2021-20404

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-2021-0459; Project Identifier MCAI-2021-00129-T; Amendment 39-21697; AD 2021-17-14] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. SUMMARY: The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register . That AD applies to certain Gulfstream Aerospace LP Model Gulfstream G280 airplanes. As published, the document number of the Civil Aviation Authority of Israel (CAAI) AD specified in the preamble and regulatory text is incorrect. This document corrects that error. In all other respects, the original document remains the same. DATES: This correction is effective October 14, 2021. The effective date of AD 2021-17-14 remains October 14, 2021. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of October 14, 2021 (86 FR 50451, September 9, 2021). ADDRESSES: For service information identified in this final rule, contact the CAAI, P.O. Box 1101, Golan Street, Airport City, 70100, Israel; telephone 972-3-9774665; fax 972-3-9774592; email aip@mot.gov.il. You may find this IBR material on the CAAI website at https://www.caa.gov.il. 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-2021-0459. 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-2021-0459; 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: Tom Rodriguez, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3226; email Tom.Rodriguez@faa.gov. SUPPLEMENTARY INFORMATION: AD 2021-17-14, Amendment 39-21697 (86 FR 50451, September 9, 2021) (AD 2021-17-14), requires non-destructive testing on the forward (front) spar vertical stiffener and rib 0 for any cracking, installation of a doubler to the forward (front) spar and rib 0 attachment, and repair if necessary. That AD applies to certain Gulfstream Aerospace LP Model Gulfstream G280 airplanes. Need for the Correction As published, the document number of the CAAI AD specified in the preamble and regulatory text of AD 2021-17-14 is incorrect. The document number of the CAAI AD is incorrectly cited as “CAAI AD I-57-2020-06-01.” The correct document number should read as, “CAAI AD ISR-I-…

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