(1)
New aircraft that are assembled and that have been .ight-tested, and other ClassIproductslocatedin theUnitedStates, except thatexport airworthiness approval maybeissuedfor[any] ofthefollowing withoutassembly or .ight-test :

(i)
[Asmall airplanetype certi.cated underPart3 or4a oftheCivilAirRegu-lations, orPart23of theFederalAviationRegulations, and manufactured under a production certi.cate;

(ii)
Aglidertype certi.cated underSec.21.23 of thispartand manufactured under a production certi.cate; or

(iii) A normal category rotorcraft type certi.cated under Part 6 of the Ci-vil Air Regulations or Part 27 of the Federal Aviation Regulations and manufactured under a production certi.cate.]

(2)
Used aircraft possessing a valid U.S. airworthiness certi.cate, or other used ClassIproductsthathavebeen maintainedinaccordancewith the applicable CARsorFARsand arelocatedinaforeigncountry,if theAdministrator .nds that the location places no undue burden upon the [FAA] in administering the provisions of this regulation.

(3)
Class II and III products that are manufactured and located in the U.S.

(c)
[Export airworthiness approval exceptions. If the export airworthiness approval is issued on the basis of a written statement by the importing state as provided for in Sec. 21.327(e)(4), the requirements that are not met and the di.erences in con.guration, if any, between the product to be exported and the related type certi.catedproduct,arelisted onthe export airworthinessapproval asexceptions.]

Amdt. 21-48, E.. 4/16/79
FAR 21.327 : Application.
(a)
Exceptasprovidedinparagraph(b) ofthis section,anapplicationforexportair-worthiness approval for a Class I or Class II product is made on a form and in a mannerprescribedby theAdministrator andis submitted to the appropriateFlight Standards District O.ce or to the nearest international .eld o.ce.

(b)
A manufacturer holding a production certi.cate may apply orally to the appro-priate Flight Standards District O.ce or the nearest international .eld o.ce for export airworthinessapproval of aClassIIproduct approved underhisproduction certi.cate.

(c)
Application for export airworthiness approval of Class III products is made to the designated representative of the Administrator authorized toissue those approvals.

(d)
A separate application must be made for–

′
Elodie Roux. Septembre 2003
Subpart L–Export Airworthiness Approvals
(1)
Each aircraft;

(2)
Each engine andpropeller,exceptthat one applicationmay be madefor more than one engine or propeller, if all are of the same type and model and are exported to the same purchaser and country; and

(3)
Each type of Class II product, except that one application may be used for more than one type of Class II product when–

(i)
They are separated and identi.ed in the application as to the type and model ofthe relatedClassIproduct; and

(ii)
They are to be exported to the same purchaser and country.

(e)
Each application must be accompanied by a written statement from the importing country thatit will validatethe exportairworthinessapprovalif theproductbeing exported is–

(1)
An aircraft manufactured outside the United States and being exported to a country with which the United States has a reciprocal agreement concerning the validation of export certi.cates;

(2)
An unassembled aircraft which has not been .ight-tested;

(3)
A product that does not meet the special requirement of the importing coun-try; or

(4)
A product that does not meet a requirement speci.ed in Secs. 21.329, 21.331, or 21.333, as applicable, for the issuance of an export airworthiness approval. The written statement must list the requirements not met.
　
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