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2026-07736
Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Resumo Rápido
- Número AD
- 2026-07736
- Autoridade
- FAA
- Data de emissão
- 21/04/2026
- Data efetiva
- 26/05/2026
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
21 de abril de 2026
Data Efetiva
26 de maio de 2026
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está substituindo a Diretiva de Aeronavegabilidade (AD) 2025-22-02, que se aplicava a certos aviões MHI RJ Aviation ULC (certificado de tipo anteriormente mantido pela Bombardier, Inc.) Modelo CL-600-2C10 (Regional Jet Série 700, 701 e 702), CL-600-2C11 (Regional Jet Série 550), CL-600-2D15 (Regional Jet Série 705), CL-600-2D24 (Regional Jet Série 900) e CL-600-2E25 (Regional Jet Série 1000). A AD 2025-22-02 exigia verificações repetitivas de torque dos parafusos do bloco de travamento anti-guinada do estabilizador horizontal (H-stab). Desde a emissão da AD 2025-22-02 pela FAA, foi determinado que ações adicionais devem ser realizadas para resolver a condição insegura. Esta AD continua exigindo as ações da AD 2025-22-02 e exige a substituição dos componentes do bloco de travamento anti-guinada do H-stab. A FAA está emitindo esta AD para resolver a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2025-22- 02, which applied to certain MHI RJ Aviation ULC (type certificate previously held by Bombardier, Inc.) Model CL-600-2C10 (Regional Jet Series 700, 701 &702), CL-600-2C11 (Regional Jet Series 550), CL-600- 2D15 (Regional Jet Series 705), CL-600-2D24 (Regional Jet Series 900), and CL-600-2E25 (Regional Jet Series 1000) airplanes. AD 2025-22-02 required repetitive torque checks of the horizontal stabilizer (H-stab) anti-yaw steady fitting block bolts. Since the FAA issued AD 2025-22- 02, it was determined that additional actions must be done to address the unsafe condition. This AD continues to require the actions in AD 2025-22-02 and requires replacing the H-stab anti-yaw steady fitting block hardware. 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-2026-0728; Project Identifier MCAI-2025-01823-T; Amendment 39-23310; AD 2026-08-02] • RIN 2120-AA64 ( printed page 21245) AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2025-22-02, which applied to certain MHI RJ Aviation ULC (type certificate previously held by Bombardier, Inc.) Model CL-600-2C10 (Regional Jet Series 700, 701 &702), CL-600-2C11 (Regional Jet Series 550), CL-600-2D15 (Regional Jet Series 705), CL-600-2D24 (Regional Jet Series 900), and CL-600-2E25 (Regional Jet Series 1000) airplanes. AD 2025-22-02 required repetitive torque checks of the horizontal stabilizer (H-stab) anti-yaw steady fitting block bolts. Since the FAA issued AD 2025-22-02, it was determined that additional actions must be done to address the unsafe condition. This AD continues to require the actions in AD 2025-22-02 and requires replacing the H-stab anti-yaw steady fitting block hardware. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective May 26, 2026. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of November 20, 2025 (90 FR 49251, November 5, 2025). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-0728; 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; telephone 888-663-3639; emailTC.AirworthinessDirectives-Consignesdenavigabilite.TC@tc.gc.ca. You may find this 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, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. It is also available atregulations.gov under Docket No. FAA-2026-0728. FOR FURTHER INFORMATION CONTACT: Fatin Saumik, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 516-228-7300; email: 9-avs-nyaco-cos@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2025-22-02, Amendment 39-23180 (90 FR 49251, November 5, 2025) (AD 2025-22-02). AD 2025-22-02 applied to certain MHI RJ Aviation ULC (type certificate previously held by Bombardier, Inc.) Model CL-600-2C10 (Regional Jet Series 700, 70…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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