SCHEDULE OF IMPLEMENTATION FROCEDURES

FOR THE

U.S./REPUBLIC OF INDONESIA BILATERAL AIRWORTHINESS AGREEMENT

Marre No.

.iN '1' goD U en ON • • iii

CHAPTER 1.

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H.

~ENRRAL •

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CHAPTER 2 . RRODUCT TYPE DESIGN APPROVAL PROCEDURES , 20. n.

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223. 214 . 225. 226. 227 .

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~ 5 , , , 8 8 9

>C 232. 1 0 233. t 11 234. Approval pror.edure!l 11

24. Design Approyals o f Produc t s Ot her Than Ail'cra f t, Ai (,Q,ril tt Engi nes. and Prope llers 11

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CHAPTER 3.

31.

311.

312..

U 32. 13

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" 3. . . ,

" 331. 15 332. 16 333. 16

CHAPTER 4. ACCOUNTABILITY 16

4 0. Gellera l 1 6 410. Communi cat ion 16 4 1 1 . NQt j. f i cat iou of unsafe condi t i ons 16 -112. Accident/incident investigation ilss i st_ilnr.p. 1.7 413. Mand,"l ton: ;lirw("]rth:i ness act i ons 1"1

CHJ\.J?T ER 5 . MUTIlAL COOPERATION AND TECHNI CAL ASSI S"l'ANCR 17

50. COtl)l!Ullications and Meetings 1") 51. Technical E'Valuilt j.,on A~Hli>ltancp. 18 52. Rxchange or. Tn f Qrma tiou on Standi;lr ds and

Certif i c~tiQn Systemp 1. 8

CHAPTER 6. SPECIAL ARRANGEMENTS 18

APPENDIX A

ii

INTRODUCTION

Thi S document <:(.mt~in!l the proccdurl'll'l <'level oped by t he Federal Avi ... tion Administration (FAA) and Lile !)i rector«te General of Air Communi cation (OOAC) , hereinafter referred to aa the rartil'lS, to 1,mplement the ll.grl;lement between the Govex:nment of t he United States of Ameriea (U.S .) and the Government of the Republic of Indonesia (ROI) concerning the airworthiness certil:'ication, approval, or acceptance of imported aeronautical products a[fected by exchange of notes at Jakarta, Indones ia, J anuary 23. 1987, and is intended to facilitate the approval process for aircraft and oLher aeronautical products being imported or exported between the U.S. and the ROI . It may oe jointly rcviewed at any time at lhe requel:1t of either the PAA ox: t .he DGAC, anu will oe reviewed pcrioc1iclllly, tak jng in to account improvcments , additions, or changes suggested by either the FAA (')1'" the WAC, by U.S. anu .1<01 aviation industry aAs(')ciati.ons or Ule ir member companies. or hy other interested parLies, to assure that the procedures remain current. Amendments may be developed by the FAA Aircraft Certification Service and t he DGAC Directorate ot Airworthiness Certifications and iSl:1ued following approval hy the FAA Admini strator ~d the DGAC Director General.

1~ese procedures provide for designated officials within the FAA and WAC to make spec ial arranHements as they deem neceSiSlax:y in unique situations to implement thiR Rchedule.

Suggestions (or imprOVemeIJ;t are welcomed and can b e 1lc1(j;ressed to either of the addresses below, whO are responsible for t he administrative proceSS of keeping Lhis document current .

(FAA address) Aircra ft Certification Service, AIR-4 Federal Aviation Administrat ion 800 Independence Avenue, sw. Washing tOIl , U.C. 20591 U.S.A .

(WAC address) Directorate of Airworthiness Certi fications Directorate General of Air Communications Jalan Angkasa No. 8 Kemayoran JaKarta 10002 P.O. Box 3049 INDONBSIh

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CHAPTER 1. GENEML.

1 0. ~lrDo~p'. Thi~ ~chedulc sets forth procedures agreed upon between the Federal Avi a t ion Admi nistrat10n (FAA) and t.he Directora te Ceneral of Air Communications (DGAC) to carry out the objec t ives of t.he Agreement. between the United StateD of America and t he Republic of I n dones i a concer n i ng the a i rworthine8$ cert if i cation, approval , or acceptance of imported civil aer o na utica l p r oducts, hereafter referred to as the b i lat eral airworthiness agreelUeut (BM).

11 . Bas is. The basis f or this Schedule, which is authorized by Section 8 of the BM, is s t a t ed 1n Section 1 o f t he BAA .

12. 'l'ennination. Either Part y may t erminate t hi s SChedule upon six months written notice to the other Party.

13. Obi ectives. The ob j ectives uf t hif:! Schedllle a r e stated i n t he Basis and Scope clauses of the BAA and are intended to enf:!ure thal Lhe maximum p r act i cal credit i$ given to the expor t i ng Stat e's cer tification syst em and t o ensure Lha t ;

1 30 . Des i gn a pproval. The p t ocedure $ for th'" ,1.pprclVCil 0 1' the t ype des i gn o f a product, i:\nd dklllges t o the Lype des i g n o f a p -.;oduct., e stCibl ish compliance with the appl icable a irwor·thines8 s t andar ds o f t he i.mport i ng State civil airworthi ness authority (importiu,J a u t hori t y), or c r i t eri a de t e rmined by the importing Ciuthority to provide a l evel of safety equivalent t o i t s own. Under the present BAA, design approval is limited to civil aeronautical products for which the FAA is the basic type certificating authority.

1 3 1 . Produc t airworthiness certificatiQIl . The procedures for aiICwor t hiness cert if1cati on of a. produc t t o fac i l itate acceptance by the impor ting a uthori t y e s tab l ish that t he p roduct conf o r ms t o the import ing authori ty's approved type des i gn and is i n i:\ cOI1(.1it ion f o r saf e ope t"atl.on.

132. My t uiil cooperation und technical assistance . 'l'he procedures enabl e the FAA and the DGAC to exchange appropriat e i n f ormation needed to understand and conduct t he appr ova l and IlIOnitoring processes within the scope of the BAA and to cooperate when techni cal assi stance is needed by e ithe r a i.rwor th i ness aut hority i n f ul f illing its national a i rworthiness regulat ory duties.

133. Accountab i l ity. The procedures enable t he p e1:'8u"8 responsibl e tor a product 's d e s i gn i ntegri ty and mCillllfact.nring

quality a~suranr.e/conr.rol, <l.nd the airworthiness authority having jtl1:-isdicUon over th~se acUvtt:ies, to be identified fot the p :n.x.1u<:ts impurted, and establish that adeguat~ t e dmical capability is available to <l.~~ure that ~afety issues which may ar:ise with r ega rd to the product in setvice will be satil:1fa<:tor ily rel:1ulved in a t imely manner'.

