49 USC § 44704 - Type certificates, production certificates, airworthiness certificates, and design organization certificates

(a) Type Certificates.—

(1) Issuance, investigations, and tests.— The Administrator of the Federal Aviation Administration shall issue a type certificate for an aircraft, aircraft engine, or propeller, or for an appliance specified under paragraph (2)(A) of this subsection when the Administrator finds that the aircraft, aircraft engine, propeller, or appliance is properly designed and manufactured, performs properly, and meets the regulations and minimum standards prescribed under section 44701 (a) of this title. On receiving an application for a type certificate, the Administrator shall investigate the application and may conduct a hearing. The Administrator shall make, or require the applicant to make, tests the Administrator considers necessary in the interest of safety.

(2) Specifications.— The Administrator may—

(A) specify in regulations those appliances that reasonably require a type certificate in the interest of safety;

(B) include in a type certificate terms required in the interest of safety; and

(C) record on the certificate a numerical specification of the essential factors related to the performance of the aircraft, aircraft engine, or propeller for which the certificate is issued.

(3) Special rules for new aircraft and appliances.— Except as provided in paragraph (4), if the holder of a type certificate agrees to permit another person to use the certificate to manufacture a new aircraft, aircraft engine, propeller, or appliance, the holder shall provide the other person with written evidence, in a form acceptable to the Administrator, of that agreement. Such other person may manufacture a new aircraft, aircraft engine, propeller, or appliance based on a type certificate only if such other person is the holder of the type certificate or has permission from the holder.

(4) Limitation for aircraft manufactured before august 5, 2004.— Paragraph (3) shall not apply to a person who began the manufacture of an aircraft before August 5, 2004, and who demonstrates to the satisfaction of the Administrator that such manufacture began before August 5, 2004, if the name of the holder of the type certificate for the aircraft does not appear on the airworthiness certificate or identification plate of the aircraft. The holder of the type certificate for the aircraft shall not be responsible for the continued airworthiness of the aircraft. A person may invoke the exception provided by this paragraph with regard to the manufacture of only one aircraft.

(b) Supplemental Type Certificates.—

(1) Issuance.— The Administrator may issue a type certificate designated as a supplemental type certificate for a change to an aircraft, aircraft engine, propeller, or appliance.

(2) Contents.— A supplemental type certificate issued under paragraph (1) shall consist of the change to the aircraft, aircraft engine, propeller, or appliance with respect to the previously issued type certificate for the aircraft, aircraft engine, propeller, or appliance.

(3) Requirement.— If the holder of a supplemental type certificate agrees to permit another person to use the certificate to modify an aircraft, aircraft engine, propeller, or appliance, the holder shall provide the other person with written evidence, in a form acceptable to the Administrator, of that agreement. A person may change an aircraft, aircraft engine, propeller, or appliance based on a supplemental type certificate only if the person requesting the change is the holder of the supplemental type certificate or has permission from the holder to make the change.

(c) Production Certificates.— The Administrator shall issue a production certificate authorizing the production of a duplicate of an aircraft, aircraft engine, propeller, or appliance for which a type certificate has been issued when the Administrator finds the duplicate will conform to the certificate. On receiving an application, the Administrator shall inspect, and may require testing of, a duplicate to ensure that it conforms to the requirements of the certificate. The Administrator may include in a production certificate terms required in the interest of safety.

(d) Airworthiness Certificates.—

(1) The registered owner of an aircraft may apply to the Administrator for an airworthiness certificate for the aircraft. The Administrator shall issue an airworthiness certificate when the Administrator finds that the aircraft conforms to its type certificate and, after inspection, is in condition for safe operation. The Administrator shall register each airworthiness certificate and may include appropriate information in the certificate. The certificate number or other individual designation the Administrator requires shall be displayed on the aircraft. The Administrator may include in an airworthiness certificate terms required in the interest of safety.

(2) A person applying for the issuance or renewal of an airworthiness certificate for an aircraft for which ownership has not been recorded under section 44107 or 44110 of this title must submit with the application information related to the ownership of the aircraft the Administrator decides is necessary to identify each person having a property interest in the aircraft and the kind and extent of the interest.

(e) Design Organization Certificates.—

(1) Issuance.— Beginning 7 years after the date of enactment of this subsection, the Administrator may issue a design organization certificate to a design organization to authorize the organization to certify compliance with the requirements and minimum standards prescribed under section 44701 (a) for the type certification of aircraft, aircraft engines, propellers, or appliances.

(2) Applications.— On receiving an application for a design organization certificate, the Administrator shall examine and rate the design organization submitting the application, in accordance with regulations to be prescribed by the Administrator, to determine whether the design organization has adequate engineering, design, and testing capabilities, standards, and safeguards to ensure that the product being certificated is properly designed and manufactured, performs properly, and meets the regulations and minimum standards prescribed under section 44701 (a).

(3) Issuance of type certificates based on design organization certification.— The Administrator may rely on certifications of compliance by a design organization when making a finding under subsection (a).

(4) Public safety.— The Administrator shall include in a design organization certificate issued under this subsection terms required in the interest of safety.

(5) No effect on power of revocation.— Nothing in this subsection affects the authority of the Secretary of Transportation to revoke a certificate.

Source

(Pub. L. 103–272, § 1(e),July 5, 1994, 108 Stat. 1188; Pub. L. 104–264, title IV, § 403,Oct. 9, 1996, 110 Stat. 3256; Pub. L. 108–176, title II, § 227(b)(2), (e)(1), title VIII, § 811,Dec. 12, 2003, 117 Stat. 2531, 2532, 2590; Pub. L. 109–59, title IV, § 4405,Aug. 10, 2005, 119 Stat. 1776.)

