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- 2024-03442
2024-03442
Diretivas de Aeronavegabilidade; Motores Pratt & Whitney Canada Corp.
Resumo Rápido
- Número AD
- 2024-03442
- Autoridade
- FAA
- Data de emissão
- 21/02/2024
- Data efetiva
- 27/03/2024
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
21 de fevereiro de 2024
Data Efetiva
27 de março de 2024
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova Diretiva de Aeronavegabilidade (AD) para todos os motores Pratt & Whitney Canada Corp. (P&WC) Modelos PW307A e PW307D. Esta AD é motivada por uma análise de causa raiz de um evento envolvendo falha não contida de um disco do estágio 1º da turbina de alta pressão (HPT) que resultou em detritos de alta energia penetrando o revestimento do motor e aborto de decolagem. Esta AD exige a remoção de serviço e substituição de certos discos HPT e também proíbe a instalação de certos discos HPT em qualquer motor, conforme especificado em uma AD do Transport Canada, que é incorporada por referência. A FAA está emitindo esta AD para abordar a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for all Pratt & Whitney Canada Corp. (P&WC) Model PW307A and PW307D engines. This AD is prompted by a root cause analysis of an event involving an uncontained failure of a high-pressure turbine (HPT) 1st-stage disk that resulted in high-energy debris penetrating the engine cowling and an aborted takeoff. This AD requires removing from service and replacing certain HPT disks and also prohibits installing certain HPT disks on any engine, as specified in a Transport Canada AD, which is incorporated by reference. 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-2023-2147; Project Identifier MCAI-2023-00663-E; Amendment 39-22670; AD 2024-03-01] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all Pratt & Whitney Canada Corp. (P&WC) Model PW307A and PW307D engines. This AD is prompted by a root cause analysis of an event involving an uncontained failure of a high-pressure turbine (HPT) 1st-stage disk that resulted in high-energy debris penetrating the engine cowling and an aborted takeoff. This AD requires removing from service and replacing certain HPT disks and also prohibits installing certain HPT disks on any engine, as specified in a Transport Canada AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective March 27, 2024. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of March 27, 2024. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2023-2147; 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 service information identified in this final rule, 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. • You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 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 atregulations.gov under Docket No. FAA-2023-2147. FOR FURTHER INFORMATION CONTACT: Barbara Caufield, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (781) 238-7146; email: barbara.caufield@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 all P&WC Model PW307A and PW307D engines. The NPRM published in the Federal Register on November 9, 2023 (88 FR 77236). The NPRM was prompted by AD CF-2023-30, dated May 8, 2023 (Transport Canada AD CF-2023-30) (also referred to as the MCAI), issued by Transport Canada, which is the aviation authority for Canada. The MCAI states that on March 18, 2020, an Airbus Model A321-231 airplane, powered by International Aero Engines AG (IAE) Mod…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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