Airworthiness Directives; The Boeing Company Airplanes, 63813-63815 [2024-17338]

Download as PDF 63813 Rules and Regulations Federal Register Vol. 89, No. 151 Tuesday, August 6, 2024 This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510. The Code of Federal Regulations is sold by the Superintendent of Documents. NUCLEAR REGULATORY COMMISSION 10 CFR Part 72 [NRC–2024–0041] RIN 3150–AL08 List of Approved Spent Fuel Storage Casks: Holtec International HI–STORM 100 Cask System, Certificate of Compliance No. 1014, Renewed Amendment No. 16 Nuclear Regulatory Commission. ACTION: Direct final rule; confirmation of effective date. AGENCY: The U.S. Nuclear Regulatory Commission (NRC) is confirming the effective date of September 9, 2024, for the direct final rule that was published in the Federal Register on June 25, 2024. This direct final rule amended its spent fuel storage regulations by revising the Holtec International HI– STORM 100 Cask System listing within the ‘‘List of approved spent fuel storage casks’’ to include Renewed Amendment No. 16 to Certificate of Compliance No. 1014. DATES: Effective date: The effective date of September 9, 2024, for the direct final rule published June 25, 2024 (89 FR 52999), is confirmed. ADDRESSES: Please refer to Docket ID NRC–2024–0041 when contacting the NRC about the availability of information for this action. You may obtain publicly available information related to this action by any of the following methods: • Federal Rulemaking Website: Go to https://www.regulations.gov and search for Docket ID NRC–2024–0041. Address questions about NRC dockets to Helen Chang; telephone: 301–415–3228; email: Helen.Chang@nrc.gov. For technical questions, contact the individuals listed in the FOR FURTHER INFORMATION CONTACT section of this document. ddrumheller on DSK120RN23PROD with RULES1 SUMMARY: VerDate Sep<11>2014 17:02 Aug 05, 2024 Jkt 262001 • NRC’s Agencywide Documents Access and Management System (ADAMS): You may obtain publicly available documents online in the ADAMS Public Documents collection at https://www.nrc.gov/reading-rm/ adams.html. To begin the search, select ‘‘Begin Web-based ADAMS Search.’’ For problems with ADAMS, please contact the NRC’s Public Document Room (PDR) reference staff at 1–800–397–4209, at 301–415–4737, or by email to PDR.Resource@nrc.gov. The renewed Amendment No. 16 of Certificate of Compliance No. 1014 and associated changes to the technical specifications, and safety evaluation report can also be viewed in ADAMS under Package Accession No. ML24178A430. • NRC’s PDR: The PDR, where you may examine and order copies of publicly available documents, is open by appointment. To make an appointment to visit the PDR, please send an email to PDR.Resource@nrc.gov or call 1–800–397–4209 or 301–415– 4737, between 8 a.m. and 4 p.m. eastern time, Monday through Friday, except Federal holidays. FOR FURTHER INFORMATION CONTACT: Alexandra Terres, Office of Nuclear Materials Safety and Safeguards, telephone: 301–415–7000, email: Alexandra.Terres@nrc.gov and Yen-Ju Chen, Office of Nuclear Materials Safety and Safeguards, telephone: 301–415– 1018 email: Yen-Ju.Chen@nrc.gov. Both are staff of the U.S. Nuclear Regulatory Commission, Washington, DC 20555– 0001. SUPPLEMENTARY INFORMATION: On June 25, 2024 (89 FR 52999), the NRC published a direct final rule amending its regulations in part 72 of title 10 of the Code of Federal Regulations to include Renewed Amendment No. 16 to Certificate of Compliance No. 1014. Renewed Amendment No. 16 updates the HI–STORM 100 Cask System to add a new overpack, include the ability to use computational fluid dynamics analysis to evaluate site-specific accident scenarios, modify the cask design, modify operational and testing requirements, and make changes to the final safety analysis report. In the direct final rule, the NRC stated that if no significant adverse comments were received, the direct final rule would become effective on September 9, 2024. The NRC did not receive any comments on the direct final rule. PO 00000 Frm 00001 Fmt 4700 Sfmt 4700 Therefore, this direct final rule will become effective as scheduled. Dated: August 1, 2024. For the Nuclear Regulatory Commission. Krupskaya T. Castellon, Acting Chief, Regulatory Analysis and Rulemaking Support Branch, Division of Rulemaking, Environmental, and Financial Support. Office of Nuclear Material Safety and Safeguards. [FR Doc. 2024–17324 Filed 8–5–24; 8:45 am] BILLING CODE 7590–01–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2023–2395; Project Identifier AD–2023–00767–T; Amendment 39–22773; AD 2024–12–09] RIN 2120–AA64 Airworthiness Directives; The Boeing Company Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. AGENCY: The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to all The Boeing Company Model 757 airplanes. As published, the AD number referenced throughout the final rule is incorrect. This document corrects that error. In all other respects, the original document remains the same. SUMMARY: This correction is effective August 22, 2024. The effective date of AD 2024–12–09 remains August 22, 2024. