Airworthiness Directives; Gulfstream Aerospace LP Airplanes; Correction, 52599-52600 [2021-20404]

Download as PDF 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. FAA–2021–0459; Project Identifier MCAI–2021–00129–T; Amendment 39–21697; AD 2021–17–14] * 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 NRC’s EA for the AP1000 design, Appendix 1B of Revision 15 of the generic DCD, the NRC’s final EA for Amendment 1 to the AP1000 design, Appendix 1B of Revision 19 of the generic DCD, and the NRC’s 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 52.55(b) and 52.57(b). This appendix remains valid for an applicant or licensee who references this appendix until the application is withdrawn or the license expires, including any period of extended operation under a renewed license.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. 2021–20226 Filed 9–21–21; 8:45 am] BILLING CODE 7590–01–P VerDate Sep<11>2014 16:04 Sep 21, 2021 RIN 2120–AA64 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 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. 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. 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 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 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–57–2020–06– 01.’’ Related Service Information Under 1 CFR Part 51 CAAI AD ISR–I–57–2020–06–01, 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:\FR\FM\22SER1.SGM 22SER1 52600 Federal Register / Vol. 86, No. 181 / Wednesday, September 22, 2021 / Rules and Regulations determined that notice and public procedures are unnecessary. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Correction Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows: (i) No Reporting Requirement Although the service information referenced in CAAI AD ISR–I–57–2020–06– 01 specifies to submit certain information to the manufacturer, this AD does not include that requirement. PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: ■ Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Corrected] 2. The FAA corrects § 39.13 by correcting the airworthiness directive published at (86 FR 50451) (October 14, 2021) to read: ■ 2021–17–14 Gulfstream Aerospace LP: Amendment 39–21697; Docket No. FAA–2021–0459; Project Identifier MCAI–2021–00129–T. (a) Effective Date This airworthiness directive (AD) is effective October 14, 2021. (b) Affected ADs None. (c) Applicability This AD applies to Gulfstream Aerospace LP Model Gulfstream G280 airplanes, certificated in any category, as identified in The Civil Aviation Authority of Israel (CAAI) AD ISR–I–57–2020–06–01, dated January 27, 2021 (CAAI AD ISR–I–57–2020–06–01). (d) Subject Air Transport Association (ATA) of America Code 57, Wings. (e) Reason This AD was prompted by a report that during full-scale fatigue testing, a crack was found in the area of the attachment of the wing rib 0 to the front spar. The FAA is issuing this AD to address any cracking at the area of the wing rib 0 to the front spar, which could affect the structural integrity of the wing. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Requirements Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, CAAI AD ISR–I–57–2020– 06–01. VerDate Sep<11>2014 16:04 Sep 21, 2021 Jkt 253001 (h) Exception to CAAI AD ISR–I–57–2020– 06–01 Where CAAI AD ISR–I–57–2020–06–01 requires compliance ‘‘not later than 5,000 flight cycles,’’ this AD requires compliance before the accumulation of 5,000 total flight cycles since the date of issuance of the original Israeli airworthiness certificate or the date of issuance of the original Israeli export certificate of airworthiness. (j) Additional AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Large Aircraft Section, International Validation Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or responsible Flight Standards Office, as appropriate. If sending information directly to the Large Aircraft Section, International Validation Branch, send it to the attention of the person identified in paragraph (k) of this AD. Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (2) Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions must be accomplished using a method approved by the Manager, Large Aircraft Section, International Validation Branch, FAA; or CAAI; or CAAI’s authorized Designee. If approved by the CAAI Designee, the approval must include the Designee’s authorized signature. (k) Related Information For more information about this AD, 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. (l) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (3) The following service information was approved for IBR on October 14, 2021 (86 FR 50451, September 9, 2021). (i) Civil Aviation Authority of Israel (CAAI) AD ISR–I–57–2020–06–01, dated January 27, 2021. (ii) [Reserved] PO 00000 Frm 00008 Fmt 4700 Sfmt 4700 (4) For CAAI AD ISR–I–57–2020–06–01, contact 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 CAAI AD on the CAAI website at https://www.caa.gov.il. (5) 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. (6) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, email fr.inspection@nara.gov, or go to: https://www.archives.gov/federal-register/cfr/ ibr-locations.html. Issued on September 16, 2021. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2021–20404 Filed 9–21–21; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2021–0515; Project Identifier AD–2021–00191–E; Amendment 39–21739; AD 2021–20–01] RIN 2120–AA64 Airworthiness Directives; Pratt & Whitney Turbofan Engines Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: The FAA is adopting a new airworthiness directive (AD) for all Pratt & Whitney PW1500G and PW1900G series turbofan engines with a certain high-pressure turbine (HPT) 1st-stage hub or HPT rotor 1st-stage blade retaining plate installed. This AD was prompted by a report from the manufacturer who determined that the HPT 1st-stage hub and HPT rotor 1ststage blade retaining plate fail to meet the published life-cycle limits for each part. This AD requires removal and replacement of the HPT 1st-stage hub and HPT rotor 1st-stage blade retaining plate prior to reaching certain cycle limits. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective October 27, 2021. ADDRESSES: For service information identified in this final rule, contact Pratt & Whitney, 400 Main Street, East Hartford, CT 06118; phone: (800) 565– SUMMARY: E:\FR\FM\22SER1.SGM 22SER1

