- AeroCopilot
- /
- Diretivas de Aeronavegabilidade
- /
- 2022-19280
2022-19280
Airworthiness Directives; Airbus SAS Airplanes
Resumo Rápido
- Número AD
- 2022-19280
- Autoridade
- FAA
- Data de emissão
- 08/09/2022
- Data efetiva
- 13/10/2022
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
08 de setembro de 2022
Data Efetiva
13 de outubro de 2022
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretriz de Aeronavegabilidade (AD) 2020-22-03, que se aplicava a todos os aviões Airbus SAS Modelo A330-200, -200 Cargueiro, e série -300. A AD 2020-22-03 exigia a revisão do Manual de Voo do Avião (AFM) existente para incorporar procedimentos a serem aplicados se ocorrer uma sobretemperatura de sangria de motor quando a válvula de sangria do motor associada ficar travada aberta, e fornecia a opção de implementação de software atualizado do Computador de Aviso de Voo (FWC), que encerrava a revisão do AFM. Esta AD foi motivada pelo desenvolvimento de novas ações de manutenção e software relacionadas a condições de falha por sobretemperatura. Esta AD continua exigindo as ações especificadas na AD 2020-22-03, exige a realização das novas tarefas de manutenção e ações corretivas, e torna obrigatória a implementação do software FWC atualizado para certos aviões, conforme especificado em uma AD da Agência da União Europeia para a Segurança da Aviação (EASA), que é incorporada por referência. Esta AD também proíbe a instalação de software FWC afetado. A FAA está emitindo esta AD para corrigir a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2020-22- 03, which applied to all Airbus SAS Model A330-200, -200 Freighter, and -300 series airplanes. AD 2020-22-03 required revising the existing airplane flight manual (AFM) to incorporate procedures to be applied if an engine bleed over-temperature occurs when the associated engine bleed valve is jammed open, and provided for the optional embodiment of updated flight warning computer (FWC) software, which terminated the AFM revision. This AD was prompted by the development of new maintenance actions and software related to over-temperature failure conditions. This AD continues to require the actions specified in AD 2020-22-03, requires accomplishing the new maintenance tasks and corrective actions, and mandates embodiment of the updated FWC software for certain airplanes, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD also prohibits the installation of affected FWC software. 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-2022-0680; Project Identifier MCAI-2021-01415-T; Amendment 39-22146; AD 2022-17-08] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2020-22-03, which applied to all Airbus SAS Model A330-200, -200 Freighter, and ( printed page 54866) -300 series airplanes. AD 2020-22-03 required revising the existing airplane flight manual (AFM) to incorporate procedures to be applied if an engine bleed over-temperature occurs when the associated engine bleed valve is jammed open, and provided for the optional embodiment of updated flight warning computer (FWC) software, which terminated the AFM revision. This AD was prompted by the development of new maintenance actions and software related to over-temperature failure conditions. This AD continues to require the actions specified in AD 2020-22-03, requires accomplishing the new maintenance tasks and corrective actions, and mandates embodiment of the updated FWC software for certain airplanes, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD also prohibits the installation of affected FWC software. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective October 13, 2022. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of October 13, 2022. ADDRESSES: For material incorporated by reference (IBR) in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; 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 material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. It is also available in the AD docket at www.regulations.gov under Docket No. FAA-2022-0680. Examining the AD Docket You may examine the AD docket at www.regulations.gov under Docket No. FAA-2022-0680; 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: Vladimir Ulyanov, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax: 206-231-3229; email: vladimir.ulyanov@faa.gov. SUPPLEMENTARY INFORMATION: Background EASA, which is the Technical Agent for the Member States of th…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
Documentos e Referências
Monitore DAs automaticamente para sua aeronave
Cadastre sua aeronave no AeroCopilot e receba alertas por e-mail e notificação quando novas diretivas de aeronavegabilidade afetarem seu tipo de aeronave.
Dados obtidos do Federal Register (federalregister.gov). As informações são fornecidas para fins de consulta — consulte sempre a fonte oficial para fins de compliance regulatório.