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- 2020-24855
2020-24855
Diretivas de Aeronavegabilidade; Aeronaves Airbus SAS
Resumo Rápido
- Número AD
- 2020-24855
- Autoridade
- FAA
- Data de emissão
- 10/11/2020
- Data efetiva
- 25/11/2020
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
10 de novembro de 2020
Data Efetiva
25 de novembro de 2020
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretriz de Aeronavegabilidade (DA) 2001-16-13, que se aplicava a determinadas aeronaves Airbus SAS série Model A330. A DA 2001-16-13 exigia inspeção roto-teste de furos de fixadores em certas junções de fuselagem para trincas, reforço da fuselagem entre determinados frames e, se necessário, inspeção e reparo por correntes parasitas de alta frequência (CPAF). Conforme publicada, a aplicabilidade da DA 2001-16-13 identificou inadvertidamente as designações de modelo como números de série. Este documento corrige esse erro. Esta nova DA exige inspeção roto-teste de furos de fixadores em certas junções de fuselagem para trincas, reforço da fuselagem e, se necessário, inspeção e reparo por CPAF. A FAA está emitindo esta DA para abordar a condição de segurança inadequada nestes produtos.
The FAA is superseding Airworthiness Directive (AD) 2001-16- 13, which applied to certain Airbus SAS Model A330 series airplanes. AD 2001-16-13 required a roto-test inspection of fastener holes of certain fuselage joints for cracks, reinforcement of the fuselage between certain frames, and, if necessary, a high frequency eddy current (HFEC) inspection and repair. As published, the applicability of AD 2001-16-13 inadvertently identified the model designations as serial numbers. This document corrects that error. This new AD requires a roto-test inspection of fastener holes of certain fuselage joints for cracks, reinforcement of the fuselage, and, if necessary, an HFEC inspection and repair. 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-2020-0970; Project Identifier AD-2020-01359-T; Amendment 39-21305; AD 2020-22-09] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; request for comments. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2001-16-13, which applied to certain Airbus SAS Model A330 series airplanes. AD 2001-16-13 required a roto-test inspection of fastener holes of certain fuselage joints for cracks, reinforcement of the fuselage between certain frames, and, if necessary, a high frequency eddy current (HFEC) inspection and repair. As published, the applicability of AD 2001-16-13 inadvertently identified the model designations as serial numbers. This document corrects that error. This new AD requires a roto-test inspection of fastener holes of certain fuselage joints for cracks, reinforcement of the fuselage, and, if necessary, an HFEC inspection and repair. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 25, 2020. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of November 25, 2020. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of September 7, 2001 (66 FR 44295, August 23, 2001). The FAA must receive comments on this AD by December 28, 2020. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments. • Fax: 202-493-2251. • Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. • Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For material incorporated by reference (IBR) in this AD, contact Airbus SAS, Airworthiness Office—EAL, Rond-Point Emile Dewoitine No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 45 80; email airworthiness.A330-A340@airbus.com; internet http://www.airbus.com. You may view this referenced 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-2020-0970. 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-2020-0970; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. Th…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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