Agencies

[Federal Register Volume 86, Number 181 (Wednesday, September 22, 2021)]
[Rules and Regulations]
[Pages 52599-52600]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-20404]


=======================================================================
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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


Airworthiness Directives; Gulfstream Aerospace LP Airplanes; 
Correction

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 
[email protected]. 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 [email protected].

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-57-2020-06-01.''

Related Service Information Under 1 CFR Part 51

    CAAI AD ISR-I-57-2020-06-01, 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

[[Page 52600]]

determined that notice and public procedures are unnecessary.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Correction

    Accordingly, pursuant to the authority delegated to me by the 
Administrator, the Federal Aviation Administration amends part 39 of 
the Federal Aviation Regulations (14 CFR part 39) as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority:  49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Corrected]

0
2. The FAA corrects Sec.  39.13 by correcting the airworthiness 
directive published at (86 FR 50451) (October 14, 2021) to read:

2021-17-14 Gulfstream Aerospace LP: Amendment 39-21697; Docket No. 
FAA-2021-0459; Project Identifier MCAI-2021-00129-T.

(a) Effective Date

    This airworthiness directive (AD) is effective October 14, 2021.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Gulfstream Aerospace LP Model Gulfstream G280 
airplanes, certificated in any category, as identified in The Civil 
Aviation Authority of Israel (CAAI) AD ISR-I-57-2020-06-01, dated 
January 27, 2021 (CAAI AD ISR-I-57-2020-06-01).

(d) Subject

    Air Transport Association (ATA) of America Code 57, Wings.

(e) Reason

    This AD was prompted by a report that during full-scale fatigue 
testing, a crack was found in the area of the attachment of the wing 
rib 0 to the front spar. The FAA is issuing this AD to address any 
cracking at the area of the wing rib 0 to the front spar, which 
could affect the structural integrity of the wing.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Requirements

    Except as specified in paragraph (h) of this AD: Comply with all 
required actions and compliance times specified in, and in 
accordance with, CAAI AD ISR-I-57-2020-06-01.

(h) Exception to CAAI AD ISR-I-57-2020-06-01

    Where CAAI AD ISR-I-57-2020-06-01 requires compliance ``not 
later than 5,000 flight cycles,'' this AD requires compliance before 
the accumulation of 5,000 total flight cycles since the date of 
issuance of the original Israeli airworthiness certificate or the 
date of issuance of the original Israeli export certificate of 
airworthiness.

(i) No Reporting Requirement

    Although the service information referenced in CAAI AD ISR-I-57-
2020-06-01 specifies to submit certain information to the 
manufacturer, this AD does not include that requirement.

(j) Additional AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Large Aircraft Section, International Validation Branch, FAA, has 
the authority to approve AMOCs for this AD, if requested using the 
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, 
send your request to your principal inspector or responsible Flight 
Standards Office, as appropriate. If sending information directly to 
the Large Aircraft Section, International Validation Branch, send it 
to the attention of the person identified in paragraph (k) of this 
AD. Information may be emailed to: [email protected]. 
Before using any approved AMOC, notify your appropriate principal 
inspector, or lacking a principal inspector, the manager of the 
responsible Flight Standards Office.
    (2) Contacting the Manufacturer: For any requirement in this AD 
to obtain instructions from a manufacturer, the instructions must be 
accomplished using a method approved by the Manager, Large Aircraft 
Section, International Validation Branch, FAA; or CAAI; or CAAI's 
authorized Designee. If approved by the CAAI Designee, the approval 
must include the Designee's authorized signature.

(k) Related Information

    For more information about this AD, 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 [email protected].

(l) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless this AD specifies otherwise.
    (3) The following service information was approved for IBR on 
October 14, 2021 (86 FR 50451, September 9, 2021).
    (i) Civil Aviation Authority of Israel (CAAI) AD ISR-I-57-2020-
06-01, dated January 27, 2021.
    (ii) [Reserved]
    (4) For CAAI AD ISR-I-57-2020-06-01, contact CAAI, P.O. Box 
1101, Golan Street, Airport City, 70100, Israel; telephone 972-3-
9774665; fax 972-3-9774592; email [email protected]. You may find this 
CAAI AD on the CAAI website at https://www.caa.gov.il.
    (5) 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.
    (6) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, email [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on September 16, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2021-20404 Filed 9-21-21; 8:45 am]
BILLING CODE 4910-13-P

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