Federal Register - September 22, 2021
Versione di testo Cosa è?Dateas è un sito indipendente non affiliato a entità governative. La fonte dei documenti PDF che pubblichiamo qui è l'entità governativa indicata in ciascuno di essi. Le versioni in testo sono trascrizioni che realizziamo per facilitare l'accesso e la ricerca di informazioni, ma possono contenere errori o non essere complete.
Source: Federal Register
Federal Register / Vol. 86, No. 181 / Wednesday, September 22, 2021 / Rules and Regulations November 10, 2016 ADAMS Accession No. ML16266A185.
DEPARTMENT OF TRANSPORTATION
V. Applicable Regulations
14 CFR Part 39
A. The regulations that apply to those portions of the AP1000 design as amended by Supplemental Information are in 10 CFR parts 20, 50, 52, 73, and 100, codified as of December 6, 2021, that are applicable and technically relevant, as described in the SEs listed in paragraphs III.D.3.a through III.D.3.f of this appendix.
Docket No. FAA20210459; Project Identifier MCAI202100129T; Amendment 3921697; AD 20211714
AGENCY:
B. All nuclear safety issues, except for the generic TS and other operational requirements, associated with the information in the FSER, Supplement Nos. 1
and 2, and the Verification Evaluation Report ADAMS Accession No. ML21131A221; Tier 1 and Tier 2 including referenced information, which the context indicates is intended as requirements, and the investment protection short-term availability controls in Section 16.3 of the DCD as amended by Supplemental Information; and the rulemaking records for initial certification, Amendment 1, and the duration extension of the AP1000 design;
7. All environmental issues concerning severe accident mitigation design alternatives associated with the information in the NRCs EA for the AP1000 design, Appendix 1B of Revision 15 of the generic DCD, the NRCs final EA for Amendment 1 to the AP1000
design, Appendix 1B of Revision 19 of the generic DCD, and the NRCs final EA relating to the extension of the AP1000 standard design certification, for plants referencing this appendix whose site parameters are within those specified in the severe accident mitigation design alternatives evaluation.
VII. Duration of This Appendix This appendix may be referenced for a period of 20 years from February 27, 2006, except as provided for in 10 CFR 52.55b and 52.57b. This appendix remains valid for an applicant or licensee who references this appendix until the application is withdrawn or the license expires, including any period of extended operation under a renewed license.
Dated September 1, 2021.
For the Nuclear Regulatory Commission.
Margaret M. Doane, Executive Director for Operations.
FR Doc. 202120226 Filed 92121; 8:45 am BILLING CODE 759001P
VerDate Sep<11>2014
16:04 Sep 21, 2021
RIN 2120AA64
Airworthiness Directives; Gulfstream Aerospace LP Airplanes; Correction Federal Aviation Administration FAA, DOT.
ACTION: Final rule; correction.
VI. Issue Resolution
Federal Aviation Administration
Jkt 253001
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 20211714 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 97239774665; fax 97239774592;
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 206231
3195. It is also available on the internet at https www.regulations.gov by searching for and locating Docket No.
FAA20210459.
SUMMARY:
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. FAA2021
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
PO 00000
Frm 00007
Fmt 4700
Sfmt 4700
52599
Operations is U.S. Department of Transportation, Docket Operations, M
30, West Building Ground Floor, Room W12140, 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 2062313226; email Tom.Rodriguez@faa.gov.
SUPPLEMENTARY INFORMATION: AD 2021
1714, Amendment 3921697 86 FR
50451, September 9, 2021 AD 2021
1714, 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
20211714 is incorrect. The document number of the CAAI AD is incorrectly cited as CAAI AD I5720200601.
The correct document number should read as, CAAI AD ISRI57202006
01.
Related Service Information Under 1
CFR Part 51
CAAI AD ISRI5720200601, dated January 27, 2021, specifies procedures for non-destructive testing high frequency, mid frequency, and bolt hole eddy current inspections; and a liquid dye penetrant inspection for cracking on the forward front spar vertical stiffener and rib 0, installation of a doubler to the forward front spar and rib 0 attachment, and repair if necessary. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the ADDRESSES section.
Correction of Publication This document corrects an error and correctly adds the AD as an amendment to 14 CFR 39.13. Although no other part of the preamble or regulatory information has been corrected, the FAA is publishing the entire rule in the Federal Register.
The effective date of this AD remains October 14, 2021.
Since this action only corrects the document number of the CAAI AD, it has no adverse economic impact and imposes no additional burden on any person. Therefore, the FAA has
E:FRFM22SER1.SGM
22SER1