1.34. Specipl art;;tngements. The pr.ocedures pr.ovide for the r-esulutiun by the FM and the OGAC by special arrangement, as necessary, o t urgent or unique situations not envisaged in this Schedul e, ptoviding the situat ion fallS within the scope and pUICpuse o f the llilA.

~4. Def.i.ni t ions. The defini tions i n Sect i on 4 o f the BAA aICe inco:qJoICated by ICefeICence in this Schedule. AS used in this Schedule, t_lle following definition!l are provided to supplement those definitions.

(a) Compli.ance means that, after examination by analysis, test, etc., the type design of a pr-oduct is found to !l<l.tisfy the notified <l.irworthiness criteria.

(b) Component means a part, material , or subassembly intended for use on <l.n aeron<l.utic<l.l product.

(c) Conf o rnu.tv means that a pICoduct is examined aga inst pertinent type design, test, <l.nd Tlality control data and is found tu me",t those data.

(d) ~orting Civ il Ai rworthiness Authority mG!ans the national ur-~j"aIliz"tiQn within the exporting State, charged by the laws of the exporting State with ICegulating the airworthiness cert ification, approval , or acceptance of aeronautical products. The exporting civil airwOICthineS8 authurity will be referred to herein <l.S the exporting authority.

(e) Equivalent Saf ety l'indin!J means a determination that a l ternative action t<l.ken provides <l. level of safety equ<l.l to that provided by th", requir",ments for which equivalency is being sought.

(f) Exempti on means acceptable !lonCQmpliance with a r.equirement when processed through the appropriate regulatory procedure by the airworthiess authority and found to be i n the public interest and not to have an adveICse effect on safety.

(g) Familiarizat i on means the process whereby t he i mporting authority obtains information and experience on an aeronautical pl;"oduct designed in the export i ng State in order to : prescribe <ldditional technical conditions for that pro<lucL; provide corrective a i.rworthiness action in the event that the pICoduct experiences service difficulties during its operation in

t_he imporl-in~ State; and dev f:' l"p appr"priate maintenance, "pe,,"e<t in'1, and pilo t type rat i ng inf ormat ion for the product ..

(h) Fi mliny means the re",ul t of a revJ.ew, invel;;ti(le<tion , inspection , test, analysis, etc . , to d"'t.<"rmi ne compliance of ,1. design with a .l aw, r egulat i on, standard, or r equi remenl, or <:"nf "nni ty "f e< product with approved type design data.

Ii) I mport ing Ci vil Airw"rthiness Authority means the national organization within thc import i ng 8t<1.t.<", charged by t be l<J.ws of th'" import.ing Stat_e witb regu l a t ing llle a i rwort hillf:'SS cert ificat ion, e<PPl'-"ve<l, "r acceptance of civil aeronautical. products . The importing civil ai r wortbiness author i t y wi ll be refe r r ed t o he re i n as the import in" auth"rity,

(j) M<.2llli.t:Q.'J;.lLm~ m<",",-ns the person r esponsible f o r t he f1.nal assembly o[ a product undet a <.:iv il ail'"Worthiness author-ity-approved qual ity assurance:: system which e::ns\lres conformity of the product_ to an a pproved type design and its cond ition f or sa f e operation.

Ik, whi ch i s only

Non~t<lndard category aircraft means an a ircrafL e l igibl e for a sp!:.'cial e<ir"Wor-thin",ss certificate .

(1) Per §on meilns ,",-ny i ndivi d llal , f i r m, copartnershi p, corporat ion , company , association, joint stock association, or body pol itic, and includes any trustce, receiver, assignee, or other similar r epr esentat i ve thereof ,

(m) Pri ority par ts means thoso parts whose filiinre could r easonabl y be expected to r esult in t he calasLrophic failure a f the product in which they are installed.

(nl Quality assurance (includiu<I quality cantrall means a systematic process which providcs confidonce th,1.t aerm"41.utical p r oducts wi ll conform to the appr oved t ype design and wil l be ill e< condition for safe operation.

(0 ) Specicll Condi.t J on means a specif ic safeLy s t andard issued by an e<itWOl'-tlli"",ss authority for a product when , because o f a novel o r unusual. design reature of the product, the establi shed aj,rwor th i ness standards do not conta i n adequate or apprapri at", saf",ty ste<udards to establish a l",vel of safety oquivil l ent to t~.t estilblishod by the airworthiness standilrds.

(p) Standard Category Airworthiness Certification means the issua nce of a standard ca t egory a i rworthi ness certificate for a i rcraft type certificated ill ttl", rlonre\l, uti l ity , ,1.Crobiltic, commutor , or transport categorie s.

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(q( component to a nunutacturcr's

"',~m::e:a:n~:",:':u:;::'~~ who contract,; to provide a , to be incorporated into the

aeronautir:al product.

(r) Type Design means the description of all charac teristics of a prodUct, including its design, m;lnl1f<lc:tu'~e, limitations, and continued airwort hiness ins t ruclions which Getenaine its ailC'Worthiness.

The f o ll owing de fini tion a l so appears in the BAA and is repeated here for the benefit of the uSer.

(8) me",ps the certific"-tioIl, approval , or airworthiness authority at t he des i gn of a p r oduct i;"i~:;;;~,; ~:::perf ormance, ope r-at i ng characteristics, ope:r;-ating , and enviJ;onrnental qualities.

CHAPTER 2. PRopue!' TYPE DESIGN APPROVAL PROCEDURES.

20. General. In accordance with the scope of the current BAA, the information in this chapter is applicable to U.S. type design approvals consistent with the limitations stated in the BAA. Approval of t he type design of a produc t , or changes t o the type design of a product, by the importing authority shall be based, to the maxi mum extent practicabl e, on technical evaluations, tests, illspections, anu compliallce c"'t-tificatiolls made by the exporting authority . The appropriate form of design appr oval is to be i ssued by the i mporting author ity for an imported product if U te exporting authority, aftet' consultation with the importing authority, certifies to the importing authority that the product type des i gn has been exami ned, tested, inspected, and found to meet the airworthiness crit"':t:-ia prescribed by the importing ;mthority, which the importing authority has found t o be equivalent t o its own national airworthiness standards for a similar product.

21. 'lYpe Design Approval APplication Consideratiolls.

210. Un ited S t a t es. An FAA t ype design approval f or a product is a prerequisite:

(a) For issuance of a U.S. airwort hiness certificate;

(b) To permit a non·U.S.-registered aircraf t to be ope~ated unde r lease hy a U.S. · certificated ai~ carrier or commercial upe rator under Federal Aviation Regulat i ons (FAR) Parts 121 or 135; or

(c) To pe:t:lnit a :(C"elateu produCl (e .g., e ng i ne, appl iances) to be installed on an aircraft having a U.S.

airworthiness certific~te.