Historical and Revision Notes

Revised Section	Source (U.S. Code)	Source (Statutes at Large)
44704(a)(1)
49 App.:1423(a)(2) (1st–4th sentences).
Aug. 23, 1958, Pub. L. 85–726, §§ 503(h), 603(a)(1) (related to regulations for appliances), (2), (b) (related to basis for issuing, and contents of, certificates), (c) (related to basis for issuing, and contents of, certificates), 72 Stat. 774, 776.
	49 App.:1655(c)(1).
Oct. 15, 1966, Pub. L. 89–670, § 6(c)(1), 80 Stat. 938; Jan. 12, 1983, Pub. L. 97–449, § 7(b), 96 Stat. 2444.
44704(a)(2)
49 App.:1423(a)(1) (related to regulations for appliances), (2) (5th, last sentences).
	49 App.:1655(c)(1).
44704(b)
49 App.:1423(b) (related to basis for issuing, and contents of, certificates).
	49 App.:1655(c)(1).
44704(c)(1)
49 App.:1423(c) (related to basis for issuing, and contents of, certificates).
	49 App.:1655(c)(1).
44704(c)(2)
49 App.:1403(h).
	49 App.:1655(c)(1).

In subsections (a)–(c)(1), the word “Administrator” in section 603 of the Federal Aviation Act of 1958 (Public Law 85–726, 72 Stat. 776) is retained on authority of 49:106(g).

In subsection (a)(1), the text of 49 App.:1423(a)(2) (1st sentence 1st–16th words) and the words “in regulations” are omitted as surplus. The words “properly designed and manufactured, performs properly” are substituted for “of proper design, material, specification, construction, and performance for safe operation” to eliminate unnecessary words. The word “rules” is omitted as being synonymous with “regulations”. The words “under section 44701 (a) of this title” and “for a type certificate” are added for clarity. The words “including flight tests and tests of raw materials or any part or appurtenance of such aircraft, aircraft engine, propeller, or appliance” are omitted as surplus.

In subsection (a)(2)(A), the words “issuance of” are omitted as surplus.

In subsection (a)(2)(B), the words “the duration thereof and such other” are omitted as surplus. The words “conditions, and limitations” are omitted as being included in “terms”.

In subsection (a)(2)(C), the words “issued for aircraft, aircraft engines, or propellers” and “all of” are omitted as surplus. The word “specification” is substituted for “determination” for clarity.

In subsection (b), the word “satisfactorily” is omitted as surplus. The words “shall inspect, and may require testing of, a duplicate to ensure that it conforms to the requirements of the certificate” are substituted for “shall make such inspection and may require such tests of any aircraft, aircraft engine, propeller, or appliance manufactured under a production certificate as may be necessary to assure manufacture of each unit in conformity with the type certificate or any amendment or modification thereof” to eliminate unnecessary words. The words “the duration thereof and such other . . . conditions, and limitations” are omitted as surplus.

In subsection (c)(1), the words “may apply to” are substituted for “may file with . . . an application” to eliminate unnecessary words. The words “in accordance with regulations prescribed by the Secretary of Transportation” are omitted because of 49:322(a). The words “the duration of such certificate, the type of service for which the aircraft may be used, and such other . . . conditions, and limitations” are omitted as surplus.

In subsection (c)(2), the words “having a property interest” are substituted for “who are holders of property interests” to eliminate unnecessary words.

References in Text

The date of enactment of this subsection, referred to in subsec. (e)(1), is the date of enactment of Pub. L. 108–176, which was approved Dec. 12, 2003.

Amendments

2005—Subsec. (a)(1) to (3). Pub. L. 109–59, § 4405(1)–(3), (5), (6), inserted par. headings, realigned margins, and substituted “Except as provided in paragraph (4), if” for “If” in par. (3).

Subsec. (a)(4). Pub. L. 109–59, § 4405(4), added par. (4).

2003—Pub. L. 108–176, § 227(e)(1), added section catchline and struck out former section catchline which read as follows: “Type certificates, production certificates, and airworthiness certificates”.

Subsec. (a)(3). Pub. L. 108–176, § 811, added par. (3).

Subsec. (e). Pub. L. 108–176, § 227(b)(2), added subsec. (e).

1996—Subsecs. (b) to (d). Pub. L. 104–264added subsec. (b) and redesignated former subsecs. (b) and (c) as (c) and (d), respectively.

Effective Date of 2003 Amendment

Amendment by Pub. L. 108–176applicable only to fiscal years beginning after Sept. 30, 2003, except as otherwise specifically provided, see section 3 ofPub. L. 108–176, set out as a note under section 106 of this title.

Effective Date of 1996 Amendment

Except as otherwise specifically provided, amendment by Pub. L. 104–264applicable only to fiscal years beginning after Sept. 30, 1996, and not to be construed as affecting funds made available for a fiscal year ending before Oct. 1, 1996, see section 3 ofPub. L. 104–264, set out as a note under section 106 of this title.

Plan for Development and Oversight of System for Certification of Design Organizations

Pub. L. 108–176, title II, § 227(b)(1),Dec. 12, 2003, 117 Stat. 2531, provided that: “Not later than 4 years after the date of enactment of this Act [Dec. 12, 2003], the Administrator of the Federal Aviation Administration shall transmit to the Committee on Transportation and Infrastructure of the House of Representatives and the Committee on Commerce, Science, and Transportation of the Senate a plan for the development and oversight of a system for certification of design organizations to certify compliance with the requirements and minimum standards prescribed under section 44701 (a) of title 49, United States Code, for the type certification of aircraft, aircraft engines, propellers, or appliances.”