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of August 22, 2024 (89 FR 58257, July 18, 2024). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2023–2395; 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 DATES: E:\FR\FM\06AUR1.SGM 06AUR1 63814 Federal Register / Vol. 89, No. 151 / Tuesday, August 6, 2024 / Rules and Regulations Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE, Washington, DC 20590. Material Incorporated by Reference: • For Boeing material identified in this AD, 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; website myboeingfleet.com. • You may view this 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 at regulations.gov under Docket No. FAA–2023–2395. FOR FURTHER INFORMATION CONTACT: Wayne Ha, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 562–627–5238; email wayne.ha@faa.gov. SUPPLEMENTARY INFORMATION: Background AD 2024–12–09, Amendment 39– 22773 (89 FR 58257, July 18, 2024), requires an inspection or records check of the wing upper skin at the drag fitting attachment holes for any existing repair; repetitive inspections for loose fasteners, skin cracking, and shim migration at the upper link drag fittings, and for cracking in the diagonal brace and diagonal brace fittings; repetitive inspections for cracking of the fastener holes and loose bolt holes; and applicable on-condition actions for all The Boeing Company Model 757 airplanes. ddrumheller on DSK120RN23PROD with RULES1 The FAA reviewed Boeing Alert Requirements Bulletin 757–57A0073 RB, Revision 3, dated May 5, 2023. This material specifies procedures for a general visual inspection or records check of the wing upper skin at the drag fitting attachment holes for any existing repair; repetitive general visual and detailed inspections for loose fasteners, skin cracking, and shim migration at the upper link drag fittings, and for cracking in the diagonal brace and diagonal brace fittings; repetitive open-hole high frequency eddy current (HFEC) inspections for cracking of the fastener holes and loose bolt holes; and applicable on-condition actions. Oncondition actions include performing an ultrasonic inspection for cracks at any repaired upper wing skin location; installing the upper link and upper link pins; replacing drag fittings; installing 17:02 Aug 05, 2024 Jkt 262001 Need for Correction As published, the AD number referenced throughout the final rule is incorrect. The final rule incorrectly references ‘‘AD 2023–12–09.’’ The correct AD number is ‘‘AD 2024–12– 09.’’ 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 August 22, 2024. Since this action only corrects an incorrect AD number, it has no adverse economic impact and imposes no additional burden on any person. Therefore, the FAA has determined that notice and public comment procedures are unnecessary. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Material Incorporated by Reference Under 1 CFR Part 51 VerDate Sep<11>2014 bolts, washers, and nuts; performing a torque check of fasteners on the affected shims; trimming affected shims and applying chemical conversion coating on the shims, fillet seal, and drag fittings; and repairing cracks, migrated shims, mistorqued bolts, and loose fasteners. This material is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in ADDRESSES. Accordingly, pursuant to the authority delegated to me by the Administrator, the FAA amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows: 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 amends § 39.13 by: a. Removing Airworthiness Directive (AD) 2022–08–12, Amendment 39– 22015 (87 FR 26964, May 6, 2022); and ■ b. Adding the following new AD: ■ ■ 2024–12–09 The Boeing Company: Amendment 39–22773; Docket No. FAA–2023–2395; Project Identifier AD– 2023–00767–T. PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 (a) Effective Date This airworthiness directive (AD) is effective