'1'11,:, J/IV\. will assign a higher priority to applications for type design approval o f Ltn import product when one of t he ;lhove si.tuations i s shown to exi st. The FAA does nOL gene rally grdll t typf:' df:'sign approvals for products manufactured outside the U.S . which are not i ntended for U.S. utilization, except for products LO be insLal led on U . S. -manufactured pI'oducts. '1'IIf:'rf:'[ore , IH,lIl' U.S. appl i cants tor design approval shoul d provide the FAA with evidence of i ntended U.S . ut.i li zation or installation on a U.S . ' mam\fact ured producl al t he t ime of application.

::! 11.. ReplJblic of I nOonesia . A DGAC t ype des ign approval for a product is a prerequisite:

(a) For issuance of an ROI airworthi ness c f:'rti f icatf:';

(b) To permit a non-ROI-reg i stered a ircraft to be opf:'r;-ated under lease by an ROI'certificated air carrier or commercial operator under Civil Aviation S~fety Regulations (CASR) Pa rts 40 o r 42; or

(c) To permit a related product (e.g . , engine, appl i ances) to be i nstal led on an a irc r a ft having an ROI airworthiness c eI"tificatf:'.

The DGAC wi ll ass i gn a higher pri ority t o applications f or t .ype design apPI"oval of an import product when OIle of the above situations is shown to exist . The DGAC docs not generally grant t ype design approvals for products manufactured outside ROI which are not intended for ROI utilization, except f or products to be insta lled on ROI -manufactu red products. Therefore, non-ROJ applicants for design approval should provide the DGl\.C with evidence of intended ROI utilization or installation on an ROI ­manufactured product a t the time of appl i cation.

n.

type design of f t, a j . engines , ;1Od propellers. The following

such product type des i gns t o be type by the DGAC for standard category

enginer> and PI"O~P,;,;l:,jL,"<i,~;,[jo;c;n:nonstandard category aircI"aft, will b e dealt with on a case - by · case basis through the spec ial aI"rangement provisions of th i s document.

220. ADo1 l cation. An applicant for type design approval shall make appli<:at ion through ilS own a i rwor t hiness authority with a reTlcst that the application and related infOI1na t ioIl l.Jf:' forwarded to the import i ng author ity. Al l ROI

ilpplicati,ons for I'lVI. type des i gn appr oval shall be senl by lhe DGAC t() t he Aircraft CertificatioIl Office (.1\(.'0 ), Long Beach, California. All U . S. applications for ROI type design approva l .'<hall b", ",,,,n t to lhe FAA ACO i n the applicant's geographical area, and the FAll. ACO will forwaI"d the application to the DGAC. Applications should include a generill description of the prOd1.1ct including :

(a) A three·view drilwing for ilircraft or a Cr08S ­section dr.awing for. engJnes and propellers;

(h) A stil.tement of the applicable airworthiness and environmental standar'ds f()r' design approval as established by the exporting authority for its own domestic design approv::ll;

(c) Any Bovel or uIl.utjual design featuI"es known to the applicant at the time ot application which might necossitate j ssuance of either FAA or: DGAC a ir:woJ:"thiness speci a l conditions;

(d) Any expected exemptions or eTlivalent safety f indings rela t ive to t he exporting authority's airworthiness standards for type design approval; and

(e) The estimated date of completion.

221. I nitial familiar i ",at ion b q efincr. On major projects, as soon as practicable after' the application has been received and accepted by the importing authority, and when the design is suffi c i ently de fi ned, a f amilia. riza.t i on briefing on the product may be requested by the importing autho1:·ity. The briefing shal l be held tlt a mutually agreeable location for attendance by t he importing authority, the exporting authori t y, and the appl icant. The primary purposes of the briefing will be to permit:

(a) The applicant to describe the design to the impOJ:"ting authority. This briefing (or series of brief i ngs) shall cover all aspects of the delSigu. Emphasis should be placed on any novel, unusual, or critical design features which might necessitate issuance o f e ither importing authority or exporting authority special conditions or new appl ications of existing standaT.ds;

(b) The importing authority to engage in detailed technical discussions with the exporting authority and the applicant on the design, including particular applications or interp r etat ions o f the airworthiness standilrds of the exporting State and the i mporting State; aud

(c) For products wi th a prior service histor y. the ctppl icant and the exporting authority to brie f t l1e iropo r- ting authori ty UIl th", p ruuuct service his t<.ay, including ~' orT",ctive measures to precl ude occurr ence of incidents or accidents.

(".j 'l 'h", import in,:! authority shall ",stablish a type certification basis for the product design in accord,mce with its own domestic a irwo rth i ness standa r-ds f o r a s i mil a r prouuc t, 'Jivi wJ CQns id",ratiOIl to the standards wbich wer e in effect in the importing St.1.t.e at tl1e time thClt ctpplicCltion was received for the approval of the produc t t yp O:' de ",igIl by t il", "'xporting authority.

(b) Once the i mporting author i t y's L.ype cer-tificatioIl basis has been established, the airworthiness standards for type certification hy the importing authority Sh,1.11 be agreed jointly by the importing au t hori t y and expor ting authority so as to:

(i) Give maxi mum credit to t he export-ing a.uthOlCity's dumestic cert if ication system; and

(ii) Prov i de t he importing au tho rity a baS is to find compl i ance with its own national airworthiness sta.ndards or to find t.ha t. equivalent crit.eri" l1ave been met, h,1.>'led nn an e xport ing authori t y cert ification of compl iance wi th the agrO:'eu a irworthiness standards.

(c ) Thus, the air-wo rthiness standar'ds uef ined by the import. i ng ".ut.hority will c onsist 01' the airworthiness s tandards as a ppl ied by the exporting aut hority under its own domestic certification system, p lus any additional technical conditions speci fi ed by t.he importing aut.hority to est ablish an equivalent level of sa fet y with i t s own domes ti c standards f o r a similar produc t .

223 . Additional t echni cal condi t i ons. The additional technical condi t i ons nay inc l ude any or all of the fol lowing:

(a ) Addi tional a irworthiness condit J.ol1s b ased on differences in the basic airworthiness standards, inter.pr e t ations, applications, policies, and guidance m.:l.terials between t he two States . I n the case of t he U. S., t he bas i c a irworthinRSS staML1.rds arc set out in the FAR Parts 23 through 35. In th", case of ROI , the basic airworthi ness standa r ds are set out in the CASR Part s S, 6, and 8 .

