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- 2025-19355
2025-19355
Diretivas de Aeronavegabilidade; Fiberglas-Technik Rudolf Lindner GmbH & Co. KG (Certificado de Tipo Anteriormente Mantido por GROB Aircraft AG, Grob Aerospace GmbH i.l., Grob Aerospace GmbH, Burkhart Grob Luft- und Raumfahrt GmbH & Co. KG) Planadores
Resumo Rápido
- Número AD
- 2025-19355
- Autoridade
- FAA
- Data de emissão
- 02/10/2025
- Data efetiva
- 17/10/2025
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
02 de outubro de 2025
Data Efetiva
17 de outubro de 2025
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova diretriz de aeronavegabilidade (AD) para todos os planadores Fiberglas-Technik Rudolf Lindner GmbH & Co. KG Modelo G103 TWIN II, G103A TWIN II ACRO, G103C TWIN III ACRO e G 103 C TWIN III SL. Esta AD foi motivada por um relato de corrosão nas faces internas da placa de acionamento do leme soldada em aço. Esta AD exige inspeções repetitivas e uma inspeção detalhada única da placa de acionamento do leme quanto à corrosão e entrada de água, além de uma modificação da placa de acionamento do leme para melhorar a proteção contra corrosão, conforme aplicável. Esta AD também exige substituição do leme se corrosão for encontrada durante as inspeções que ultrapassem ferrugem superficial leve. Esta AD também exige aplicação de selante adicional na placa de acionamento do leme, o que constitui ação de encerramento para as inspeções repetitivas. A FAA está emitindo esta AD para tratar a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for all Fiberglas-Technik Rudolf Lindner GmbH & Co. KG Model G103 TWIN II, G103A TWIN II ACRO, G103C TWIN III ACRO, and G 103 C TWIN III SL gliders. This AD was prompted by a report of corrosion on the inner sides of the welded steel rudder drive plate. This AD requires repetitive inspections and a one-time detailed inspection of the rudder drive plate for corrosion and water entry and a modification of the rudder drive plate to improve corrosion protection, as applicable. This AD also requires replacement of the rudder if corrosion is found during the inspections that exceed light surface rust. This AD also requires applying additional sealing to the rudder drive plate, which constitutes terminating action for the repetitive inspections. 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-2025-3421; Project Identifier MCAI-2025-01202-G; Amendment 39-23160; AD 2025-20-07] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all Fiberglas-Technik Rudolf Lindner GmbH & Co. KG Model G103 TWIN II, G103A TWIN II ACRO, G103C TWIN III ACRO, and G 103 C TWIN III SL gliders. This AD was prompted by a report of corrosion on the inner sides of the welded steel rudder drive plate. This AD requires repetitive inspections and a one-time detailed inspection of the rudder drive plate for corrosion and water entry and a modification of the rudder drive plate to improve corrosion protection, as applicable. This AD also requires replacement of the rudder if corrosion is found during the inspections that exceed light surface rust. This AD also requires applying additional sealing to the rudder drive plate, which constitutes terminating action for the repetitive inspections. The ( printed page 47541) FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective October 17, 2025. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of October 17, 2025. The FAA must receive comments on this AD by November 17, 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-2025-3421; 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 street address for Docket Operations is listed above. Material Incorporated by Reference: • For Fiberglas-Technik Rudolf Lindner material identified in this AD, contact Fiberglas-Technik Rudolf Lindner GmbH & Co. KG, Steige 3 Walpertshofen, Germany; phone: +49 (0) 7353 22 43; email:info@LTB-Lindner.com; website: ltb-lindner.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…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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