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- FAA-2026-10167
FAA-2026-10167
Airworthiness Directives; Bell Textron Canada Limited Helicopters
Resumo Rápido
- Número AD
- FAA-2026-10167
- Autoridade
- FAA
- Data de emissão
- 21/05/2026
- Data efetiva
- 25/06/2026
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
21 de maio de 2026
Data Efetiva
25 de junho de 2026
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova diretiva de aeronavegabilidade (AD) para certos helicópteros modelo 407 fabricados pela Bell Textron Canada Limited (BTCL). Esta AD foi motivada pela determinação de que desgaste por atrito pode ocorrer em várias localizações nos chicotes elétricos localizados na área do painel de instrumentos da aeronave. Esta AD requer uma inspeção visual detalhada única dos chicotes elétricos para desgaste por atrito e ações corretivas se necessário. Esta AD também requer rotação da carcaça fundida do conector da unidade motor-fuselagem e instalação de suporte e braçadeira do chicote de fios, e para certos helicópteros, instalação de manga protetora do feixe de fios. A FAA está emitindo esta AD para corrigir a condição insegura destes produtos.
The FAA is adopting a new airworthiness directive (AD) for certain Bell Textron Canada Limited (BTCL) Model 407 helicopters. This AD was prompted by a determination that chafing can occur at various locations on the electrical harnesses located in the aircraft instrument panel area. This AD requires a one-time detailed visual inspection of the electrical harnesses for chafing and corrective actions if necessary. This AD also requires rotation of the backshell cast housing of connectors of the lower engine airframe unit and installation of a wire harness bracket and support, and for certain helicopters, installation of a wire bundle sleeve. 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-2026-0736; Project Identifier MCAI-2025-00698-R; Amendment 39-23344; AD 2026-10-04] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Bell Textron Canada Limited (BTCL) Model 407 helicopters. This AD was prompted by a determination that chafing can occur at various locations on the electrical harnesses located in the aircraft instrument panel area. This AD requires a one-time detailed visual inspection of the electrical harnesses for chafing and corrective actions if necessary. This AD also requires rotation of the backshell cast housing of connectors of the lower engine airframe unit and installation of a wire harness bracket and support, and for certain helicopters, installation of a wire bundle sleeve. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective June 25, 2026 The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of June 25, 2026. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-0736; 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 address for Docket Operations is U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. Material Incorporated by Reference: • For Transport Canada material identified in this 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. You may find the Transport Canada material on the Transport Canada website at tc.canada.ca/en/aviation. • 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) 222-5118. It is also available atregulations.gov under Docket No. FAA-2026-0736. FOR FURTHER INFORMATION CONTACT: Matthew Williams, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (316) 946-4134; email: matthew.t.williams@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain BTCL Model 407 helicopters. The NPRM was published in the Federal Register on February 3, 2026 (91 FR 4857). The NPRM was prompted by Transport Canada AD CF-2025-22, dated April 23, 2025, (Transport Canada AD CF-2025-22) (also referred to as the MCAI), issued by Transport Can…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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