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(b) Spooial Conditions r8lating to novel or unu."l\lal f<,at_\l res of the p r.oduct des i gn which are not covered by Lhe a.irwor Lh.iness sti:u,dan% o f t he <:,xporting authority;

(c) Airwort hiness condi t_i ons based On an evaluation of equivalent safet y findings and <:'xempt ioIlS "ranted by the exporting authority to th8 appl icant tor domestic oert i f i ca t ion;

(d) At the option ot tho applicant. operation;:tl r equirements o f t he i mport i ng authority f or a pa rti cul ar k i nd or oondition of operation which would affect the design or perfm:mance of t_h e product . Thi>'! could inClude the p rovi si.on of addi t ional equipment required to mee t t he operat ional requirements of the importing authority, as well as supplementary adv isory inform."lti.on in the aircraft fli.ght ITk"lnual; the provifl i on of an aircra ft operating manual wi t h procedures for t he dispatch at the aircraf t with inoperative equipment; and the provision by the export i.ng author.i ty of advi sor.y maintenance i nformation . This latter infonnation will ass i st an airc:c:lft op~rator in satisfying the importing authority that hc has an acceptable maintenance spec if icat i on f o r h i s a irc r aft operat i on; and

(e) Act_ions deemed necessary for conti nued safe operation in t he import ing S t a t e as a resul t o f t he .impor t ing authority review of the service history and the actions taken by the exporting author i ty to correct. unsafe conditions on products of a type d<:,~ign previously certificate d by the export ing authority and having accumul ated a measurable service history.

221. Data submi t t a l and de s i gn r e v i ew . Requ i r ed technical data representing the product will vary with the type and complexity o f t he p r oduct i nvol ved. Preceding the i ssuance of type certification. the importing autho:r;-ity may request additional t eChnical design data, may review the product, and may fly the p r oduct for fami lia ri za tion pur poses. Also, wIlen deemed necessary by both the exporting authority and Un" import i ng author ity, the importing ;:mthority rn."ly fly, or conduct a detailed review of, the p roduct to assure compliance wi t h t he addi t ional technical conditions . The appl icant shal l submit a l l data to the exporting authori ty f or verificat i on and transmi ssion to t he importing authority. Requests for additional technical data, reviews. and fli.ght tests as described here shal l , in the spiri t of t he BAA, be t he mini mum necessary t o assure t hat t he i mporting authority acquires the needed familiarity.

22 5 . Technical !!!!;!etin<ls. I n a ddi t ion t o t he i n it ial familiar i za t ion briefing, othcr technical meetings may be necessary LO assure tha t any addit i ona l technical cond i t i ons t hat_ have been communicated to the exporting authority a n" wel l under stood. and t l1at ilny Qut>'!tanding technical issues arc resolved. All t edmical mee t ings will normally be a r ranged

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Lhrough the export i ng auttlorily . LocaLion of the meetJ.ngs may vary, depending on the needs and pri orities, and will nOl~l ly h.1.v", import i ng aut.ho r i ty/export.ing ,1.uthori t.¥ represent atives in attendance. Sudl meeti""S (and guidelines fo r the mee l;:ings) may include:

(a) Technica l meetings requested by Lhe appiicant, the exporting a u thority, or the import i ng authori ty f or the pU T: pose o f l~epo:r;ting new deve lopment.s, rev iewing r:h'l.l1ge8, or resolvin(J technical compliance questions;

Ib) Technical meetings between the importing authority and exportiIl!1 authority to effect the t ime ly resolut ion of cllltstanding issues;

(c) Teclmical rueetin,,::; held with t he applican t t o provide the applicant with the import ing authority's position with r espect t o a ny unresolved t.echnical issues; and

(d) Teehnical meetings involving flight operati ons and ma intenance specia lists of t.he importing authori ty, exporting authority , and the applicant t o facil itate operational acceptance of the product by the importing authority f o r a part icular kind or cond i t i on of operation .

226 . l 11JllliLll ill1Q.r.ll. . Isslle papers may be prepared by the import ing aUlhority which descr ibe issues , such as Addi.t i ona l Technica l Conditions, which need to be resolved b",fore th", i mporting authori.ty can grant a TC or hefore an ilircraf t can enter a special type of operation, such as commer c i al oper at i on, in the importing authority's country. The exact form and scop'" of the i ssue papers will be determined by each Ciirworthiness authority and details of th", ir use will be p rovided to the othe r a irwor thi nes!'l authority .

227. lWproyal of chang"'!;) to a t ype certificate.

(a) Appr oval o f changes to the t.ype design (e.g ., model changes) sought by ttl'" type certifica te holder shall be is sued as amendments to the TC by the importing authority . A c",rtificat ion procedur e s i mil a r to that descrihed in Section 22 shal l be appl ied , but adjusted as appropri ate for t he magni tude and complexi ty o f t.he design change . Thc importing authority retains tll", ricJht to determine if the p r oposed change is of such significance as to require a new type certificate for the changed t y pe design, based on how the change would he dealt with for a similar product and circumstances in the import ing State .

(b) Cha nges or produc ti on design i mprovements nt.her thCin those to be dealt with under Sectiou 22"1(a), such as changes introduced by service bulletins, shal l be considered approved by the import ing authority upon approval by the

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exporting Llathor; ty under it.s norm,ll pro<'edllres; provided i nformation on t he changes i s suppl ied LO the import i ng authori t y by the export i ng authority. Upon requeE't, the export i ng <luthority shall ,lrrange to hLl.ve service bulletins reflflcting changes provided LO t he import i ng a llthority all a timely basi" .

23. 2l!Pplf'rnf'ntal TyPof' Certl.ficatf'!'I.

(a ) Both the FAA and the DGAC may issue supplemental type cert.ificates (STC) to grant approva l for changes to a type des i gn for which a type certificate has been prev iuu"ly granted. The importing authority shail consider approving a change in type design on a product made by a n appl i cant i n the export ing State, provided the product b«s been type certificated by both the FAA and the OCAC for standard category <lirworthiness certific,,-tion.

(b) lI.pplic«tion for S'.l'C relating to products certificated in nonstandard catcgories and design <lpprov,,-ls for f i eld modi fication authorized under FAA field approval procedures (FAA Form ACA-337) shall be dealt with on a case-by · case basis, simi l ar to type certificates of nonstandard category.

230. Application for STC . An applicant shal l submit STC appl i cations to the exportj.ng authority wjth a r equest that the application and related information be fOLwarded to the import ing ,,-uthority. E,,-ch <lpplication will provide the following i n f ormati on:

(;:t) Description of the change , together with the make and model of the product;

(h) Copy of exporting authority approval document and cert iLi.cat i on basis ; and

(c) I nformation on any equivalent safety find i ngs or exelnptiunt; "ranted by th"" exporting authority for the domestic STC .

