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- FAA-2026-16657
FAA-2026-16657
Diretivas de Aeronavegabilidade; Aviões ATR-GIE Avions de Transport Régional
Resumo Rápido
- Número AD
- FAA-2026-16657
- Autoridade
- FAA
- Data de emissão
- 14/08/2026
- Data efetiva
- 18/09/2026
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
14 de agosto de 2026
Data Efetiva
18 de setembro de 2026
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está substituindo a Diretiva de Aeronavegabilidade (DA) 2023-21-10, que se aplicava a determinados aviões ATR-GIE Avions de Transport Régional, modelos ATR42-500 e ATR72-212A. A DA 2023-21-10 exigia uma inspeção das costelas laterais das bordas de ataque esquerda e direita do estabilizador horizontal (EH), da caixa entre elas, do painel superior da caixa central e do encaixe de reforço frontal do EH para discrepâncias e ações corretivas aplicáveis. Desde que a FAA emitiu a DA 2023-21-10, foi determinado que aviões adicionais são afetados e áreas adicionais devem ser inspecionadas. Esta DA continua a exigir as ações da DA 2023-21-10 e exige a expansão da aplicabilidade e a inspeção da alma do esparre frontal do EH e da área interna da caixa central para discrepâncias e a realização de ações corretivas aplicáveis. A FAA está emitindo esta DA para abordar a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2023-21- 10, which applied to certain ATR-GIE Avions de Transport R[eacute]gional Model ATR42-500 and ATR72-212A airplanes. AD 2023-21-10 required an inspection of the horizontal stabilizer (HS) left- and right-hand leading edge lateral ribs, the box in between, the center box upper panel, and HS forward back-up fitting for discrepancies and applicable corrective action. Since the FAA issued AD 2023-21-10, it was determined that additional airplanes are affected and additional areas must be inspected. This AD continues to require the actions in AD 2023-21-10 and requires expanding the applicability and inspecting the HS front spar web and center box internal area for discrepancies and accomplishing applicable corrective actions. 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-2026-3878; Project Identifier MCAI-2025-00913-T; Amendment 39-23437; AD 2026-16-07] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2023-21-10, which applied to certain ATR-GIE Avions de Transport Régional Model ATR42-500 and ATR72-212A airplanes. AD 2023-21-10 required an inspection of the horizontal stabilizer (HS) left- and right-hand leading edge lateral ribs, the box in between, the center box upper panel, and HS forward back-up fitting for discrepancies and applicable corrective action. Since the FAA issued AD 2023-21-10, it was determined that additional airplanes are affected and additional areas must be inspected. This AD continues to require the actions in AD 2023-21-10 and requires expanding the applicability and inspecting the HS front spar web and center box internal area for discrepancies and accomplishing applicable corrective actions. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective September 18, 2026. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of September 18, 2026. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-3878; 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. Material Incorporated by Reference: • For European Union Aviation Safety Agency (EASA) material identified in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; emailADs@easa.europa.eu. You may find this material on the EASA website at ad.easa.europa.eu. • For ATR-GIE Avions de Transport Régional material identified in this AD, contact ATR—GIE Avions de Transport Régional, 1 Allée Pierre Nadot, 31712 Blagnac Cedex, France; telephone +33 (0) 5 62 21 62 21; fax +33 (0) 5 62 21 67 18; emailcontinued.airworthiness@atr aircraft.com; website atr-aircraft.com. • 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 atregulations.gov under Docket No. FAA-2026-3878. FOR FURTHER INFORMATION CONTACT: Christopher Spencer, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 516-228-7332; email: 9-AVS-AIR-BACO-COS@faa.gov. ( printed page 52485) SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of p…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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