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- FAA-2026-14238
FAA-2026-14238
Diretivas de Aeronavegabilidade; Helicópteros Bell Textron Canada Limited
Resumo Rápido
- Número AD
- FAA-2026-14238
- Autoridade
- FAA
- Data de emissão
- 15/07/2026
- Data efetiva
- —
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
15 de julho de 2026
Data Efetiva
Não informada
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA propõe revogar a Diretriz de Aeronavegabilidade (DA) 2022-27-08, que se aplica a certos helicópteros modelo 407 da Bell Textron Canada Limited (Bell). A DA 2022-27-08 exige inspeção da estrutura de fixação do boom de cauda e relato dos resultados da inspeção. Desde a emissão da DA 2022-27-08, foram relatados dois parafusos de fixação do boom de cauda superior esquerdo adicionais quebrados. Esta DA proposta exigiria inspeções repetitivas da estrutura de fixação do boom de cauda, realização de inspeção de torque e substituição de peças de fixação. Esta DA proposta também incluiria a realização de inspeção detalhada do conjunto do boom de cauda e estrutura da fuselagem traseira associada, que seria uma ação terminante aos requisitos de inspeção repetitiva. Esta DA proposta também proibiria a instalação de certos conjuntos de longarina. Esta DA proposta também exigiria revisão da seção de limitações de aeronavegabilidade (SLA) existente do manual de manutenção do helicóptero para incluir novo limite de vida útil dos parafusos de fixação do boom de cauda. A FAA está propondo esta DA para resolver a condição insegura nesses produtos.
The FAA proposes to supersede Airworthiness Directive (AD) 2022-27-08, which applies to certain Bell Textron Canada Limited (Bell) Model 407 helicopters. AD 2022-27-08 requires inspecting the tailboom attachment structure and reporting the inspection results. Since the FAA issued AD 2022-27-08, two additional broken upper-left tailboom attachment bolts have been reported. This proposed AD would require repetitively inspecting the tail boom attachment structure, performing a torque inspection, and replacing attachment hardware. This proposed AD would also include performing a detailed inspection of the tail boom assembly and associated aft fuselage structure, which would be a terminating action to the repetitive inspection requirements. This proposed AD would also prohibit installing certain longeron assemblies. This proposed AD would also require revising the existing airworthiness limitations section (ALS) of the helicopter maintenance manual to include a new life limit for the tail boom attachment bolts. 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-2026-7220; Project Identifier MCAI-2025-01738-R] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD) 2022-27-08, which applies to certain Bell Textron Canada Limited (Bell) Model 407 helicopters. AD 2022-27-08 requires inspecting the tailboom attachment structure and reporting the inspection results. Since the FAA issued AD 2022-27-08, two additional broken upper-left tailboom attachment bolts have been reported. This proposed AD would require repetitively inspecting the tail boom attachment structure, performing a torque inspection, and replacing attachment hardware. This proposed AD would also include performing a detailed inspection of the tail boom assembly and associated aft fuselage structure, which would be a terminating action to the repetitive inspection requirements. This proposed AD would also prohibit installing certain longeron assemblies. This proposed AD would also require revising the existing airworthiness limitations section (ALS) of the helicopter maintenance manual to include a new life limit for the tail boom attachment bolts. The FAA is proposing this AD to address the unsafe condition on these products. DATES: The FAA must receive comments on this NPRM by August 31, 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-2026-7220; 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 Transport Canada material identified in this proposed AD, contact Transport Canada, Transport Canada National Aircraft Certification, 159 Cleopatra Drive, Nepean, Ontario, K1A 0N5, Canada; phone: (888) 663-3639; email:TC.AirworthinessDirectives-Consignesdenavigabilite.TC@tc.gc.ca; website: tc.canada.ca/en/aviation. ( printed page 43346) • You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 10101 Hillwood Parkway, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222-5110. FOR FURTHER INFORMATION CONTACT…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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