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- FAA-2025-16263
FAA-2025-16263
Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes
Resumo Rápido
- Número AD
- FAA-2025-16263
- Autoridade
- FAA
- Data de emissão
- 25/08/2025
- Data efetiva
- —
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
25 de agosto de 2025
Data Efetiva
Não informada
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA propõe superseder a Diretiva de Aeronavegabilidade (DA) 2007-06-11, que se aplica a determinados aviões SOCATA (certificado de tipo atualmente mantido pela DAHER AEROSPACE) Modelo TBM 700. A DA 2007-06-11 exige inspeção repetitiva dos pontos de fixação e parafusos do estabilizador vertical quanto à presença de trincas ou corrosão e, se necessário, reparo ou substituição da peça danificada, seguido de aplicação de reforço de proteção contra corrosão. Desde a emissão da DA 2007-06-11, a Agência Europeia para a Segurança da Aviação (EASA), que é o Agente Técnico dos Estados-Membros da União Europeia, supersedeu a anterior DA francesa da Direction générale de l'aviation civile (DGAC) para introduzir novas informações de serviço fornecendo instruções para instalação de novos pontos de fixação do estabilizador vertical com material melhorado resistente à corrosão como ação opcional de encerramento das inspeções repetitivas. Esta DA proposta manteria os requisitos da DA 2007-06-11 e incluiria uma nova ação opcional de encerramento das inspeções repetitivas. A FAA está propondo esta DA para abordar a condição insegura nestes produtos.
The FAA proposes to supersede Airworthiness Directive (AD) 2007-06-11, which applies to certain SOCATA (type certificate now held by DAHER AEROSPACE) Model TBM 700 airplanes. AD 2007-06-11 requires repetitively inspecting the vertical stabilizer attachment fittings and bolts for cracks or corrosion, and, if necessary, repairing or replacing the damaged part and then applying a corrosion protection reinforcement. Since the FAA issued AD 2007-06-11, the European Union Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, superseded the previous Direction generale de l'aviation civile (DGAC) France AD to introduce new service information providing instructions for installing new vertical stabilizer attachment fittings having improved corrosion resistant material as an optional terminating action for the repetitive inspections. This proposed AD would retain the requirements of AD 2007- 06-11 and include a new optional terminating action for the repetitive inspections. The FAA is proposing 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-2025-2265; Project Identifier MCAI-2024-00714-A] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD) 2007-06-11, which applies to certain SOCATA (type certificate now held by DAHER AEROSPACE) Model TBM 700 airplanes. AD 2007-06-11 requires repetitively inspecting the vertical stabilizer attachment fittings and bolts for cracks or corrosion, and, if necessary, repairing or replacing the damaged part and then applying a corrosion protection reinforcement. Since the FAA issued AD 2007-06-11, the European Union Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, superseded the previous Direction generale de l'aviation civile (DGAC) France AD to introduce new service information providing instructions for installing new vertical stabilizer attachment fittings having improved corrosion resistant material as an optional terminating action for the repetitive inspections. This proposed AD would retain the requirements of AD 2007-06-11 and include a new optional terminating action for the repetitive inspections. The FAA is proposing this AD to address the unsafe condition on these products. DATES: The FAA must receive comments on this NPRM by October 9, 2025. 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-2025-2265; 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 NPRM, the mandatory continuing airworthiness information (MCAI) any comments received, and other information. The street address for Docket Operations is listed above. Material Incorporated by Reference: • For DAHER AEROSPACE and EADS SOCATA material identified in this proposed AD, contact DAHER AEROSPACE, Customer Support, Airplane Division, 65921 Tarbes Cedex 9, France; phone: 33 (0)5 62.41.73.00; email:tbmcare@daher.com; website: daher.com. • You may view this service information 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. FOR FURTHER INFORMATION CONTACT: Hye Yoon Jang, Aviation Safety Engineer, FAA, 1600 Ste…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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