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- FAA-2026-16672
FAA-2026-16672
Diretivas de Aeronavegabilidade; Aviões Air Tractor, Inc.
Resumo Rápido
- Número AD
- FAA-2026-16672
- Autoridade
- FAA
- Data de emissão
- 14/08/2026
- Data efetiva
- 31/08/2026
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
14 de agosto de 2026
Data Efetiva
31 de agosto de 2026
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretiva de Aeronavegabilidade (AD) 2024-16-06, que se aplicava a todos os aviões Air Tractor, Inc. (Air Tractor) Modelos AT-802 e AT-802A com o Certificado de Tipo Suplementar (STC) No. SA01795CH da Wipaire, Inc. instalado. A AD 2024-16-06 exigia inspeções repetitivas nas longarinas do estabilizador horizontal esquerdo e direito, dianteiro e traseiro, quanto a trincas, substituição de qualquer longarina do estabilizador horizontal encontrada trincada ou danificada, instalação de conexões tipo bathtub e comunicação dos resultados de inspeção à FAA. Desde que a FAA emitiu a AD 2024-16-06, foram relatadas trincas adicionais nas longarinas do estabilizador horizontal no local onde o travessão de suporte estrutural da deriva vertical se monta na longarina do estabilizador horizontal. Esta AD retém todas as ações da AD 2024-16-06 e acrescenta inspeções em outra área. A FAA está emitindo esta AD para corrigir a condição não segura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2024-16- 06, which applied to all Air Tractor, Inc. (Air Tractor) Model AT-802 and AT-802A airplanes with Wipaire, Inc. Supplemental Type Certificate (STC) No. SA01795CH installed. AD 2024-16-06 required repetitively inspecting the left and right, forward and rear, horizontal stabilizer spars for cracks, replacing any horizontal stabilizer spar found cracked or damaged, installing bathtub fittings, and reporting inspection results to the FAA. Since the FAA issued AD 2024-16-06, additional cracks in the horizontal stabilizer spars were reported where the vertical fin structural support brace mounts to the horizontal stabilizer spar. This AD retains all the actions of AD 2024- 16-06 and adds inspections to another area. 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-2026-7236; Project Identifier AD-2026-00543-A; Amendment 39-23442; AD 2026-16-12] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2024-16-06, which applied to all Air Tractor, Inc. (Air Tractor) Model AT-802 and AT-802A airplanes with Wipaire, Inc. Supplemental Type Certificate (STC) No. SA01795CH installed. AD 2024-16-06 required repetitively inspecting the left and right, forward and rear, horizontal stabilizer spars for cracks, replacing any horizontal stabilizer spar found cracked or damaged, installing bathtub fittings, and reporting inspection results to the FAA. Since the FAA issued AD 2024-16-06, additional cracks in the horizontal stabilizer spars were reported where the vertical fin structural support brace mounts to the horizontal stabilizer spar. This AD retains all the actions of AD 2024-16-06 and adds inspections to another area. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective August 31, 2026. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of August 31, 2026. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of September 4, 2024 (89 FR 67267, August 20, 2024). The FAA must receive comments on this AD by September 28, 2026. 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 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. AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-7236; 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 street address for Docket Operations is listed above. Material Incorporated by Reference: • For Wipaire, Inc. material identified in this AD, contact Wipaire, Inc., 1700 Henry Avenue, Fleming Field (KSGS), South St. Paul, MN 55075; phone: (651) 451-1205; email:customerservice@wipaire.com; website: wipaire.com. • You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (817) 222-5110. It is also available atregulations.gov under Docket No. FAA-2026-7236. …
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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