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- 2021-01783
2021-01783
Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes
Resumo Rápido
- Número AD
- 2021-01783
- Autoridade
- FAA
- Data de emissão
- 22/02/2021
- Data efetiva
- 29/03/2021
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
22 de fevereiro de 2021
Data Efetiva
29 de março de 2021
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova diretriz de aeronavegabilidade (AD) para todos os aviões Modelo PC-7 da Pilatus Aircraft Ltd. Esta AD resulta de informação obrigatória de continuidade de aeronavegabilidade (MCAI) originada por uma autoridade aeronáutica de outro país para identificar e corrigir uma condição insegura em um produto aeronáutico. Esta AD exige a revisão da seção de Limitações de Aeronavegabilidade (ALS) do manual de manutenção de aeronave (AMM) existente para introduzir novas inspeções repetitivas obrigatórias para os conjuntos de braço pivô do flap e para certos suportes de ângulo de asa, e para implementar uma alteração no item de tarefa do cilindro de oxigênio e redutor de pressão. A FAA está emitindo esta AD para corrigir a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for all Pilatus Aircraft Ltd. Model PC-7 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. This AD requires revising the Airworthiness Limitations section (ALS) of the existing aircraft maintenance manual (AMM) to introduce new mandatory repetitive inspections for the flap pivot arm assemblies and for certain wing angle brackets, and to implement a change to the Oxygen cylinder and pressure reducer task item. 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-2020-0849; Project Identifier MCAI-2020-01036-A; Amendment 39-21374; AD 2020-26-19] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all Pilatus Aircraft Ltd. Model PC-7 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. This AD requires revising the Airworthiness Limitations section (ALS) of the existing aircraft maintenance manual (AMM) to introduce new mandatory repetitive inspections for the flap pivot arm assemblies and for certain wing angle brackets, and to implement a change to the Oxygen cylinder and pressure reducer task item. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective March 29, 2021. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of March 29, 2021. ADDRESSES: For service information identified in this final rule, contact Pilatus Aircraft Ltd., CH-6371, Customer Technical Support (MCC), P.O. Box 992, CH-6371, Stans, Switzerland; phone: +41 (0)41 619 67 74; fax: +41 (0)41 619 67; email: techsupport@pilatus-aircraft.com; website: https://www.pilatus-aircraft.comen/​. You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. It is also available at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-0849. Examining the AD Docket You may examine the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-0849; 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 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. FOR FURTHER INFORMATION CONTACT: Doug Rudolph, Aerospace Engineer, FAA, General Aviation & Rotorcraft Section, International Validation Branch, 901 Locust, Room 301, Kansas City, Missouri 64106; phone: (816) 329-4059; fax: (816) 329-4090; email: doug.rudolph@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 Pilatus Aircraft Ltd. Model PC-7 airplanes. The NPRM published in the Federal Register on September 24, 2020 (85 FR 60097). The NPRM was prompted by MCAI originated by the Federal Office for Civil Aviation (FOCA), which is the aviation authority for Switzerland. FOCA has issued FOCA AD HB-2020-007, dated July 23, 2020 (referred to after this as the MCAI), to correct an unsafe condition with new mandat…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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