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2020-16121
Airworthiness Directives; GE Aviation Czech s.r.o. Turboprop Engines
Resumo Rápido
- Número AD
- 2020-16121
- Autoridade
- FAA
- Data de emissão
- 27/07/2020
- Data efetiva
- 31/08/2020
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
27 de julho de 2020
Data Efetiva
31 de agosto de 2020
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está substituindo as Diretivas de Aeronavegabilidade (AD) 2016-07-13 e 2018-03-22, que se aplicam a certos motores turbohélice M601D-11, M601E-11, M601E-11A, M601E-11AS, M601E-11S e M601F da GE Aviation Czech s.r.o. A AD 2016-07-13 exigia inspeção do disco da turbina de potência (PT) do motor e, se encontrado danificado, sua substituição por uma peça elegível para instalação. A AD 2018-03-22 exigia a remoção de certos discos PT do motor identificados pelo número de peça (P/N) instalados nos motores afetados. Esta AD exige uma inspeção do disco PT do motor e, se encontrado danificado, sua substituição por uma peça elegível para instalação. Esta AD também exige a remoção de certos discos PT do motor identificados por P/N instalados nos motores afetados. Esta AD foi motivada pela descoberta de danos em certos discos PT do motor e por uma análise do fabricante que determinou que certos rotores PT do motor têm margem de velocidade excessiva menor do que a originalmente declarada durante a certificação do produto. Esta AD também foi motivada pelo fabricante ter identificado P/Ns e números de série (S/Ns) adicionais de discos PT do motor afetados por danos ou não conformidade desde a publicação das ADs 2016-07-13 e 2018-03-22. A FAA está emitindo esta AD para resolver a condição insegura nestes produtos.
The FAA is superseding Airworthiness Directive (AD) 2016-07-13 and AD 2018-03-22 which apply to certain GE Aviation Czech s.r.o. M601D-11, M601E-11, M601E-11A, M601E-11AS, M601E-11S, and M601F model turboprop engines. AD 2016-07-13 required inspection of the engine power turbine (PT) disk and, if found damaged, its replacement with a part eligible for installation. AD 2018-03-22 required the removal of certain engine PT disks identified by part number (P/N) installed on the affected engines. This AD requires an inspection of the engine PT disk and, if found damaged, its replacement with a part eligible for installation. This AD also requires the removal of certain engine PT disks identified by P/N installed on the affected engines. This AD was prompted by the discovery of damage to certain engine PT disks and a review by the manufacturer that determined that certain engine PT rotors have less overspeed margin than originally declared during product certification. This AD was also prompted by the manufacturer identifying additional P/Ns and serial numbers (S/Ns) of engine PT disks affected by damage or non-conformity since publishing AD 2016-07- 13 and AD 2018-03-22. The FAA is issuing this AD to address the unsafe condition on these products.Texto Completo da Diretiva
Expandir texto completo (Federal Register)Texto completo (Federal Register)
Document Headings Document headings vary by document type but may contain the following: • the agency or agencies that issued and signed a document • the number of the CFR title and the number of each part the document amends, proposes to amend, or is directly related to • the agency docket number / agency internal file number • the RIN which identifies each regulatory action listed in the Unified Agenda of Federal Regulatory and Deregulatory Actions See the Document Drafting Handbook for more details. Department of Transportation Federal Aviation Administration • 14 CFR Part 39 • [Docket No. FAA-2019-1021; Project Identifier MCAI-2019-00120-E; Amendment 39-21166; AD 2020-15-03] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2016-07-13 and AD 2018-03-22 which apply to certain GE Aviation Czech s.r.o. M601D-11, M601E-11, M601E-11A, M601E-11AS, M601E-11S, and M601F model turboprop engines. AD 2016-07-13 required inspection of the engine power turbine (PT) disk and, if found damaged, its replacement with a part eligible for installation. AD 2018-03-22 required the removal of certain engine PT disks identified by part number (P/N) installed on the affected engines. This AD requires an inspection of the engine PT disk and, if found damaged, its replacement with a part eligible for installation. This AD also requires the removal of certain engine PT disks identified by P/N installed on the affected engines. This AD was prompted by the discovery of damage to certain engine PT disks and a review by the manufacturer that determined that certain engine PT rotors have less overspeed margin than originally declared during product certification. This AD was also prompted by the manufacturer identifying additional P/Ns and serial numbers (S/Ns) of engine PT disks affected by damage or non-conformity since publishing AD 2016-07-13 and AD 2018-03-22. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective August 31, 2020. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of August 31, 2020. ADDRESSES: For service information identified in this final rule, contact GE Aviation Czech s.r.o., Beranových 65, 199 02 Praha 9—Letňany, Czech Republic; phone: +420 222 538 111; fax +420 222 538 222; email: tp.ops@ge.com. You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 1200 District Avenue, Burlington, MA 01803. For information on the availability of this material at the FAA, call 781-238-7759. It is also available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-1021. Examining the AD Docket You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-1021; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this final rule, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The address for Docket Operations is U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Mehdi Lamnyi, Aerospace Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7743; fax: 781-238-7199; email: Mehdi.Lamnyi@faa.gov. SUPPLEMENTARY INFORMATION: Discussion The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2016-07-13, Amendment 39-18458 (81 F…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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