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2020-00700
Diretivas de Aeronavegabilidade; Aviões The Boeing Company
Resumo Rápido
- Número AD
- 2020-00700
- Autoridade
- FAA
- Data de emissão
- 17/01/2020
- Data efetiva
- 21/02/2020
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
17 de janeiro de 2020
Data Efetiva
21 de fevereiro de 2020
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está substituindo a Diretiva de Aeronavegabilidade (AD) 2017-12-07, que se aplicava a certas aeronaves da série Model 737-800, -900 e -900ER da The Boeing Company. A AD 2017-12-07 exigia a substituição da válvula de controle de temperatura do lado esquerdo afetada e da válvula moduladora de ar de trim da cabine de comando. Esta AD mantém os requisitos da AD 2017-12-07, expande a aplicabilidade para incluir aeronaves adicionais e adiciona um novo requisito para certas aeronaves identificarem e substituírem as peças afetadas. Esta AD foi motivada por relatos de falhas em voo da válvula de controle de temperatura do lado esquerdo e da válvula moduladora de ar de trim da cabine de comando. A FAA está emitindo esta AD para abordar a condição insegura nestes produtos.
The FAA is superseding Airworthiness Directive (AD) 2017-12- 07, which applied to certain The Boeing Company Model 737-800, -900, and -900ER series airplanes. AD 2017-12-07 required replacing the affected left temperature control valve and control cabin trim air modulating valve. This AD retains the requirements of AD 2017-12-07, expands the applicability to include additional airplanes, and adds a new requirement for certain airplanes to identify and replace the affected parts. This AD was prompted by reports of in-flight failure of the left temperature control valve and control cabin trim air modulating valve. 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-2019-0478; Product Identifier 2019-NM-040-AD; Amendment 39-19817; AD 2020-01-11] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2017-12-07, which applied to certain The Boeing Company Model 737-800, -900, and -900ER series airplanes. AD 2017-12-07 required replacing the affected left temperature control valve and control cabin trim air modulating valve. This AD retains the requirements of AD 2017-12-07, expands the applicability to include additional airplanes, and adds a new requirement for certain airplanes to identify and replace the affected parts. This AD was prompted by reports of in-flight failure of the left temperature control valve and control cabin trim air modulating valve. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective February 21, 2020. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of July 20, 2017 (82 FR 27416, June 15, 2017). ADDRESSES: For service information identified in this final rule, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; telephone 562-797-1717; internet https://www.myboeingfleet.com. You may view this service information at the FAA, Transport Standards 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-2019-0478. 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-2019-0478; 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 regulatory evaluation, 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: Julie Moon, Aerospace Engineer, Cabin Safety and Environmental Systems Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3571; email: julie.moon@faa.gov. SUPPLEMENTARY INFORMATION: Discussion The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2017-12-07, Amendment 39-18922 (82 FR 27416, June 15, 2017) (“AD 2017-12-07”), for certain The Boeing Company Model 737-800, -900, and -900ER series airplanes. The NPRM published in the Federal Register on July 8, 2019 (84 FR 32341). The NPRM was prompted by reports of in-flight failure of the left temperature control valve and control cabin trim air modulating valve, and a determination that the affected parts may be installed on airplanes outside the applicability of AD 2017-12-07. The NPRM proposed to ret…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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