August 22, 2024. (b) Affected ADs This AD replaces AD 2022–08–12, Amendment 39–22015 (87 FR 26964, May 6, 2022) (AD 2022–08–12). (c) Applicability This AD applies to all The Boeing Company Model 757–200, PF, –200CB, and –300 series airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 57, Wings. (e) Unsafe Condition This AD was prompted by reports of bolt rotation in the engine drag fitting joint and fastener heads and cracks found in the skin of the fastener holes, a determination that certain drag fittings may be made of alternate materials, which could result in reduced structural integrity of the engine strut, and a determination that additional inspections and revised compliance times are needed. The FAA is issuing this AD to address cracking in the wing upper skin and forward drag fittings, which could lead to a compromised upper link and reduced structural integrity of the engine strut, and possible separation of a strut and engine from the airplane during flight. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Except as specified by paragraph (h) of this AD: At the applicable times specified in the ‘‘Compliance’’ paragraph of Boeing Alert Requirements Bulletin 757–57A0073 RB, Revision 3, dated May 5, 2023, do all applicable actions identified in, and in accordance with, the Accomplishment Instructions of Boeing Alert Requirements Bulletin 757–57A0073 RB, Revision 3, dated May 5, 2023. Note 1 to paragraph (g): Guidance for accomplishing the actions required by this AD can be found in Boeing Alert Service Bulletin 757–57A0073, Revision 3, dated May 5, 2023, which is referred to in Boeing Alert Requirements Bulletin 757–57A0073 RB, Revision 3, dated May 5, 2023. (h) Exceptions to Service Information Specifications (1) Where the Compliance Time columns of the tables in the ‘‘Compliance’’ paragraph of Boeing Alert Requirements Bulletin 757– 57A0073 RB, Revision 3, dated May 5, 2023, use the phrase ‘‘the Original Issue date of Requirements Bulletin 757–57A0073 RB,’’ this AD requires using ‘‘September 10, 2018 (the effective date of AD 2018–16–05, Amendment 39–19345 (83 FR 38250, August 6, 2018))’’ (AD 2018–16–05). (2) Where the Compliance Time columns and notes of the tables in the ‘‘Compliance’’ paragraph of Boeing Alert Requirements Bulletin 757–57A0073 RB, Revision 3, dated E:\FR\FM\06AUR1.SGM 06AUR1 Federal Register / Vol. 89, No. 151 / Tuesday, August 6, 2024 / Rules and Regulations May 5, 2023, use the phrase ‘‘the Revision 1 date of Requirements Bulletin 757–57A0073 RB,’’ this AD requires using ‘‘January 14, 2021 (the effective date of AD 2020–21–17, Amendment 39–21290 (85 FR 79418, December 10, 2020))’’ (AD 2020–21–17). (3) Where the Compliance Time columns and notes of the tables in the ‘‘Compliance’’ paragraph of Boeing Alert Requirements Bulletin 757–57A0073 RB, Revision 3, dated May 5, 2023, use the phrase ‘‘the Revision 2 date of Requirements Bulletin 757–57A0073 RB,’’ this AD requires using ‘‘June 10, 2022 (the effective date of AD 2022–08–12).’’ (4) Where the Compliance Time columns and notes of the tables in the ‘‘Compliance’’ paragraph of Boeing Alert Requirements Bulletin 757–57A0073 RB, Revision 3, dated May 5, 2023, use the phrase ‘‘the Revision 3 date of Requirements Bulletin 757–57A0073 RB,’’ this AD requires using the effective date of this AD. (5) Where Boeing Alert Requirements Bulletin 757–57A0073 RB, Revision 3, dated May 5, 2023, specifies contacting Boeing for repair instructions or for alternative inspections: This AD requires doing the repair, or doing the alternative inspections and applicable on-condition actions using a method approved in accordance with the procedures specified in paragraph (j) of this AD. ddrumheller on DSK120RN23PROD with RULES1 (i) Credit for Previous Actions (1) This paragraph provides credit for the actions specified in paragraph (g) of this AD, except for the open-hole high frequency eddy current inspections at fastener locations 11– 18, if those actions were performed before January 14, 2021 (the effective date of AD 2020–21–17) using Boeing Alert Requirements Bulletin 757–57A0073 RB, dated July 14, 2017. (2) This paragraph provides credit for the actions specified in paragraph (g) of this AD, if those actions were performed before June 10, 2022 (the effective date of AD 2022–08– 12) using Boeing Alert Requirements Bulletin 757–57A0073 RB, Revision 1, dated August 1, 2019. (3) This paragraph provides credit for the actions specified in paragraph (g) of this AD, if those actions were performed before the effective date of this AD using Boeing Alert Requirements Bulletin 757–57A0073 RB, Revision 2, dated March 1, 2021. (j) Alternative Methods of Compliance (AMOCs) (1) The Manager, AIR–520, Continued Operational Safety 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 manager of the certification office, send it to the attention of the person identified in paragraph (k)(1) of this AD. Information may be emailed to: AMOC@ faa.gov. