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- 2026-07170
2026-07170
Airworthiness Directives; Airbus Helicopters
Resumo Rápido
- Número AD
- 2026-07170
- Autoridade
- FAA
- Data de emissão
- 14/04/2026
- Data efetiva
- 14/04/2026
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
14 de abril de 2026
Data Efetiva
14 de abril de 2026
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está removendo a Diretriz de Aeronavegabilidade de Emergência (AD) 2026-01-51, que se aplicava a todos os helicópteros Airbus Helicopters Modelo H160-B. A AD de Emergência 2026-01-51 exigia a substituição dos casquilhos de articulação da haste de comando de passo superior e inferior nas hastes de comando de passo do rotor principal por novos casquilhos de articulação e o fornecimento de informações após a conclusão da substituição. A AD de Emergência 2026-01-51 também proibia a instalação de qualquer casquilho de articulação da haste de comando de passo superior e inferior do rotor principal afetado em qualquer helicóptero, a menos que seja uma peça em condição de aeronavegabilidade. A FAA emitiu a AD de Emergência 2026-01-51 para abordar a falha estrutural dos casquilhos de articulação da haste de comando de passo superior e inferior do rotor principal. Desde a emissão da AD de Emergência 2026-01-51, o fabricante determinou que a falha do casquilho de articulação da haste de comando de passo do rotor principal foi causada por um procedimento de manutenção inadequado e que a questão de aeronavegabilidade não constitui uma condição insegura e, portanto, nenhuma AD é justificada. A FAA concorda e remove a AD de Emergência 2026-01-51.
The FAA is removing Emergency Airworthiness Directive (AD) 2026-01-51, which applied to all Airbus Helicopters Model H160-B helicopters. Emergency AD 2026-01-51 required replacing the upper and lower pitch rod end bearings on the pitch rods of the main rotor with new pitch rod end bearings and reporting information after accomplishment of the replacement. Emergency AD 2026-01-51 also prohibited installing any affected main rotor lower and upper pitch rod end bearings on any helicopter, unless it is a serviceable part. The FAA issued Emergency AD 2026-01-51 to address the structural failure of the main rotor lower and upper pitch rod end bearings. Since the FAA issued Emergency AD 2026-01-51, the manufacturer determined the failure of the main rotor pitch rod end was caused by an inadequate maintenance procedure and that the airworthiness concern is not an unsafe condition and therefore no AD is warranted. The FAA concurs and removes Emergency AD 2026-01-51.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-2026-0732; Project Identifier MCAI-2026-00008-R; Amendment 39-23249; AD 2026-01-51 R1] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; removal. SUMMARY: The FAA is removing Emergency Airworthiness Directive (AD) 2026-01-51, which applied to all Airbus Helicopters Model H160-B helicopters. Emergency AD 2026-01-51 required replacing the upper and lower pitch rod end bearings on the pitch rods of the main rotor with new pitch rod end bearings and reporting information after accomplishment of the replacement. Emergency AD 2026-01-51 also prohibited installing any affected main rotor lower and upper pitch rod end bearings on any helicopter, unless it is a serviceable part. The FAA issued Emergency AD 2026-01-51 to address the structural failure of the main rotor lower and upper pitch rod end bearings. Since the FAA issued Emergency AD 2026-01-51, the manufacturer determined the failure of the main rotor pitch rod end was caused by an inadequate maintenance procedure and that the airworthiness concern is not an unsafe condition and therefore no AD is warranted. The FAA concurs and removes Emergency AD 2026-01-51. DATES: This AD becomes effective April 14, 2026. The FAA must receive comments on this AD by May 29, 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-2026-0732; 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. FOR FURTHER INFORMATION CONTACT: Jacob Fitch, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (817) 222-4130; email: jacob.fitch@faa.gov. SUPPLEMENTARY INFORMATION: Comments Invited The FAA invites you to send any written data, views, or arguments about this final rule. Send your comments using a method listed under ADDRESSES . Include “Docket No. FAA-2026-0732; Project Identifier MCAI-2026-00008-R” at the beginning of your comments. The most helpful comments reference a specific portion of the final rule, explain the reason for any recommended change, and include supporting data. The FAA will consider all comments received by the…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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