Angon. 22200-1988
| | October g, 2000
| Charles M. Auer
| |
Director, Office of
PCohlelmutiicoanlPCroenvternotlisonDiavnidsiTonox(i7c4s05)
| AUrSieElPRAioHseBaudiqludairngters
| 1200 Pennsylvania Avenue, Nw.
| Washington, DC 20480
7 soENG
||
Dear Mr. Auer:
|| FcrooersnittsahtieannstpaFhsCyt-d9r28a5,uyiaecaffrllsuu,oidrTiinhnaettesBdocceoiomnmmgperoCcuoinmadplatahnnaydt Ihmsialcsiritutatirciyallitzrieandnpasrpneovrsetrnoatsiiirnocrnga-fdater.treeTrsoittoiernagftiifoignre
|
|
oefxttrheemaeilrycreaffftescthiyvderianuiinchisbiytsitnegmercoosmipoonnoefntthse.seThhyedrFaCul-i9c8paadrdtistidvueehtaosepxrpoovseunre
tothe hydrauiic fluids. The 3M company,
|| dmaatneu,ftahcetruereisrnoof FalCt-e9r8n,atiisvpehmaastiernigalouftorisFCpw-rh9oi8dc.uhctiisocnurorfetnhtlsyctrihteicoanllaydddiotmievset.icT:o
|| |
itRniutlsheeBo(feSuitNnuUgreR'.s) uBtnhoadeteircnsogtuaidnsdacilunsgroictihoaBntocEaeiPmnAga'disnttahbeaintlditsthytetooSpuNrsoUepRoFsCceo-u9al8dSiifgnniiimtfsifhcyoadenrtaNuleiwc fUlsuei.ds
| developmant of a workable substitute material.
|| |
taSiniuyvidaSnaNdtdUhieRticpvrreiteiisnceaclrovamenmtBieo-reecirionasgli'vsaenapbdriolmipitelyritttoayrcoyofaniFtrCci-rna8uf8ot,.tBoouesiengFCis-9r8eqausesathiyndgrtahualtic
|| |
hcTyohdmermaecuorlncitciiafnliuieoddrwhuiotsuhesteohfheotlFhedC-Fu9Gs8-e9sa8dodfistdpiirvtoeidviusectuissnetodhuaritnhcyaocncrtalauoilsniecda-fsllioumioidplsasirysassdtadfeietm.iveU,nitihkee
|| |
oairripfltanhee.hyTdhrearueliics lliittdle n`oepepdorstutnoibtye maintenance workers are required
froerpelxepnoissuhreed.(wEhviechn to wear proper
iisf
tnhoetrae
on an irsouatnineextaecrtnlayl)l,eak
| uinsceluodfinFgC-g9lo8veins,ousrafaeitrycrgalftashsyedsr,aualnidc fplruoitdescwtiilvepgoesapere.lrisAtoesnatalhrrpeerasotutltetoc,toaiupvrperwsooqvruekiseprorfsenfotor,e
| the public at large.
|
Background
|{ Phosphate ester hydraulic luds wers first introduced in the 1950's as a iro
| Trehseissteanpthoflsupidharteepleascteemrefnltuifdosrptehrefhoirgmheldy fsaltaimsfmaacbtolreilpyewtirtohlreeusmp-ebcatsteodeflruiads.n
when uncontaminated. Early in the 1970's, however, it was discoveredthat
2
a
BOEING
Socecvuerrrseedlwechterno-tchheesmeicfalluiedrsobsieocnaomfececrotnatianmcionmapteodnewnitthsoorfgtahneichycdhrlaourliince system sceormvpicoeunwedrseufsoeudndtotcolheaavnehyhdyrdarualuilciccfolmupidonseynsttse.msSwoitmheaasimrpulcahneassin30co0m0mperpcmial cofhltohreinfeluiind tbhyeiarsflmuuidcshamapsl5est.imIensm. aBnayccaaussees,thcehrieorwianesinnocrseuaitsaabdlethaenedroefsfievcetnievess cdleevaenlionpgefdlutihdattheaftfewcatsivenloyteclhilmoirniantaetedde,raosrieofnosrmoulloantgedahsytdhreauclhiicorfliuniedcwoanstent was less than 1000 ppm. This newfluid contained the FC-98 additive. Bosing also
set a maximum fluid in-service limit for chlorine of 200 ppm.
TBohaeirneghfalveeetbseiencnentohereicnutrrroidnugcthiyodnroafutlihcefcluuirdreenrtoshiyodnr-aruelliactefdlupidrsobinle1m9s74i.n the TBehceacursieticoaflidtsifanfteir-eenrcoesihvaesqubaleietinest,hethiasddhiydtriaounliocf fFlCui-d9w8itthotthheeFhCy-d9r8aualdidcitfilvueid. comprises the vast majority of aircraft phosphate ester hydraulic fivid in use tpohdoasyp.haTtoedeasttee,rahllydBroaeuilnigc,flfuoirdsmeurtiMiczeDoFnCn-e9l8l. Douglas, and Airbus approved
cChhlloorriinnaetecdonctlaemainniantgifolnuirdesmianiunsseatsoidganyifiincatnhte
hurdle. United
SWthaitlese,thcehrlosrminaaytebdesonlovne-nts
hayrderastuillliaccftliuviedlysaimn pulseesownitahir5cr0a0ft~th2r0o0u0ghpopumt tchheiowroirnle.d. Boeing is still seeing
Electro-chemical Erosion and itCs onsequences
FmeCt-e9r8iinngtehdegheysdorfacuolnictrfolulidvparlevevsenatnsderleelcattredochhyedmriaculailcecroosmipoonneonnttsh.e aElnedctmreot-aclhecmoimcearlseroorseiodngeisnvwoiltvheisn acnonetlreocltrvoallyvteisc. reCaocnttiroonlbveatlwveeesnarheydtrhaeulpircimfiauriyd targets of electro-chemical erosion. These valves, which are designed to
function for the life of the aircraft, rely on the sharp, accurate edges of their
tpinheteresfreonarelmdapganerctsescothfoatcnhogenetsrsuorltfhtaehceerefoslrpoawocnotsfueahtycodhrraartuahlceitcevrafillsuvtieidcctsoonotafrnoalasvc.atluvOaetnoara.nndTathihreepldaence,aythoifs could be noticad by slow or partial rasponsa from the component controlled by
the valve.