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. VerDate Sep<11>2014 17:02 Aug 05, 2024 Jkt 262001 (3) An AMOC that provides an acceptable level of safety may be used for any repair, modification, or alteration required by this AD if it is approved by The Boeing Company Organization Designation Authorization (ODA) that has been authorized by the Manager, AIR–520, Continued Operational Safety Branch, FAA, to make those findings. To be approved, the repair method, modification deviation, or alteration deviation must meet the certification basis of the airplane, and the approval must specifically refer to this AD. (k) Related Information (1) For more information about this AD, contact Wayne Ha, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 562–627–5238; email wayne.ha@faa.gov. (2) Service information identified in this AD that is not incorporated by reference is available at the address specified in paragraph (l)(3) of this AD. (l) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the material listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this material as applicable to do the actions required by this AD, unless this AD specifies otherwise. (3) The following material was approved for IBR on August 22, 2024 (89 FR 58257, July 18, 2024). (i) Boeing Alert Requirements Bulletin 757–57A0073 RB, Revision 3, dated May 5, 2023. (ii) [Reserved] (4) For Boeing material identified in this AD, 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; website myboeingfleet.com. (5) You may view this 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. (6) You may view this material at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, visit www.archives.gov/federal-register/cfr/ ibr-locations or email fr.inspection@nara.gov. Issued on August 1, 2024. Peter A. White, Deputy Director, Integrated Certificate Management Division, Aircraft Certification Service. [FR Doc. 2024–17338 Filed 8–5–24; 8:45 am] BILLING CODE 4910–13–P PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 63815 DEPARTMENT OF HOMELAND SECURITY Coast Guard 33 CFR Part 117 [Docket No. USCG–2024–0628] Drawbridge Operation Regulation; Gulf Intracoastal Waterway, Osprey, FL Coast Guard, DHS. Notification of temporary deviation from regulations; request for comments. AGENCY: ACTION: The Coast Guard has issued a temporary deviation from the operating schedule that governs the Blackburn Point Bridge across the Gulf Intracoastal Waterway (GICW), mile 63.1, at Osprey, FL. The Casey Key Association has requested the Coast Guard changing the operating schedule allowing the drawbridge scheduled openings. This deviation will test a change to the drawbridge operation schedule to determine whether a permanent change to the schedule is needed. The Coast Guard is seeking comments from the public regarding this deviation. DATES: This deviation is effective from 7 a.m. on August 12, 2024, through 7 p.m. on January 31, 2025. Comments and related material must reach the Coast Guard on or before September 20, 2024. ADDRESSES: You may submit comments identified by docket number USCG– 2024–0628 using Federal Decision Making Portal at https:// www.regulations.gov. See the ‘‘Public Participation and Request for Comments’’ portion of the SUPPLEMENTARY INFORMATION section below for instructions on submitting comments. SUMMARY: If you have questions on this test deviation, call or email Ms. Jennifer Zercher, Bridge Management Specialist, Seventh Coast Guard District; telephone 571–607–5951, email Jennifer.N.Zercher@uscg.mil. SUPPLEMENTARY INFORMATION: FOR FURTHER INFORMATION CONTACT: I. Background, Purpose and Legal Basis Blackburn Point Bridge across the Gulf Intracoastal Waterway (GICW), mile 63.1, at Osprey, FL, is a swing bridge with a 9-foot vertical clearance at mean high water in the closed position. The normal operating schedule for the bridge is set forth in 33 CFR 117.5. The Coast Guard received a request from the Casey Key Association to consider changing the operating schedule for the Blackburn Point Bridge E:\FR\FM\06AUR1.SGM 06AUR1

