In Plain English
FAR 21.29 sets the rules for the FAA to issue a type certificate for a product (aircraft, engine, or propeller) built in a foreign country and imported into the United States. It only applies when the U.S. has a bilateral agreement with that country for accepting exports and imports.
For the FAA to issue the type certificate, three conditions must be met:
- The State of Design (the country where the product was designed) must certify that the product has been examined and tested, and meets:
- Applicable noise, fuel venting, exhaust emissions, and fuel efficiency requirements (per § 21.17), or equivalent State of Design standards that produce no greater levels than U.S. rules; and
- Applicable airworthiness requirements (per § 21.17), or equivalent State of Design standards providing an equivalent level of safety.
- The applicant must submit technical data proving compliance.
- All manuals, placards, listings, and instrument markings required by airworthiness and noise rules must be in English.
Why it matters: this is how foreign-built aircraft (think Airbus, Diamond, Pilatus) become legal to operate under U.S. registration. Compliance under this section also satisfies Parts 34, 36, and 38 for emissions, noise, and fuel efficiency.
Regulation Text
14 CFR § 21.29§ 21.29 Issue of type certificate: import products.
(a) The FAA may issue a type certificate for a product that is manufactured in a foreign country or jurisdiction with which the United States has an agreement for the acceptance of these products for export and import and that is to be imported into the United States if—
(1) The applicable State of Design certifies that the product has been examined, tested, and found to meet—
(i) The applicable aircraft noise, fuel venting, exhaust emissions, and fuel efficiency requirements of this subchapter as designated in § 21.17, or the applicable aircraft noise, fuel venting, exhaust emissions, and fuel efficiency requirements of the State of Design, and any other requirements the FAA may prescribe to provide noise, fuel venting, exhaust emission, and fuel efficiency levels no greater than those provided by the applicable aircraft noise, fuel venting, exhaust emissions, and fuel efficiency requirements of this subchapter as designated in § 21.17; and
(ii) The applicable airworthiness requirements of this subchapter as designated in § 21.17, or the applicable airworthiness requirements of the State of Design and any other requirements the FAA may prescribe to provide a level of safety equivalent to that provided by the applicable airworthiness requirements of this subchapter as designated in § 21.17;
(2) The applicant has provided technical data to show the product meets the requirements of paragraph (a)(1) of this section; and
(3) The manuals, placards, listings, and instrument markings required by the applicable airworthiness (and noise, where applicable) requirements are presented in the English language.
(b) A product type certificated under this section is determined to be compliant with the fuel venting and exhaust emission standards of part 34 of this subchapter, the noise standards of part 36 of this subchapter, and the fuel efficiency requirements of part 38 of this subchapter. Compliance with parts 34, 36, and 38 of this subchapter is certified under paragraph (a)(1)(i) of this section, and the applicable airworthiness standards of this subchapter, or an equivalent level of safety, with which compliance is certified under paragraph (a)(1)(ii) of this section.
[Amdt. 21-92, 74 FR 53386, Oct. 16, 2009, as amended by Amdt. No. 21-107, 89 FR 12653, Feb. 16, 2024]