231. Establishment o f appl i cabl e airworthiness cr i teri a. The approval bas i s for ,,-n STC shall nonn.lly be the ai:n.orthiness standards originally established by t he importing authority for TC approval of the basic product . Additional techni ca l cond i t i ons may be prescribed by the importing authority when the circumstances of the design chan~le make them necessary.

232 . Basic document a tion. wil l , under no=l circumstances, be import ing aut hori t y:

The following documentat i on required for rev iew by the

(a) Compl i,,-nce Checklist .

(b ) Aircraft Fl ight Manual Supplement.

Liost. tel Master Dom)ment~tion List/MatSter Drnwing

(dj Manu(acturing a nd Install;).t:ion IutStruction Dr "will!lS .

(e) Maint enance/Repair Manual Supplements, et,C.

( t ) In1Jt r UCliOlls t or ConL.iuued Airworth i uells .

233 . Addi t i ona l doC\)m"ntat ion t o r comul ex STC ' f!. Where the techn ical compl~ity or t}le de s ign cha n'le warrants, e.g ., where addi tional technica l cond itions are required, it may he necessary to provide additional d~ta , such a s:

(n ) l1n~! ineering Reports: Structural analY!li s , e lC.

(hj Flight Test Da ta.

23>l . r ev i.ew t he STC authori t y' fI importing 10'111 a uthority cond i t i ons . c onditions wil l request from the possibil ity that complex STe'S , will a s flight r.e81., etc.

'1'l1 e i lupo rting au thority will with t he export i ng

certification bas is. The conr.ur with the exporting

o r propos e ;).ddiLional teCh nical <l g,1 i ns t t hese technical

be by the exporting a uthor ity upon authority. This will not preclude lile . authority, for familiari~ation on

t o perfoun additional eva l uations, ~ul':h

21.. ~ign Approval s Of ProducL!! Other Than Ai rcratt , Aircraft Eng ines, a nd l'rorellera. The PAA issues a lotter of '1'90 design a pproval for ilppliances of a kind [or wnich a performance s tandar d has been publ i shed in a n FAA 'l'echn i c;).l SLandard Orde r ('1'SO). The OOAC is sues a let t er of TSO design approval for a ppliance s of a k i nd for wh i ch a perfor.mance standard has been published in a OOAC Technical Standard Order ('1'SO) . Appr oval of sueh appliances may be a ccomplished by corre spondence between the FAA and the DCAC. The a pprop ria t e form o f d esign approval may be i Bosued to the a ppl i cant by the i mp ort ing a uthority af ter:

(3.) Rece ipt of a statemenL from t he applicant through the exporting aut hority, with conf irmation by tll!! exporting nuthorit y , t ha t t h e de8 i gn and p e r formance of the a pp lia nce or articl e comply with the appl jcable TSO or ot.her accep t ed s tandllrds ; alld

(b) Re ceipt o f a ll the required da ta pert a ining to th@ proper i n., tal lation, perro rmance , operation, and m.1. i n tenan(;e o f the appl i a n ce,

11

CHAP'l'ER 3. PROpUCT AJ]?WOR'fHINEBS CF:RTlFT(",A'l'ION OR ACCBPTANCE.

30. Productign Ol.!.iil.ity Assuc<l.Uce Byst@rn AQprovals for £.!:oduct.s M<lnufactureY in Bitber the 0 . :;> . or ROI . AU prodUL'tfl tndnntactnreY in either the U. s. or ROt alld exported under the provisioIls of the EAA shall be manufactured in accor-dance .. i th a production quali t y asaurance system acceptable tu the exporting aUlhoriLy, .. hjch assures cunformity to the type design approved by the importing autho:dty <lnd ensures that completed products are ill 11 condition for Gafe operation . Therer.ore, a separaLe approval o f t he manufac turer 's production qual ity assurance syotem by the importing authority is 1I0t ~ired, a lthough it is consisLent .... ith the inteut of the BAA that the ilIlPorting ;lU thority may become familiar .. ith the manufacturer ' ", proouClion quality aSS\lraocc s ystem.

31. airworthineSS Certific<tt:ioll or Aqeet/tance of ProductR.

310. !:2rrtQlete aircraft manufac tured in the U,S, or ROI. The i mportin9 authority shall accept the certifj,cation or the I:'xporting authority on the air .... orthinel;s of <t n aircraft ill m.:lking its finaing that the aircraft is eligible for 31l airworthiness certificate. The certification by the eXporting authority ~hall altCGt that the Clircra f t:

(d) Confo~ to a type design approved by the importing authori ty, Which meets the importing authority's standards for airworthiness , as specified in the importing <tuthority's type certific.lte data sheet ;

(b) 11:1 in a condition for safe operation, i ncluding compliance .... i th applicablo importing allUw rity mandatory airwort hineas modifications and special inl;pections; =d

(e) Contains equipment .. llich enoures compliance with the importing authority's operatlonal requirements all notified by the importiug lluthori t y.

311.

on '::;;,:::~~i't jmport~ng the exporting makes a

conf i gura t ion:~'::~:i:~r~ installation safe operll tion.

coufm:ms to a type des ign the aut.hority for of and is in a condition for

with any applicablc special i nspectiono, and

the importing author;ity. mandatory airworthiness ~pecial requirements of

312 . pevi utions from the importing authority type <1£.3)..gn. Any dev i at i ons from the importing authority t.ype design shall be noted by the exporting authority on the certifying statement. Any such deviations shal l be resolved by the app1ir."nt. / installer before;;m Clircraft is e lig i ble for", U.S. 01" ROI airworthiness cert ificate, or a :"",,,lated p:r;'Qduct i8 eli<jib1e for installation on an aircrart having a U.S. or ROI ait"wot"thineS8 cet"tjii.cate.

313. Aircratt. aircraft engines . or propellero manvfactured in a third State. I n making its f i nd ing of eli~libility for an airwo:r;thiness certificate or approval for eHi aircraft, engine, or propeller manufactured in a third State, the importing authority shall accept the ce rtifi cation of the exporting authori ty as to the airworthiness of that aircraft, engine, or propeller , providing the exporting authority rn."lKeS .J.

certifi cation to the impot"ting authority gi.mi l a); to that I"equ :\);ed in Sections 310 or 312, as appropriate, and further providin~·l tmt,

(a) Eoth the FAA and the DGJ\C have approved the busie type design of the uircraft, uircruft engine, or propeller, as appropriate; and

(b) In the cuse of un aircraft, the aircraft TIonn.ally would have been regis t ered and certificated in the exporting authority State, or had been in the exporting State for the purpose of complet_ioll; e.g. , int.erior installation.

