2020-23658

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-2020-0908; Project Identifier MCAI-2020-01256-T; Amendment 39-21282; AD 2020-21-09] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments; correction. SUMMARY: The FAA is correcting an airworthiness directive (AD) that published in the Federal Register . That AD applies to all Airbus SAS Model A318 series airplanes; Model A319 series airplanes; Model A320 series airplanes; and Model A321 series airplanes. As published, a paragraph reference located in the reporting exception is incorrect. This document corrects that error. In all other respects, the original document remains the same. DATES: This correction is effective October 30, 2020. The effective date of AD 2020-21-09 remains October 30, 2020. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of October 30, 2020 (85 FR 65200, October 15, 2020). The date by which the FAA must receive comments on AD 2020-21-09 remains November 30, 2020. ADDRESSES: For material incorporated by reference (IBR) in this AD, contact the European Union Aviation Safety Agency (EASA), Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 000; email: ADs@easa.europa.eu; internet: www.easa.europa.eu. You may find this IBR material on the EASA website at https://ad.easa.europa.eu. You may view this IBR material 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 in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-0908. 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-2020-0908; 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: Sanjay Ralhan, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3223; email: sanjay.ralhan@faa.gov. SUPPLEMENTARY INFORMATION: AD 2020-21-09, Amendment 39-21282 (85 FR 65200, October 15, 2020) (AD 2020-21-09), currently requires a general visual inspection of the main landing gear (MLG) sliding tubes for cracks, and replacement, if necessary. That AD applies to all Airbus SAS Model A318 series airplanes; Model A319 series airplanes; Model A320 series airplanes; and Model A321 series airplanes. Need for the Correction As published, paragraph (h)(3) of the regulatory text of …

Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.