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- 2022-15485
2022-15485
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Resumo Rápido
- Número AD
- 2022-15485
- Autoridade
- FAA
- Data de emissão
- 21/07/2022
- Data efetiva
- 25/08/2022
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
21 de julho de 2022
Data Efetiva
25 de agosto de 2022
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretriz de Aeronavegabilidade (DA) 2015-07-05, que se aplicava a todos os aviões da série Model BAe 146 da BAE Systems (Operations) Limited e aviões da série Model Avro 146-RJ. A DA 2015-07-05 exigia inspeções repetitivas por correntes parasitas externas nas costuras sobrepostas da fuselagem traseira quanto a trincas, corrosão e outros defeitos, e reparo se necessário. Esta DA continua exigindo as ações da DA 2015-07-05, em prazos de conformidade revisados, e também exige inspeções repetitivas por correntes parasitas de baixa frequência (LFEC) para qualquer trinca, corrosão e outros defeitos nas costuras sobrepostas da fuselagem traseira e nos painéis de pele da fuselagem, e reparo se necessário. Esta DA foi motivada pelo relato de um problema de pressurização em um avião durante a decolagem; uma investigação subsequente revelou uma trinca na pele da fuselagem; e que inspeções repetitivas por LFEC nas costuras sobrepostas da fuselagem traseira e nos painéis de pele da fuselagem são necessárias. Certos prazos de conformidade também devem ser revisados. A FAA está emitindo esta DA para resolver a condição insegura nestes produtos.
The FAA is superseding Airworthiness Directive (AD) 2015-07- 05, which applied to all BAE Systems (Operations) Limited Model BAe 146 series airplanes and Model Avro 146-RJ series airplanes. AD 2015-07-05 required repetitive external eddy current inspections on the aft skin lap joints of the rear fuselage for cracking, corrosion, and other defects, and repair if necessary. This AD continues to require the actions in AD 2015-07-05, at certain revised compliance times, and also requires repetitive low frequency eddy current (LFEC) inspections for any cracking, corrosion, and other defects in the aft skin lap joints of the rear fuselage and in the fuselage skin panels, and repair if necessary. This AD was prompted by a report of a pressurization problem on an airplane during climb-out; a subsequent investigation showed a crack in the fuselage skin; and that repetitive LFEC inspections in the rear fuselage aft skin lap joints and in the fuselage skin panels are necessary. Certain compliance times must also be revised. 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-2022-0508; Project Identifier MCAI-2021-01120-T; Amendment 39-22118; AD 2022-14-13] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2015-07-05, which applied to all BAE Systems (Operations) Limited Model BAe 146 series airplanes and Model Avro 146-RJ series airplanes. AD 2015-07-05 required repetitive external eddy current inspections on the aft skin lap joints of the rear fuselage for cracking, corrosion, and other defects, and repair if necessary. This AD continues to require the actions in AD 2015-07-05, at certain revised compliance times, and also requires repetitive low frequency eddy current (LFEC) inspections for any cracking, corrosion, and other defects in the aft skin lap joints of the rear fuselage and in the fuselage skin panels, and repair if necessary. This AD was prompted by a report of a pressurization problem on an airplane during climb-out; a subsequent investigation showed a crack in the fuselage skin; and that repetitive LFEC inspections in the rear fuselage aft skin lap joints and in the fuselage skin panels are necessary. Certain compliance times must also be revised. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective August 25, 2022. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of August 25, 2022. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of May 19, 2015 (80 FR 19871, April 14, 2015). ( printed page 43401) ADDRESSES: For service information identified in this final rule, contact BAE Systems (Operations) Limited, Customer Information Department, Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United Kingdom; telephone +44 1292 675207; fax +44 1292 675704; email RApublications@baesystems.com; internet https://www.baesystems.com/​Businesses/​RegionalAircraft/​index.htm. You may view this referenced service information 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 on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-0508. Examining the AD Docket You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-0508; 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: Todd Thompson, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 206-231-3228; email Todd.Tho…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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