32. Special Requirements for Products. The following identifies those spec i al tequirements wh ich m\lst be complied with as a condition of accepteUlce of products imported into the U . S. or ROI, or for use on U.S . /ROI-rcgistercd aircraft .

320. U,S. special requirements.

(a) IdentHic<ltion <lnd marking.

(i) Aircraft, aircraft engines, and propellers mus t be identified in a manner outl ined in FAR Section 45.11 with the information outlined in FAA Section 4 5 .13 .

(ii) Criti cal components as defined in FAR Section 45.14 to be used as spare or replacement/modification parts must be l denti fi ed with a part numher und seriul number.

(iii) Appliunces and articles of a design approved by an FAA let ter o f TSO des i gn approva l must be nnrked in accordance with the requirements outlined ill Part 21 , SubparL 0, a nd <lny additioni"ll m"rking requirements specified in the particula:L- TSO.

(1v) P!l.ct.rl a nd matcri!l.ls t o be u8erl ;:'I E Ilparf'l or replacemeflL/modificatiOD parts must be idenU fied by il part numb!!!: a nd the manufacturer's name or trade mark. Tn addi t:lon , information concerning th!! model desi.gnat iun 01: the Lype cert-ificated product Cor which the pa rt- is c lig Jb1e for inst alla tion mus t he furn iflhed,

(b) Ma intenance rpcordli!, The prOOllcts must be accompanie"- by maintenance recordlil equiv«lent t o t hoa e cpec ififlci ill FAR Seceion 91,173 that r e flect the s tatus <'ll' require"­inslJt:!ctions, life limits , e tc,

(c) Operatiopa l check, In the case of ~ircraC t eng ines or pr'opellers, t he air"craft engi ne o r prope ller must hay!! been subjected to a final operational check to the manufacturer 'c specificatioMl "

321 . EOI specia l requirements.

(a ) Identification and mar~inq

(i) Aircraft, a i rcraft enginco, and propellers must. be identified ill a manner Olltl ined i n the CASR .. a.rt 1 .

(ii) Cr.iti cal components as derined in the CASR to be used as spare or replacement./modi tj C<ltion parts mus t be identified with a part number and seri a l number.

(iii) J\ppl i <lncel:! an"- articles of a desig a <lpproved by an DGAC l etter of TSO l1c sign approval must be l'Mrked i n accordance with t.he requir ement. s outlined in CASR Part 6, Subpart Y, and <my additiona l marking requirements specified in the particular TSO.

(iv) Parts and mate rial s to be used as spare o r r eplacement/modif i cat i on parts must be identifj ed by a. part number and the manufacturer' 8 name or tra de marie I II addit ion , information con cerning tho model rtec igna tion or the t ype certificated p r oduct t o r whiCh the part i s eligibl e for i nf:! Lallation must be furnislled.

(b) Mwinteoance records . The products must be accompanied by maintenance records e quiva lent to those spe cified i n CASR Part 18 t hat reCl ect the status of required inspections , liCe l i mi tf:! , et c,

(cJ Qpcra tion,l l c heCk , I n the case o f a iI,craft engines or prepe llers, the airc ratt engine or p ropel ler must h(lve been Subject ed to a final operat i onal check to the manufacturer' Iii flpecificatiollS "

33. hs in Section 'Olaf thi", lOchedulc, of the S t ate i n .... hich a product manufact.ure r i s l ocated may reque.,t c<.mformity cerlificat e., of the airworthiness authority in the State in which the product manufClcturer's suppl ier i " l ()cated for spec if ied components produced by lhal supplier.

330. RfLqu!"st for r.(lnfonnitv cf' rtifica liolls. Requests for such certi f i ca tiolls .... ou1d be considered appropriate when:

ICl) Th!" product manufac t u rer has dev e loped and implement ed qual il y cOlltI'ol procedures acceptable to the product manufacturer's airworthiness authority to !"nsure that. the supplicr furni"herl components wi l l meet. t he pert iIlt:"Ilt desigJl data and be i n a condi t ion tor safe operat i on. This would include provisions for the product manufctcturer to m..ke iniUa l on-s ite !'Illpplier capab i.1 ity evaluati olls, ( i r st a rt icle inspections, and perform any suusequent audits, source inspections, etc ., ctt the supplier f acil i ty, as ncccssary, to ~.k8 th8 final airworth j ness det.ermi nat;i,on .

(h) The product m.J.nufacturer's airwort hi.ness ctuthority · · not t.he p r oduct manu f acturer · · makes t ilt:" request for conformi t y cert ification., .... hen the airworthiness authority tinds such certification!) necessary to enSl1r8 th,J.t th!" product manufacturer is demonstrat i ng adequat e contI'ol v( the paIt i cul ar supplie,.;· .

Ie) The produc t manufac t urer's aiI'WoI·thiness autho,.;'ity notifies to the supplier's airworthiness authority t h!" design , test:, ctnd C]ll,J.lity control requ i rements to wh i ch the component muS l conform.

33 1 . Compon!'nt. giltegori e s. Reques t s ( or COllfOLnlity cert ifications should ue limited to components that are of such complexity that they arc not inspectClhle hy t.he product m..nllfa.cture >:e p r j,or to i nsta lla tion in tile final product and fall int o ont:" ot the following categories :

(a) Protot ype components to be used for design !:'valuation purposes; e. g., type certification programs.

(b) Pre· production components, i . e., components to be used in a completed product submitted for airworthiness certificat.ion or approvil l after. a type certificate has been issued but befo~e p~oduction privileges have been granted .

(c) Firs t article inspections on production components whi ch tall into a priority part category.

Id) J>r<.xluction components, when feedback to the product manufact urer's airworthiness authority rcvcctls Cl s tlfet.y

15

probl em.

332. Deviations . The suppl ier's a i rworth i ne ss authority will not.e any deviations from the reqnirem<"nt;; noti f i ed by the produc t manu( a ct uL"er'S a i rwor t hiness au t hori ly on the conformity cert i fication for the particular component.

333 . Airworth i n e ss de t e rminat ions. The conformi t y certification i ssued by the supplier's airworthiness authority should nat b<" misconstrued al1 being an export. airwort h i ness approval, since t hey do not constitute a n "i:n'orthiness determi nat ion. such determinations remain the responsibi l ity of the product manu f acturer and its a i rworthiness a u thority. The certifications only serve to "ttest to the product manufacturer's air worthiness au t hority that a component confo rms t o the design, t es t , and qua li.t y cont.rol r equ i.rements wh i Ch t hat a irwort.h iness a u t hori t y has not i f i e d t o t hO:' su!,>pliO:'L" s "iL"Worthiness authori ty. Accordingly. when a product manufacturer desires to ship a componen t d irectly to an operator/user , it must make the necessary airwor thiness determination. In these instances, any necessary export airworthiness approv als must he issued hy the produc t manu f ac turer's airworthiness aut hority or its designe e. The onl y condition under which the suppl i er's airworthiness author ity cou l d issue a n expor t a i rwor thi ness approva l f o r such components would be where the supplier obtains its own production approval for t he part icular component s from the supplier's a i L"Wor t hiness aut hori t y.

