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- 2021-08849
2021-08849
Airworthiness Directives; The Boeing Company Airplanes
Resumo Rápido
- Número AD
- 2021-08849
- Autoridade
- FAA
- Data de emissão
- 04/05/2021
- Data efetiva
- 08/06/2021
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
04 de maio de 2021
Data Efetiva
08 de junho de 2021
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretiva de Aeronavegabilidade (DA) 2019-22-10, que se aplicava a todos os aviões das séries Model 737-600, -700, -700C, -800, -900 e -900ER da The Boeing Company. A DA 2019-22-10 exigia inspeções repetitivas quanto à presença de trincas nos reforços externos das asas esquerda e direita dos encaixes de longarinas e cintas de segurança em uma determinada estação em torno de oito fixadores, e reparo caso alguma trinca fosse encontrada. Para certos aviões, esta DA reduz o prazo de conformidade para a inspeção inicial e, para todos os aviões, esta DA reduz o intervalo de inspeção repetitiva. Esta DA foi motivada pela determinação de que o limite da inspeção inicial e o intervalo da inspeção repetitiva são inadequados para abordar as trincas de forma oportuna. A FAA está emitindo esta DA para resolver a condição insegura nestes produtos.
The FAA is superseding Airworthiness Directive (AD) 2019-22- 10, which applied to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. AD 2019-22-10 required repetitive inspections for cracking of the left- and right-hand side outboard chords of frame fittings and failsafe straps at a certain station around eight fasteners, and repair if any cracking is found. For certain airplanes, this AD reduces the compliance time for the initial inspection, and for all airplanes this AD reduces the repetitive interval. This AD was prompted by a determination that the initial inspection threshold and repetitive inspection interval are inadequate to address the cracking in a timely manner. 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-2020-0789; Project Identifier AD-2020-00849-T; Amendment 39-21519; AD 2021-09-06] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2019-22-10, which applied to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. AD 2019-22-10 required repetitive inspections for cracking of the left- and right-hand side outboard chords of frame fittings and failsafe straps at a certain station around eight fasteners, and repair if any cracking is found. For certain airplanes, this AD reduces the compliance time for the initial inspection, and for all airplanes this AD reduces the repetitive interval. This AD was prompted by a determination that the initial inspection threshold and repetitive inspection interval are inadequate to address the cracking in a timely manner. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective June 8, 2021. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of June 8, 2021. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of November 13, 2019 (84 FR 61533, November 13, 2019). The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of October 3, 2019 (84 FR 52754, October 3, 2019). ADDRESSES: For service information identified in this final rule, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; telephone 562-797-1717; internet https://www.myboeingfleet.com. You may view this service information 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 on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-0789. 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-2020-0789; 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. ( printed page 23596) FOR FURTHER INFORMATION CONTACT: Greg Rutar, Aerospace Engineer, Airframe Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3529; email: Greg.Rutar@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2019-22-10, Amendment 39-19789 (84 FR 61533, November 13, 2019)…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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