Section 21.119

14 CFR Ch. I (1-1-19 Edition)

finds that the applicant meets the requirements of SectionSection 21.113 and 21.115.
(b) A supplemental type certificate
consists of - 
(1) The approval by the FAA of a
change in the type design of the product; and
(2) The type certificate previously
issued for the product.
[Doc. No. 5085, 29 FR 14568, Oct. 24, 1964, as
amended by Amdt. 21-92, 74 FR 53387, Oct. 16,
2009]

Section 21.119 Privileges.
The holder of a supplemental type
certificate may - 
(a) In the case of aircraft, obtain airworthiness certificates;
(b) In the case of other products, obtain approval for installation on certificated aircraft; and
(c) Obtain a production certificate in
accordance with the requirements of
subpart G of this part for the change in
the type design approved by the supplemental type certificate.
[Doc. No. 5085, 29 FR 14568, Oct. 24, 1964, as
amended by Amdt. 21-92, 74 FR 53387, Oct. 16,
2009]

Section 21.120 Responsibility
of
supplemental type certificate holders to
provide written permission for alterations.
A supplemental type certificate holder who allows a person to use the supplemental type certificate to alter an
aircraft, aircraft engine, or propeller
must provide that person with written
permission acceptable to the FAA.
[Doc. No. FAA-2003-14825, 71 FR 52258, Sept.
1, 2006]

Subpart F - Production Under Type
Certificate
SOURCE: Docket No. 5085, 29 FR 14568, Oct.
24, 1964, unless otherwise noted.

spaschal on DSK3GDR082PROD with CFR

Section 21.121 Applicability.
This subpart prescribes rules for production under a type certificate.
Section 21.122 Location of or change to manufacturing facilities.
(a) A type certificate holder may utilize manufacturing facilities located
outside of the United States if the FAA

finds no undue burden in administering
the applicable requirements of Title 49
U.S.C. and this subchapter.
(b) The type certificate holder must
obtain FAA approval before making
any changes to the location of any of
its manufacturing facilities.
(c) The type certificate holder must
immediately notify the FAA, in writing, of any change to the manufacturing facilities that may affect the inspection, conformity, or airworthiness
of its product or article.
[Doc. No. FAA-2006-25877, Amdt. 21-92, 74 FR
53387, Oct. 16, 2009; Amdt. 21-92A, 75 FR 9095,
Mar. 1, 2010]

Section 21.123 Production under type certificate.
Each manufacturer of a product
being manufactured under a type certificate must - 
(a) Maintain at the place of manufacture all information and data specified
in SectionSection 21.31 and 21.41;
(b) Make each product and article
thereof available for inspection by the
FAA;
(c) Maintain records of the completion of all inspections and tests required by SectionSection 21.127, 21.128, and 21.129 for
at least 5 years for the products and articles thereof manufactured under the
approval and at least 10 years for critical
components
identified
under
Section 45.15(c) of this chapter;
(d) Allow the FAA to make any inspection or test, including any inspection or test at a supplier facility, necessary to determine compliance with
this subchapter;
(e) Mark the product in accordance
with part 45 of this chapter, including
any critical parts;
(f) Identify any portion of that product (e.g., sub-assemblies, component
parts, or replacement articles) that
leave the manufacturer-s facility as
FAA approved with the manufacturer-s
part number and name, trademark,
symbol, or other FAA-approved manufacturer-s identification; and
(g) Except as otherwise authorized by
the FAA, obtain a production certificate for that product in accordance
with subpart G of this part within 6

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