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- 2022-10782
2022-10782
Airworthiness Directives; General Electric Company Turbofan Engines
Resumo Rápido
- Número AD
- 2022-10782
- Autoridade
- FAA
- Data de emissão
- 20/05/2022
- Data efetiva
- 24/06/2022
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
20 de maio de 2022
Data Efetiva
24 de junho de 2022
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está substituindo a Diretriz de Aeronavegabilidade (AD) 2019-22-05, que se aplicava a todos os motores turbofan modelo CF34-8C da General Electric Company (GE). A AD 2019-22-05 exigia inspeções iniciais e repetitivas da operabilidade dos tubos de combustível da válvula de sangria (OBV), dos conjuntos de hastes de ligação do coletor de ar de sangria da OBV e dos conectores de combustível da OBV. A AD 2019-22-05 também exigia a substituição de OBVs ou do hardware relacionado de hastes de ligação da OBV que falhassem na inspeção. Esta AD foi motivada por múltiplos relatos de vazamentos de combustível, alguns resultando em incêndios de motor, que ocorreram como resultado de mau funcionamento relacionado à OBV. Adicionalmente, o fabricante redesenhou a OBV, o que elimina a necessidade das inspeções repetitivas. Esta AD exige inspeções iniciais e repetitivas dos tubos de combustível da OBV, dos conjuntos de hastes de ligação do coletor de ar de sangria da OBV e dos conectores de combustível da OBV instalados em motores turbofan modelo CF34-8C da GE. Esta AD exige a substituição de OBVs ou do hardware relacionado de hastes de ligação da OBV que falharem na inspeção. Como ação de término das inspeções repetitivas, esta AD exige a substituição de certas OBVs instaladas em motores turbofan modelo CF34-8C da GE. Esta AD também exige a substituição de certas OBVs instaladas em motores turbofan modelo CF34-8E da GE. A FAA está emitindo esta AD para resolver a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2019-22- 05, which applied to all General Electric Company (GE) CF34-8C model turbofan engines. AD 2019-22-05 required initial and repetitive inspections of the operability bleed valve (OBV) fuel tubes, OBV bleed air manifold link rod assemblies, and the OBV fuel fittings. AD 2019- 22-05 also required replacement of OBVs or related OBV link rod hardware that fail inspection. This AD was prompted by multiple reports of fuel leaks, some leading to engine fires, which have occurred as a result of malfunctions related to the OBV. Additionally, the manufacturer has redesigned the OBV, which terminates the need for the repetitive inspections. This AD requires initial and repetitive inspections of the OBV fuel tubes, OBV bleed air manifold link rod assemblies, and the OBV fuel fittings installed on GE CF34-8C model turbofan engines. This AD requires replacement of OBVs or related OBV link rod hardware that fail inspection. As a terminating action to the repetitive inspections, this AD requires replacement of certain OBVs installed on GE CF34-8C model turbofan engines. This AD also requires replacement of certain OBVs installed on GE CF34-8E model turbofan engines. 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-2021-1167; Project Identifier AD-2021-00823-E; Amendment 39-22034; AD 2022-09-14] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2019-22-05, which applied to all General Electric Company (GE) CF34-8C model turbofan engines. AD 2019-22-05 required initial and repetitive inspections of the operability bleed valve (OBV) fuel tubes, OBV bleed air manifold link rod assemblies, and the OBV fuel fittings. AD 2019-22-05 also required replacement of OBVs or related OBV link rod hardware that fail inspection. This AD was prompted by multiple reports of fuel leaks, some leading to engine fires, which have occurred as a result of malfunctions related to the OBV. Additionally, the manufacturer has redesigned the OBV, which terminates the need for the repetitive inspections. This AD requires initial and repetitive inspections of the OBV fuel tubes, OBV bleed air manifold link rod assemblies, and the OBV fuel fittings installed on GE CF34-8C model turbofan engines. This AD requires replacement of OBVs or related OBV link rod hardware that fail inspection. As a terminating action to the repetitive inspections, this AD requires replacement of certain OBVs installed on GE CF34-8C model turbofan engines. This AD also requires replacement of certain OBVs installed on GE CF34-8E model turbofan engines. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective June 24, 2022. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of June 24, 2022. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of December 23, 2019 (84 FR 63569, November 18, 2019). ADDRESSES: For service information identified in this final rule, contact General Electric Company, 1 Neumann Way, Cincinnati, OH 45215; phone: (513) 552-3272; email: aviation.fleetsupport@ge.com; website: https://www.ge.com. You may view this service information at the Airworthiness Products Section, Operational Safety Branch, FAA, 1200 District Avenue, Burlington, MA 01803. For information on the availability of this material at the FAA, call (817) 222-5110. It is also available at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-1167. Examining the AD Docket You may examine the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-1167; 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, 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. FOR FURTHER INFORMATION CONTACT: Scott Stevenson, Aviation Safety Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone: (781) 238-7132; fax: (781) 238-7199; email: Scott.M.Stevenson@faa.gov. SUPPLEMENTARY INFORM…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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