CHAPTER 4. ACCOUNTABILITY .

40. Ge neral. Each airworthiness authority has r8sponsihility to the other to assure hath design or manufac t urin<J de ficiencies are correct e d as specif ied i n t his chapter on products whi ch were imported or exported under the BAA and whic h h ave current TC's o r production approval s iflsued by t ha t airwoL-thiness "uthority to " person located in its S t ate. When a pcrson in the Contracting State holds onl y design or manu f act u ring r espon s i b il ity, t hat a i rwor th i ness authority's respons i bil ity under this chapter is equal l y limited. These respon;; ihi l it i efl include:

410. communication. The need for FAA/DGAe dialogue t o assu re tha t t he same or cons istent informat i on and re~lirem8nts a r e issued on a g i ven product;

411. Notifi cation of uusaf e couditions. Wheu the servicc expericnce in the importing Statc indicates the existence o f an unsafe condit i on associ ated wj th the des i gn, manufac t u r e, or mai ntenance of a p r oduct, such infoLm:ttiol1 shoul d prompt ly be provi ded to the exporting authority. When such inf ormation is so pr ovided, the exporting authority shoul d give e x pe d ient a tten ti on t o thc information and cons i der appropriate actio ll to c orre ct the

,",ond1t: i on.

412 . AQgjd8nt: /-incident i nvestigation assist~ . When a n impor-t i ng ao thoriLy ne",ds a irworthiness informat ion f or Lhe iIlvesti"atioIl uf service incidents Ol:: a cc i dents invol ving a product impor ted und8r the BAA , the request for the i nform;J. tion should b e direcLed t o t h", a ppropriate e xport ing aut horily o f fice. In tUl::n, upon l::eceipt 01 the l::equest for infonnati on, the exporting ;:mt:hority ",hOllld immediatel y d o everyt:hing necessary t.o make sure the r equested i nformation is provided in a t i mely manner. I f ul::gency l::equi l::es that the importing authol::ity l::equest t:he inform.1. t ion di l::ect:ly fl::om the man\lfact\lrer, the importing a u t hori t y shal l i nuuediatel y info n n t he l::esponsible e xpor t i ng au thority of ti ce of t his action .

413. Mi:t!uid t Ql;Y airwu.thim:ss ac t iuIls. I n the Cds e of mandatory a irworthiness actions, each airworthiness authority sha l l keep the other- fol l y infor-med in a t i mely manner. Of a ll lnamja tory airwozc·thill<:'SS modiEic«tioIls a lld speci«l inspectiuns which are dctermincd to bc necessary an products designed or mal1ll f actu r ed j,n ei.ther. Sta t e. The issu i ng a irwo. thjness «uthurity shall id",ntify th<:' ~«fety p r obl",m (unsaf", condi t ion) rcquiring the mandatary airworthiness action . A standard not if ication system sha ll be establ i shed which will assure t ha t al l such «c t i un!> «re promptly not if ied to t h e other ai~'worthiness authority . In thc casc of emcrgency airworthiness information, Lhe issu i ng air worthi nes s authority should ensure speci a l handling so that the othel:: airworthines~ authol:: i ty is notified immedi<l t.ely <)nd can t,1.ke appropriate parallel action within the constrain t s of t he orig i nal act i on . Unless d i ffering opera t i ona l conditi ons obviate the need, t he othel:: airworthiness authol::ity Shall i.ssue e xpedient and consist:ent mandatory airworthiness inforrnat iorl to operators of the product in i ts country .

CHAPTER 5. MUJ]JAT, COOPRRATI0 N AND TECHNICAL ASSISTANCE.

50. Communications and Meet ings. Applicants fOl:: product t ype des i gn appr oval f r equentl y r.equest teChni c a l meet_ings or cOl::l::espond dil::eetly with t he imp0l::ting «uthor ity to d iscuss and r.esol v e technic«l isslles that commonly arifle in t hC'! applicants' prO'j rams . Becaus", each a i rworthiness <wthori t y rel i es heavily on t he othel:: 's understanding of its position on SUell iSt;ue~, til", e xpor. t i ng authority shall be included in any such mect ings or eorresponde!).,",,,,. Also, each airwort hiness authori ty shall seek the other airworthincss authority's opinions before significant issues rega rding an appl i cant's pr.ogram are resolved and, accordingly, will genel::ally diseoul::age a meeting with the appl i cant to d i scuss a nd resolve technical issucs unlcss the o thel:: ail::worthinet;s authority is also invited . Si mila r l y, corn'lspondcnce will gencrally be answel::ed through, coordin«ted wilh, or copi e d to t_he exporti ng alJthori t.y.

51. reque>;t and mutua l agreement , one may perform t echnical evaluation to airworth l.ness authority in fur. t herance of t he purpo>;e>; and ub j ective>; of the BAA. S"cll an"a>; uf a>;>;i>; t allce may inc l ude, but arc not limi ted to wi tnessing tests, performing inspect ions , r evi ewing r eports, doing flight test s, and obt a i ning data .

52. Exchange of I nform1,tiQn on St andards and Certifi cat ion SYfltem."l. I t is recogn i ?ed t ha t a n essential factor in a smoothi y ope ra t ing BM i>; a thorough and up-to·date knowledge by the exporting authority 01' the regUlations, poJ i c i es, pract ices, a nd int.erpr eta U ons o f the i mpor t ing authority. Early efforts shoul d assure tl~t each airworthiness authority h~s in i ts possess i on a complete set at t he other ,.<irworth j.ness author il.y's wri t t ell regUla tions, g tl i danee, policie s, practices, and i nterpret ations, or have a source for such informat ion. Since such rf>gu l ;)t i ons, policies, practices, ,lIld i nterpre t a tions are cont inually under goi ng revi ew and revision, i t is imperative that the exporting authority's maxinrum practicahle i nvolvement in t he revi flw and revi si.on process be per mit Led and ellcouraged. Thi s should t a ke the form of earl y and direct notification of all comments resulting, and early notifi cation o f the t ext , impact, and e f fectiv e da t e of any adopted changes.

