(3)
After determining that the type design meets the applicable requirements, a statement certifying thatthisdeterminationhasbeen made;

(4)
After placing the required technical data and type inspection report in the technicaldata .lerequiredbySec.21.293(a)(1)(i),astatementcertifying that this has been done;

(5)
A proposed type certi.cate data sheet; and

(6)
AnAircraftFlightManual(if required) or a summary of requiredoperating limitations and otherinformation necessaryfor safe operation of theproduct.]

Amdt. 21-5, E.. 10/8/65
FAR21.255 :[Deleted.]
[Deleted.] Amdt. 21-5, E.. 10/8/65
FAR21.257 :Type certi.cates;issue.
[An applicant is entitled to a type certi.cate for a product manufactured under a delegation option authorization if the Administrator .nds that the product meets the applicable airworthiness, noise,fuel venting, and exhaust emission requirements(inclu-ding applicable acoustical change or emissions change requirementsin the case of changes in type design).] Amdt. 21-68, E.. 9/10/90
FAR21.259 :[Deleted.]
[Deleted.] Amdt. 21-5, E.. 10/8/65
FAR21.261 :[Equivalent safetyprovisions.]
[The manufacturer shall obtain the Administrator’s concurrence on the application of all equivalent safety provisions applied under Sec. 21.21.] Amdt. 21-5, E.. 10/8/65
FAR21.263 :[Deleted.]
[Deleted.] Amdt. 21-5, E.. 10/8/65
FAR21.265 :[Deleted.]
[Deleted.] Amdt. 21-5, E.. 10/8/65
FAR21.267 :[Production certi.cates.]
[Tohave a new modelor newtype certi.catelisted onhisproduction certi.cate(issued under Subpart G of this part), the manufacturer must submit to the Administrator–
(a)
An application for an amendment to the production certi.cate;

(b)
After determining that theproduction certi.cation requirements ofSubpartG, with respect to the new model or type, are met, a statement certifying that this deter-minationhasbeen made;

(c)
A statementidentifying the type certi.cate number under which theproductisbeing manufactured; and

(d)
After placing the manufacturing and quality control data required by Sec. 21.143 with the data requiredbySec. 21.293(a)(1)(ii), a statement certifying that this has been done.]

Amdt. 21-5, E.. 10/8/65
FAR21.269 :[Export airworthiness approvals.]
[The manufacturer may issue export airworthiness approvals.] Amdt. 21-5, E.. 10/8/65
FAR 21.271 : Airworthiness approval tags.
(a)
A manufacturermayissueanairworthinessapprovaltag[(FAAForm8130-3)] for each engine andpropeller coveredbySec.21.251(b)(4), and mayissue an airworthi-ness approval tag for parts of each product covered by that section, if he .nds, on the basis of inspection and operation tests, that those products conform to a type design for which he holds a type certi.cate and are in condition for safe operation.

(b)
When a new model has been included on the Production Limitation Record, the production certi.cate number shallbe stamped onthe engine orpropelleridenti.-cation data plate instead of issuing an airworthiness approval tag.

Amdt. 21-43, E.. 2/14/75
′
Elodie Roux. Septembre 2003
Subpart J–Delegation Option Authorization Procedures
FAR 21.273 : Airworthiness certi.cates other than experimental.
(a)
The manufacturer may issue[an] airworthiness certi.catefor aircraft manufactured under a delegation option authorization if he .nds, on the basis of the inspection andproduction .ightcheck,thateach aircraftconformstoatypedesignforwhich he holds a type certi.cate and is in a condition for safe operation.

(b)
The manufacturer may authorize any employee to sign airworthiness certi.cates if that employee–

(1)
Performs,orisindirect chargeof,theinspection speci.edinparagraph(a) of this section; and

(2)
Is listed on the manufacturer’s application for the delegation option authori-zation, or on amendments thereof.
　
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