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- 2023-14003
2023-14003
Airworthiness Directives; Bombardier, Inc., Airplanes
Resumo Rápido
- Número AD
- 2023-14003
- Autoridade
- FAA
- Data de emissão
- 03/07/2023
- Data efetiva
- 07/08/2023
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
03 de julho de 2023
Data Efetiva
07 de agosto de 2023
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretriz de Aeronavegabilidade (DA) 2020-07-13, que se aplicava a certos aviões Bombardier, Inc., Modelo BD-100-1A10. A DA 2020-07-13 exigia a revisão do Manual de Voo do Avião (MVA) existente para fornecer à tripulação de voo novos avisos para "Autoflight" e "Falha de Motor em Subida Durante ALTS CAP". Esta DA exige a revisão do MVA existente para fornecer à tripulação de voo novos avisos para "Autoflight" e "Falha de Motor em Subida Durante (V) ALTS CAP ou (V) ALTV CAP". Esta DA foi motivada por uma revisão dos procedimentos para garantir que todos os modos de captura de altitude aplicáveis utilizados e anunciados na frota afetada sejam incluídos e para denunciar mais claramente estes modos de captura de altitude. A FAA está emitindo esta DA para resolver a condição insegura nestes produtos.
The FAA is superseding Airworthiness Directive (AD) 2020-07- 13, which applied to certain Bombardier, Inc., Model BD-100-1A10 airplanes. AD 2020-07-13 required revising the existing airplane flight manual (AFM) to provide the flightcrew with new warnings for "Autoflight" and "Engine Failure in Climb During ALTS CAP." This AD requires revising the existing AFM to provide the flightcrew with new warnings for "Autoflight" and "Engine Failure in Climb During (V) ALTS CAP or (V) ALTV CAP." This AD was prompted by a revision to the procedures to ensure that all applicable altitude capture modes utilized and annunciated in the affected fleet are included and to more clearly denote these altitude capture modes. 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-2023-0662; Project Identifier MCAI-2022-00745-T; Amendment 39-22464; AD 2023-12-06] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2020-07-13, which applied to certain Bombardier, Inc., Model BD-100-1A10 airplanes. AD 2020-07-13 required revising the existing airplane flight manual (AFM) to provide the flightcrew with new warnings for “Autoflight” and “Engine Failure in Climb During ALTS CAP.” This AD requires revising the existing AFM to provide the flightcrew with new warnings for “Autoflight” and “Engine Failure in Climb During (V) ALTS CAP or (V) ALTV CAP.” This AD was prompted by a revision to the procedures to ensure that all applicable altitude capture modes utilized and annunciated in the affected fleet are included and to more clearly denote these altitude capture modes. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective August 7, 2023. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of August 7, 2023. ADDRESSES:   AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2023-0662; 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 Bombardier Business Aircraft Customer Response Center, 400 Côte-Vertu Road West, Dorval, Québec H4S 1Y9, Canada; telephone 514-855-2999; emailac.yul@aero.bombardier.com; website bombardier.com. • You may view this 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 atregulations.gov under Docket No. FAA-2023-0662. FOR FURTHER INFORMATION CONTACT: Steven Dzierzynski, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7367; email 9-avs-nyaco-cos@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2020-07-13, Amendment 39-19892 (85 FR 20394, April 13, 2020) (AD 2020-07-13). AD 2020-07-13 applied to certain Bombardier, Inc., Model BD-100-1A10 airplanes. AD 2020-07-13 required revising the existing AFM to provide the flightcrew with new warnings for “Autoflight” and “Engine Failure in Climb During ALTS CAP.” T…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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