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- 2021-26975
2021-26975
Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters
Resumo Rápido
- Número AD
- 2021-26975
- Autoridade
- FAA
- Data de emissão
- 14/12/2021
- Data efetiva
- 18/01/2022
- Criticidade
- routine
- Aeronaves afetadas
- Airbus Helicopters EC135/H135
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
14 de dezembro de 2021
Data Efetiva
18 de janeiro de 2022
Prazo de Cumprimento
Antes do próximo voo
Aeronaves Afetadas
Resumo da Diretiva
A FAA está adotando uma nova diretiva de aeronavegabilidade (AD) para certos helicópteros dos modelos EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+ e EC135T3 fabricados pela Airbus Helicopters Deutschland GmbH. Esta AD foi motivada pelo estabelecimento de limites de vida reduzidos para certas pás do rotor de cauda (TR) com números de peça específicos. Esta AD exige determinar o total de horas em serviço (TIS) de certas pás TR com números de peça específicos, estabelecer um limite de vida para certas pás TR com números de peça específicos, remover do serviço qualquer pá TR que tenha atingido ou excedido seu limite de vida, criar um cartão de histórico de componente, re-identificar certas pás TR com números de peça específicos e remover qualquer pá TR do serviço antes de atingir sua vida de aposentadoria. Esta AD também proíbe a instalação de certas pás TR em certos modelos de helicóptero. A FAA está emitindo esta AD para abordar a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Deutschland GmbH Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, and EC135T3 helicopters. This AD was prompted by reduced life limits being established for certain part-numbered tail rotor (TR) blades. This AD requires determining the total hours time-in-service (TIS) of certain part- numbered TR blades, establishing a life limit for certain part-numbered TR blades, removing from service any TR blade that has reached or exceeded its life limit, creating a component history card, re- identifying certain part-numbered TR blades, and removing any TR blade from service before reaching its retirement life. This AD also prohibits installing certain TR blades on certain model helicopters. 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-2021-0797; Project Identifier MCAI-2021-00218-R; Amendment 39-21838; AD 2021-24-17] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Deutschland GmbH Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, and EC135T3 helicopters. This AD was prompted by reduced life limits being established for certain part-numbered tail rotor (TR) blades. This AD requires determining the total hours time-in-service (TIS) of certain part-numbered TR blades, establishing a life limit for certain part-numbered TR blades, removing from service any TR blade that has reached or exceeded its life limit, creating a component history card, re-identifying certain part-numbered TR blades, and removing any TR blade from service before reaching its retirement life. This AD also prohibits installing certain TR blades on certain model helicopters. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective January 18, 2022. The Director of the Federal Register approved the incorporation by reference of certain documents listed in this AD as of January 18, 2022. ADDRESSES: For service information identified in this final rule, contact Airbus Helicopters, 2701 North Forum Drive, Grand Prairie, TX 75052; telephone (972) 641-0000 or (800) 232-0323; fax (972) 641-3775; or at https://www.airbus.com/​helicopters/​services/​technical-support.html. You may view the referenced service information 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 at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0797. Examining the AD Docket You may examine the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0797; 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 European Union Aviation Safety Agency (EASA) AD, any comments received, and other information. The street 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: Andrea Jimenez, Aerospace Engineer, COS Program Management Section, Operational Safety Branch, Compliance & Airworthiness Division, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 11590; telephone (516) 228-7330; email andrea.jimenez@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to Airbus Helicopters Deutschland GmbH Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, and EC135T3 helicopters, with TR blade part number L642A2002101, L642A2002103, L642A2002104, L642A2002111, or L642A2002112 installed. The NPRM published in the …
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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