Valve itself.
eUrnodseironnaolrsmoalinocpreeraasteisngthceonadmiotiuonnts,oaf
intemal leakage small amount of
within the valve fluid travels through
vcaalllveedsianntdemoatlhelreackoamgep.onVeanltvseteorporsoivoindienbcerneeafsiecsiatlhleubarmiocautniotn.ofTfhluiisd stmhaatllpaflsoswes1s
through each valve even when the valves are not operating. As a consequence
opfuampssigniinftihcaenhtyidnrcaruelaiscesiynstinetmermnaalylneoatkabgee ltahrrgoeuegnhoaugnhumtboeprowofervatlhveess,ytshteems
3
a BOEING
arierqpuliarneed ofporereaftfieocntsi.ve Irteesmpsotnypsicfarlolym ptohewehryderdaublyichayldlryapuloiwcesriendcliutdeemfsirgehqtuciornetdroflo,r
abirrackrea,ftloapnedriantgiognesa.r,Hayndrdasutleiecriflnugidspyestrefmosr.manScoemies ooff ptahretsiecuslyarstceomnscearrnabcreictiacualsefo
the redundancy provided by a common-mode failure that
mauflfteicptlsealhlysdryasutleimcsssyismtuelmtsaniesocusolmyp.romised
if
thera
is
rSeinndceereaxicrecrsasfitvseyisntteemrnsalinleeffaekcatgivee,witthheinaiarihiyndersaaurleicrseqyusitreemd
has the potential to monitor, by
to
peerroisoidoincctaesntibneg,dettheectiendt.emaWlhleenaktahgeelienaekaacghe ehyxdcreaeudlisctshyestmeanmu.faTchtiusreisr'hsolwimits,
the airine replaces the failed valves or components containing valves.
Development, Qualification, and Approval of Substitute
nGoirveitns tshueppplrioervsenhapveerfeonrgmaangceed oifn FaCn-y9r8esoevaerrcthhaenpdasdtev2e5lyoepamresn,tneoiftahenr Bosing faolrtearnsautbisvteitaunttei-meartoesriivaelafdodritFiCv-e.98,InBooeridnegr'tsosduepvpellioepr,s qwuoaullifdyhaanvdeotbotainiintiaapteproval ernesgeaagrechinaenxdtdenesvievleoplmaebnorta,tocroymteestuipngw.ithBoaecianngdaidnadteFAreApwlaocuelmdetnhtenfluried,quainred aepxptreonvsailv,e tqhuealfilfuiicdatmiuosntteusntdinegrgaondfulfllifgihitghatpsperrovviacle. evOanlucaetiwoen (rFeScEa)iv.e fInigohrtder to initiate the FSE, al formal fluid qualification testing must first be completed, rreecpeoirvtsedi.ssued, willing and capable operators identified, and FAAapproval
The FSE demonstrates the following:
+
TCohmaptatthiebicliatnydoifdattheefclainddpiedraftoerwmisthasexeisxtpiencgtfelduiidns tihn ealslypsrtoepmo;rtions;
That the candidate hydraulic system;
fluid
does
not
cause
any
abnormal
wear
in
the
CTohmapattitbhierleitayreofnothaebcnaonrdmiadlatcehfalnuigdewsittho
the the
hydraulic pumps; acidity level, nor any
adverse
Thchaatngtehes ftlouitdheisfmliuisdcitbhlate icnouallldrdateigorsawdiethseyxsitsetminpgefrlfuoidrsmawnitche;noanhdarmful
effects.
The FSE gives Bosing and operators the reassurance that the fluid will be
suitable in the airplane environment.
Based on past experience, research and development, laboratory testing, and
Ffluilglhtfiagphptrsoevnavliocfe aevcaalnudaitidoantewislubtsatkiteuatte laeraestan1tiyceiapra.teAdftteortFaSkEe,fr2omsa5mptloi8nygeaorf s.
sOEa ING
a`cnodmdpeotneerniotrsatmiuosn.t be removed from the airplanes and examined for signs of wear aAdsdiatirveesuflotr, FiCti-s9e8x,psehcotuelddtBooteaikneg7b1e0c1o0mypeealrlsetdotdoedvoelsoop. and qualify a substitute 4W8e5-a3p2p4re3csihaoteulydoyurouatnteenetdiotnotcoontthiasctimmpeortprainotritsosuoeu.r m|eceatninbgeorneaOcchteodbeart (1720,3) 2000.
Sincerely, Matti) Famke Matthew Frank
~ 5a