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- 2021-18704
2021-18704
Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
Resumo Rápido
- Número AD
- 2021-18704
- Autoridade
- FAA
- Data de emissão
- 31/08/2021
- Data efetiva
- 05/10/2021
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
31 de agosto de 2021
Data Efetiva
05 de outubro de 2021
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretiva de Aeronavegabilidade (DA) 2020-23-13, que se aplicava a todos os aviões ATR-GIE Avions de Transport Régional, modelos ATR42-200, -300 e -320. A DA 2020-23-13 exigia uma inspeção única em relação a discrepâncias dos feixes de fios entre as sondas de ângulo de ataque (AOA) dos lados esquerdo e direito e o computador de alertas da tripulação, e, conforme os resultados, as ações corretivas aplicáveis. Esta DA continua exigindo as ações da DA 2020-23-13, e também exige, para certos aviões, a modificação da fiação do comando de vibração do capitão, e, para todos os aviões, a revisão do manual de voo da aeronave (AFM) existente e dos procedimentos operacionais correspondentes aplicáveis para incorporar procedimentos do empurrador/vibrador de estol, conforme especificado em uma DA da Agência Europeia de Segurança da Aviação (EASA), que é incorporada por referência. Esta DA foi motivada pela ativação falsa do sistema de aviso de estol devido a dano na fiação do feixe de fios entre uma sonda AOA e o computador de alertas da tripulação, e o desenvolvimento de uma modificação de fiação e atualização do AFM para solucionar a condição insegura. A FAA está emitindo esta DA para solucionar a condição insegura desses produtos.
The FAA is superseding Airworthiness Directive (AD) 2020-23- 13, which applied to all ATR--GIE Avions de Transport R[eacute]gional Model ATR42-200, -300, and -320 airplanes. AD 2020-23-13 required a one-time inspection for discrepancies of the wire bundles between the left- and right-hand angle of attack (AOA) probes and the crew alerting computer, and, depending on findings, applicable corrective actions. This AD continues to require the actions in AD 2020-23-13, and also requires for certain airplanes, modifying the captain stick shaker wiring, and for all airplanes, revising the existing aircraft flight manual (AFM) and applicable corresponding operational procedures to incorporate procedures for the stick pusher/shaker, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD was prompted by false activation of the stall warning system due to wiring damage on the wire bundle between an AOA probe and the crew alerting computer, and the development of a wiring modification and AFM update to address 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-2021-0366; Project Identifier MCAI-2021-00080-T; Amendment 39-21685; AD 2021-17-02] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2020-23-13, which applied to all ATR—GIE Avions de Transport Régional Model ATR42-200, -300, and -320 airplanes. AD 2020-23-13 required a one-time inspection for discrepancies of the wire bundles between the left- and right-hand angle of attack (AOA) probes and the crew alerting computer, and, depending on findings, applicable corrective actions. This AD continues to require the actions in AD 2020-23-13, and also requires for certain airplanes, modifying the captain stick shaker wiring, and for all airplanes, revising the existing aircraft flight manual (AFM) and applicable corresponding operational procedures to incorporate procedures for the stick pusher/shaker, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD was prompted by false activation of the stall warning system due to wiring damage on the wire bundle between an AOA probe and the crew alerting computer, and the development of a wiring modification and AFM update to address the unsafe condition. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective October 5, 2021. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of October 5, 2021. ADDRESSES: For material incorporated by reference (IBR) in this AD, contact ( printed page 48491) 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 IBR 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 on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0366. 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-2021-0366; 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: Shahram Daneshmandi, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3220; email: shahram.daneshmandi@faa.gov. SUPPLEMENTARY INFORMATION: Backgro…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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