CHAPTER 6. .sPECIAL ARRANGRMRlITS. I t i s antic ipa ted that urg ent o r unique situa tion>; will develop··with respect to design, product airworthiness certification or <J. c c8p tance, or t echni cal ass i stanc8 ·· wh i ch have not been speci fically addressed in thi s Sclledule o f Implerm:'lltatiQIl PrQcedures, but which arc broadly covered in the BAA. When such a situat ion arises, i t shall b e revi ewed hy the respect i ve FAA and DGAC per sonnel , and a p r ocedure developed to deal with t h e situat i on. Confirmation of the procedure shal l be either by routine correspondence o r , if considered signi fi cant, by the signing of a Memorandum of Unders t anding . Part of the process ot reviewing the problem and preparing an a ppropriate procedure shall i nc l ude a determination of t he uni qu eness o f t he si t ua t ion. 1 1' it is apparent that the situat i on is unique, wi t h littl e possibility of repe t ition, then a t erminat ion date may, if appr opriale, be a tt ached to the cor respondence or Memor audum o f Understanding. However, if the s i tuati on has anticipat ed new technology or management dflvelopments wh i ch will l ead t o f ur t her repetition>;, then this Schedule of i mplementation Procedures shall be r evised and submitted for <J.pproval hy the FAA Admi n i s trator a nd t he DGAC Direct or General a t the next r eview meeting. I t shoul d be noted that , when the unique o r urgent situation f<J.lls wi t.hin the responsib i l ity of a n FAA Ai rc r a f l Cerl i f ication Directora te Manager , that Manager will be responsible for developing the np.ce ~ sary p r OCedures.

'l'his Sr;hedul", <.I f Impl ",ment « ti<.lIl approved by the u ndersigned.

Barry Lambert Harri s Il.dmi,n j,gtrator, FAA

Datr:.

Procedul:'e,; has b e en r ev i e wed and

\

.. ~

zainuddin Sikado Direr.tor General of Air Communi. ca c i. ons

Date

APPENDIX A

Li9t. of addresses Ear FAA Aircraft Certification Off ices and DGAC Airworthiness Reg i onal Off i ces.

1.0 FAA AIRCRAFT CERTIFICA~TON OFFICES

Brussels ACQ (AEU- 100) Addre,;,; ,,11 c()rre,;pondence to Manager, Airc~'aft

Certification Staff.

15 rue de 1a I--oi, (3rd III oar I B-l040 Brussel s , BeLgium

(Mail au,hes>:; from North /Im<o> rici:i ) c\o American Embassy APO New York, NY 09667- 1 011

Tel. :l22 - 51:l < l fl :lO Ext. 2710 Fax. 322-230-0534

iLoston AC":O 12 New En~llelI1J Pi:!.rk Burlingt.on, Mass. 01830

'1"<0>1. 617-2"n-71111 F~x . 617-273 - 2412

New 'iuz:-k fICO 181 South Franklin Avenue Room 20:< Vi:ill<o>y Str<o>;;.m, NY 11581

Tel. 516 - 79 1 -6680 l-'ax. 516-791-90:l4

Atlan ta bCQ Suit.e 210 1669 Phoenix Parkway Atlauta, GJ'I 30319

Tel . 4 0 4 -99 1 - 612 1 Fax . 40 4 - 991 - 726 1

Chicaqu Al'O Room 232 2300 East Devon Avenue Des [,laines, IL 60018

Tel. 3 1 2-691 - "/3':>"7 Fax. 312 -694-7310

1801 Airport Rn~d Mi d -Conl-inenL Airport wirhita, KN 67209

Tel. 316 - 946-4100 Fax . 316 - 946-4407

S".a l,t) e lIeo 1 (;01 Lind I\venue , !;; .W . Renton , W<lshing t.cln 'HIO .~5 405!'i

Tel. 2 06 - 227 - 2180 Fax. ?06-??7-U8l

Anchorage ACO Federal Building ~.O. Box 12, 701 CSt. Anchorage, AX 99515

'l'el . Fax .

Denyer N,'Q

104 55 E<ls t AUrOL:a , CO

Tel. [la.x .

90·'- 2"11- ~92·' 907-276 - 7261

25th Avenu e 00010

303 140 5575 303-340-5430

I,OR An9""1"",,, Am 3229 East Spring StreeL Long Beach, CA 90806-2425

Tel. Fax.

213-988- 5200 213 - 988-5210

Fort Worth, Texas 76 1 93-0 1 00

Street Mdress: 4400 Blue Mound Road For.t Wor th, TX 76101

Tel. 817 - 624 5150 Fax. 817-624-5031

,

AlRCMl"l' CERl'U' .L Cl\.TlON lJIREcrORllTES

Ai rcr.a ft ce rt.i fj ca t i.on Directoriltes h;:r'le formulcttion <l n d stemdardiz"-tiuIl respuIl>;ibilities for specific types o ( aircraft and aeronautical products.

Eng i ne and Propeller Directurate

Regul a t ory and pol i cy r.esponsibil i t.y fnr <1 11 aircr<1ft. en']ines and prupel le:n;.

1 2 Ne w England Executjve Park Bu rlington , Massachusetts 01130 3

Te l. 617 - 270-71 00 Fax. 617-270-2~12

ROlocccail Di r ecto r a t e

Regu l atory and policy n'lspons i hi l ity for normal and tIC-ansport cate~jQry rotorcrail.

Ma iling Add ress: Rotorcraft Directorate Fort. Worth, Tex J.s 76193 - 0100

Street. Addres::;: 4400 Blue Mound Ro,.d I'ort. wurth , Texas 7 6193

Tel. A17 - 624 - 510S I'ax. 81 7-624-5988

Sm~ ll Airplane DirectoK~_~~

Regulat.ory and pol i cy responsibil i ty for:

1. h irplanes weighiI1<j less t hat 12,500 pounds and hav i ng p<1sseng",r configurat.ions of 9 seat.s or less ,

2. Commut.er a i rpl anes weighin'j 19,000 PUUllUS ur l ess , wi th passenger coofigur<lt.ions of 19 seats or l ess, and

3 . Gl iders, airships, and hot ai l: ballouns.

601 East. 12th Street Kansas City, Missouri 64106

Te l . 816 - 426 - 6937 Fax. 016-426-:<1.69

3

Tril'l!ll!0rt A i cplCl'"'' ni rRc torCl t- e

Regulatory ctnd policy respons ihili ty for ,,1 1 tral1spon r.iltegory CI j r planes.

1601 Lind Avenue, S.W. Rel1ton, Washi ngton 98055 · 4056

Tel. 206·227·2104 PClX. ).06·).).7·)100

)..0 ATRWQRTHTNIlSS OFFICE OF WAC

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