FAA-2026-10854
Diretivas de Aeronavegabilidade; Aeronaves Embraer S.A.
Resumo Rápido
- Número AD
- FAA-2026-10854
- Autoridade
- FAA
- Data de emissão
- 01/06/2026
- Data efetiva
- 06/07/2026
- Criticidade
- routine
- Aeronaves afetadas
- Embraer Phenom 300
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
01 de junho de 2026
Data Efetiva
06 de julho de 2026
Prazo de Cumprimento
Antes do próximo voo
Aeronaves Afetadas
Requisitos de Conformidade
Requisitos de Conformidade
Ação Requerida
Inspect left-hand and right-hand horizontal stabilizer backlash and replace applicable hinge point attachment parts, pitch trim actuator rod-end attachment parts, and pitch trim actuator.
Prazo de Conformidade
Data Limite
06 de julho de 2026
AD effective date is July 6, 2026
Dados extraídos automaticamente via IA do texto original da DA FAA-2026-10854. Verifique sempre o documento oficial.
Resumo da Diretiva
A FAA está adotando uma nova diretiva de aeronavegabilidade (AD) para determinados aviões Embraer S.A. (Embraer) Modelo EMB-505. Esta AD foi motivada pela possibilidade de que alguns aviões possam ter resultados inválidos dos testes de folga do estabilizador horizontal (EH) devido ao uso de procedimentos incorretos. Esta AD requer a inspeção da folga do estabilizador horizontal esquerdo (E) e direito (D) do avião e substituição, conforme aplicável, de certos pontos de dobradiça e peças de fixação do atuador de comando de arfagem, bem como do atuador de comando de arfagem. A FAA está emitindo esta AD para corrigir a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for certain Embraer S.A. (Embraer) Model EMB-505 airplanes. This AD was prompted by the possibility that some airplanes may have invalid horizontal stabilizer (HS) backlash test results due to the use of incorrect procedures. This AD requires inspecting the airplane's left- hand (LH) and right-hand (RH) HS backlash and replacement, as applicable, of certain hinge point and pitch trim actuator attachment parts and the pitch trim actuator. 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-2025-3993; Project Identifier MCAI-2025-00630-A; Amendment 39-23358; AD 2026-10-18] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Embraer S.A. (Embraer) Model EMB-505 airplanes. This AD was prompted by the possibility that some airplanes may have invalid horizontal stabilizer (HS) backlash test results due to the use of incorrect procedures. This AD requires inspecting the airplane's left-hand (LH) and right-hand (RH) HS backlash and replacement, as applicable, of certain hinge point and pitch trim actuator attachment parts and the pitch trim actuator. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective July 6, 2026. The Director of the Federal Register approved the incorporation by reference ( printed page 32327) of a certain publication listed in this AD as of July 6, 2026. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2025-3993; 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 Agência Nacional de Aviação Civil (ANAC) material identified in this AD, contact ANAC, Continuing Airworthiness Technical Branch (GTAC), Rua Doutor Orlando Feirabend Filho, 230-Centro Empresarial Aquarius-Torre B-Andares 14 a 18, Parque Residencial Aquarius, CEP 12.246-190-São José dos Campos-SP, Brazil; phone: 55 (12) 3203-6600; email:pac@anac.gov.br; website: anac.gov.br/en/. You may find this material on the ANAC website at sistemas.anac.gov.br/certificacao/DA/DAE.asp. • 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 Docket No. FAA-2025-3993. FOR FURTHER INFORMATION CONTACT: Jim Rutherford, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (816) 329-4165; email: jim.rutherford@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 Embraer Model EMB-505 airplanes. The NPRM was published in the Federal Register on November 18, 2025 (90 FR 51607). The NPRM was prompted by ANAC AD 2025…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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