STC SE2007NM

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13 </lhQ Civil Air YJL.Jml'/':v~,;:~9'L.Jjtn (:to,:?,. Military engine model R-3350-93, which is a model R-3350-91 engine remanufactured to a R-3350-93 configuration per USAF SAAMAcontract AF41(608), is approved when inspected, altered and tested in accordance with Afpendix 1 of T.B.M., Inc. Report 70/72-01. The R-3350-93 compared to the R-3350-91, includes a three planetary impeller drive and other changes to improve durabiiity and increase performance. The R-3350-93 engine is identified by the USAF 'arts Manual T.O. 2R-R3350-54 dated July 1, 1974.

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jt,/,/ E-272 Curtiss - wright R-3350-91 Engine ;;!:~i{;~H~!

This approval is limited to R-3350-93 rnx1el engines which, if previously overhauled, were overhauled per military manuals listed under Item 5 of Page 4 of the continuation sheet. This approval should rot be extended to any engine on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved rnx1ifications will introduce ro adverse effect upon the airworthiness of the engine.

A.Refer.l;o continuation sheet. Page 3..) ,.7A~, ~.,"/'0'€4U' AI nu ~ ..u1l0#'~ 'ny4al'a ,u;,-s4€h'£J" ~.I'aJiJ /,... "1j0.1'(~/'01dull ""HUN n' #,,/#<1..,u.n/#/~U-~ July 21, 1983 (/ , .F .J'QU' I~ ~nc.6 .

2 SEP 1983 :'.,,', :i ~ l.c"atulf') Manager, Los Angeles Aircraft Certification Office (T.ll, ) A'!}' a/l~ra/ion of 'niscertificate is punis'ltiblt ~)' afmt of no! exceeding 1/ .GOO.or imp,isonmtnl not ucuding 3 }'tors. or both.

This urtificQU m~)' h# Irans/nud,n auo,danu with fAR 2/.17, .AA.(III.oo '110-2 (10-611

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i)cpartrncntof~ran.sportation-jcdcralamationadministration ~upplcmcntQI1C~pc(icrtificQtc (ltontinuation~hcct) JV~ Thelimitationsandconditionsof TypeCertificationDataSheetNo.E-272apply exceptas follows:

3) TheR-3350-93modelengineisapprovedonlyforlowratioinductioncompressor driveoperationwithauto-richmixture,andmanualsparkretardsetting

(20.- 20.)using100/130minimumgradeaviationgasoline.

An FAAapprovednameplateshallbe installedadjacentto theexistingnameplate includingthefollowinginformation:

STCNo.SE2007NM STCHolder-TulareAircraftserviceInc.

EngineModel- R3350-93 EngineSIN FuelOctane 100/130 ------- IgnitionTiming- ManualSparkRetard(20.- 20.)

FuelMixture AutoRich PowerRating - Takeoff2880HP @ 2900RPM (AtSeaLevel) Max.Cont.2380HP @ 2600RPM EngineWeightandC.G.location(dry) 3720lbs.

..•.;.;, ..: , CompleteEngineWeight C.G.{i)Cation- Forwardof !'bunting FlangeCenterline AbovePropellerShaft Leftof VerticalCenterline

18.06 .133 .014 inches inches lnches ~~"::!;~.~H ~:~~:lilt:~!,'j Completeengineincludes- allaccessarydrives,enginelubricationsystem, firesealadaptercomplete,allpipingandcontrolsbetweenengineparts,fuel injectionsystem,mastercontrolscreensandgaskets,ignitionsystem,priming systemon engine,coolingairdeflectorsandbaffles,accessorydrivecovers, androckerboxdrainmanifoldandsumpsystemperWrightServiceBulletinNo.

TC18E-166A.

Arrya/leration of this ctrtijicatt ispurzish,!hltbyajint of no/txcuding 11,000, or imprisomnm/ no/ txcuding 3 years, or both..~l~:~i.~.~.J ';:.

',,' FAA FORM 8110-2-1 (1Q-69) Tltir '"/if~lJl,rna)'1"trofuj""d in dCco,danu willa FAR 2/.17.

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SE2007NM 'Ilnlttd,StaltJDr>1mmn 1Elrpartrnrntof1:ronsportation-j'rdrral9IJiation9dmini.sttation ~upp([mtntal1t~ptQ:trtificatt (ltontinuationcShcct) JtI:~ PerformanceRating- (Ref.Curtiss-wrightOperatingInstructionsdatedMay 1963 forR-3350-34,42,93 and981TC18EA-1engines) TheR-3350-93modeliseligibleforusewithgrade100/130,108/135octanefuel, withauto-richmixtureat thefollowingratings:

4) withlowimpellergearratio R-3350-93

20.BTCIgnition Max.Cbntinuoushp,rpm,in.Hg.,at:

Criticalpressurealtitude(ft.)

SeaLevelpressurealtitude 2440-2600-42.5-8800 2380-2600-44.5-S.L.

Operationinhighimpellerratiowithanygradefuelisnotpermitted.

5) The followingMaintenance,OverhaulandPartsManualsor laterapproved revisionsarerequiredforcontinuedairworthiness:

USAFOverhaulManualT.O.2R-R3350-53datedDecember15,1977andUSAFParts ManualT.O.2R-R3350-54datedJuly1, 1974arerequiredforModelR-3350-93 engines.

2940-2900-50.0-7300 2880-2900-52.0-S.L.

WrightAircraftEnginesTurboGompoundMaintenanceManualforModel972TC18DA & 988TC18EAseriesenginesrevisedJune1, 1969(Sections70-83)is required fortheR-3350-93engine.

Takeoff(5min)hp,rpm,in.Hg.,at:

Criticalpressurealtitude(ft.)

SeaLevelpressurealtitude - Atry alt~rationof this certificat~is puni5ha.,hl~byafine of not excuding 11,000, or imprisonmtnt not excuding 3 years, or both_ :~9:1' .' ~jj ~'0. ..~~ FAA FORM 811().2-1 (To-e.g) T1I.il ("Ii/leott may bt t,a~JtT"d in ouo,da1UI M-,h FAR 2/.#7.

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