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- 2020-24263
2020-24263
Diretivas de Aeronavegabilidade; Airbus Helicopters Deutschland GmbH
Resumo Rápido
- Número AD
- 2020-24263
- Autoridade
- FAA
- Data de emissão
- 03/11/2020
- Data efetiva
- 18/11/2020
- Criticidade
- routine
- Aeronaves afetadas
- Airbus Helicopters EC135/H135
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
03 de novembro de 2020
Data Efetiva
18 de novembro de 2020
Prazo de Cumprimento
Antes do próximo voo
Aeronaves Afetadas
Resumo da Diretiva
A FAA está adotando uma nova diretriz de aeronavegabilidade (AD) para todos os helicópteros Airbus Helicopters Deutschland GmbH Modelo EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3 e EC635T2+. Esta AD foi motivada por relatos de tratamento térmico inadequado de parafusos de titânio (Ti) instalados nos eixos de acionamento do rotor de cauda dianteiro e traseiro, resultando em ruptura do parafuso de Ti. Esta AD exige inspeção para determinar se os parafusos de Ti instalados nos eixos de acionamento do rotor de cauda dianteiro e traseiro são partes afetadas, e substituição se necessário, conforme especificado em uma AD da Agência Europeia de Segurança da Aviação (EASA), que é incorporada por referência. A FAA está emitindo esta AD para abordar a condição insegura nestes produtos.
The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Deutschland GmbH Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3, and EC635T2+ helicopters. This AD was prompted by reports of improper heat treatment of titanium (Ti)-bolts installed on the forward and aft tail rotor drive shafts, resulting in a broken Ti-bolt. This AD requires an inspection to determine if Ti-bolts installed on the forward and aft tail rotor drive shafts are affected parts, and replacement if necessary, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. 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-2020-0919; Project Identifier MCAI-2020-00637-R; Amendment 39-21300; AD 2020-22-04] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Deutschland GmbH Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3, and EC635T2+ helicopters. This AD was prompted by reports of improper heat treatment of titanium (Ti)-bolts installed on the forward and aft tail rotor drive shafts, resulting in a broken Ti-bolt. This AD requires an inspection to determine if Ti-bolts installed on the forward and aft tail rotor drive shafts are affected parts, ( printed page 69494) and replacement if necessary, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD becomes effective November 18, 2020. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of November 18, 2020. The FAA must receive comments on this AD by December 18, 2020. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments. • Fax: 202-493-2251. • Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. • Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For material incorporated by reference (IBR) in this AD, contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 1000; email: ADs@easa.europa.eu; internet: www.easa.europa.eu. You may find this IBR material on the EASA website at https://ad.easa.europa.eu. You may view this IBR material at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call 817-222-5110. It is also available in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-0919. 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-2020-0919; 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 AD, any comments received, and other information. The street address for Docket Operations i…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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