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- 2021-14775
2021-14775
Airworthiness Directives; Airbus Helicopters
Resumo Rápido
- Número AD
- 2021-14775
- Autoridade
- FAA
- Data de emissão
- 13/07/2021
- Data efetiva
- 17/08/2021
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
13 de julho de 2021
Data Efetiva
17 de agosto de 2021
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está substituindo a Diretiva de Aeronavegabilidade (AD) 2017-17-01, que se aplicava a certos helicópteros Airbus Helicopters modelo AS332L2 e EC225LP. A AD 2017-17-01 exigia inspeções repetitivas dos pinos de fixação do rotor principal (MRB). Esta AD continua a exigir inspeções repetitivas dos pinos de fixação do MRB e também exige medição repetitiva do chanfro do pino de fixação em certos intervalos após a remoção de corrosão, conforme especificado em uma AD da Agência Europeia de Segurança da Aviação (agora Agência da União Europeia para a Segurança da Aviação) (EASA), que é incorporada por referência. Esta AD foi motivada pela determinação da FAA de que é necessário medir o chanfro do pino de fixação após a remoção de corrosão, de que a substituição de um pino de fixação após quatro remoções de corrosão não é mais necessária e de que todos os helicópteros Airbus Helicopters modelo AS332L2 e EC225LP são afetados pela condição insegura. A FAA está emitindo esta AD para abordar a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2017-17- 01, which applied to certain Airbus Helicopters Model AS332L2 and EC225LP helicopters. AD 2017-17-01 required repetitive inspections of the main rotor blade (MRB) attachment pins. This AD continues to require the repetitive inspections of the MRB attachment pins, and also requires repetitive measurement of the attachment pin chamfer at certain intervals after corrosion removal, as specified in a European Aviation Safety Agency (now European Union Aviation Safety Agency) (EASA) AD, which is incorporated by reference. This AD was prompted by the FAA's determination that it is necessary to measure the attachment pin chamfer after corrosion removal, that replacement of an attachment pin after four corrosion removals is no longer necessary, and that all Airbus Helicopters Model AS332L2 and EC225LP helicopters are affected by the unsafe condition. 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-2020-1033; Project Identifier MCAI-2020-01393-R; Amendment 39-21622; AD 2021-13-17] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2017-17-01, which applied to certain Airbus Helicopters Model AS332L2 and EC225LP helicopters. AD 2017-17-01 required repetitive inspections of the main rotor blade (MRB) attachment pins. This AD continues to require the repetitive inspections of the MRB attachment pins, and also requires repetitive measurement of the attachment pin chamfer at certain intervals after corrosion removal, as specified in a European Aviation Safety Agency (now European Union Aviation Safety Agency) (EASA) AD, which is incorporated by reference. This AD was prompted by the FAA's determination that it is necessary to measure the attachment pin chamfer after corrosion removal, that replacement of an attachment pin after four corrosion removals is no longer necessary, and that all Airbus Helicopters Model AS332L2 and EC225LP helicopters are affected by the unsafe condition. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective August 17, 2021. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of August 17, 2021. ADDRESSES: For material incorporated by reference (IBR) in this AD, contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 000; email: ADs@easa.europa.eu; internet: www.easa.europa.eu. You may find this material on the EASA website at https://ad.easa.europa.eu. You may view this 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-2020-1033. 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-2020-1033; 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, 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: Katherine Venegas, Aviation Safety Engineer, Cabin Safety, Mechanical and Environmental Systems Section, Los Angeles ACO Branch, FAA, 3960 Paramount Boulevard, Lakewood, CA 90712-4137; phone: 562-627-5353; email: katherine.venegas@faa.gov. SUPPLEMENTARY INFORMATION: Background The EASA, which is the Technical Agent for the Member States of the ( printed page 36636) European Union, has issued EASA AD 2018-0172, dated August 7, 2018 (EASA AD 2018-0172) (also referred to as the Mandatory Continuing Airworthiness Information, or the MCAI), to correct an unsafe condition for all Airbus Helicopters Model AS332L2 and EC225LP helicopters. EASA AD 2018-0172 superseded EASA AD 2015-0016, dated January 30, 2015 (which prompted FAA AD 2017-17-01, Amendment 39-18991 (82 FR 39506, August 21, 2017) (AD 2017-17-01)). The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2017-17-01. AD 2017-17-01 applied to certain Airbus Helicopters Model AS332L2 and EC225LP helicopters. The NPRM published in the Federal Register on November 24, 2020 (85 FR 74…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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