Agencies

[Federal Register Volume 89, Number 151 (Tuesday, August 6, 2024)]
[Rules and Regulations]
[Pages 63813-63815]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-17338]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-2395; Project Identifier AD-2023-00767-T; 
Amendment 39-22773; AD 2024-12-09]
RIN 2120-AA64


Airworthiness Directives; The Boeing Company Airplanes

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 all The Boeing 
Company Model 757 airplanes. As published, the AD number referenced 
throughout the final rule is incorrect. This document corrects that 
error. In all other respects, the original document remains the same.

DATES: This correction is effective August 22, 2024. The effective date 
of AD 2024-12-09 remains August 22, 2024.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of August 22, 
2024 (89 FR 58257, July 18, 2024).

ADDRESSES: 
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2023-2395; 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

[[Page 63814]]

Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE, Washington, DC 20590.
    Material Incorporated by Reference:
     For Boeing material identified in this AD, 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; website myboeingfleet.com.
     You may view this 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 at regulations.gov under 
Docket No. FAA-2023-2395.

FOR FURTHER INFORMATION CONTACT: Wayne Ha, Aviation Safety Engineer, 
FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 562-627-
5238; email [email protected].

SUPPLEMENTARY INFORMATION:

Background

    AD 2024-12-09, Amendment 39-22773 (89 FR 58257, July 18, 2024), 
requires an inspection or records check of the wing upper skin at the 
drag fitting attachment holes for any existing repair; repetitive 
inspections for loose fasteners, skin cracking, and shim migration at 
the upper link drag fittings, and for cracking in the diagonal brace 
and diagonal brace fittings; repetitive inspections for cracking of the 
fastener holes and loose bolt holes; and applicable on-condition 
actions for all The Boeing Company Model 757 airplanes.

Material Incorporated by Reference Under 1 CFR Part 51

    The FAA reviewed Boeing Alert Requirements Bulletin 757-57A0073 RB, 
Revision 3, dated May 5, 2023. This material specifies procedures for a 
general visual inspection or records check of the wing upper skin at 
the drag fitting attachment holes for any existing repair; repetitive 
general visual and detailed inspections for loose fasteners, skin 
cracking, and shim migration at the upper link drag fittings, and for 
cracking in the diagonal brace and diagonal brace fittings; repetitive 
open-hole high frequency eddy current (HFEC) inspections for cracking 
of the fastener holes and loose bolt holes; and applicable on-condition 
actions. On-condition actions include performing an ultrasonic 
inspection for cracks at any repaired upper wing skin location; 
installing the upper link and upper link pins; replacing drag fittings; 
installing bolts, washers, and nuts; performing a torque check of 
fasteners on the affected shims; trimming affected shims and applying 
chemical conversion coating on the shims, fillet seal, and drag 
fittings; and repairing cracks, migrated shims, mistorqued bolts, and 
loose fasteners. This material is reasonably available because the 
interested parties have access to it through their normal course of 
business or by the means identified in ADDRESSES.

Need for Correction

    As published, the AD number referenced throughout the final rule is 
incorrect. The final rule incorrectly references ``AD 2023-12-09.'' The 
correct AD number is ``AD 2024-12-09.''

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 August 22, 2024.
    Since this action only corrects an incorrect AD number, it has no 
adverse economic impact and imposes no additional burden on any person. 
Therefore, the FAA has determined that notice and public comment 
procedures are unnecessary.

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

    Accordingly, pursuant to the authority delegated to me by the 
Administrator, the FAA 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 amends Sec.  39.13 by:
0
a. Removing Airworthiness Directive (AD) 2022-08-12, Amendment 39-22015 
(87 FR 26964, May 6, 2022); and
0
b. Adding the following new AD:

2024-12-09 The Boeing Company: Amendment 39-22773; Docket No. FAA-
2023-2395; Project Identifier AD-2023-00767-T.

(a) Effective Date

    This airworthiness directive (AD) is effective August 22, 2024.

(b) Affected ADs

    This AD replaces AD 2022-08-12, Amendment 39-22015 (87 FR 26964, 
May 6, 2022) (AD 2022-08-12).

(c) Applicability

    This AD applies to all The Boeing Company Model 757-200, PF, -
200CB, and -300 series airplanes, certificated in any category.

(d) Subject

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

(e) Unsafe Condition

    This AD was prompted by reports of bolt rotation in the engine 
drag fitting joint and fastener heads and cracks found in the skin 
of the fastener holes, a determination that certain drag fittings 
may be made of alternate materials, which could result in reduced 
structural integrity of the engine strut, and a determination that 
additional inspections and revised compliance times are needed. The 
FAA is issuing this AD to address cracking in the wing upper skin 
and forward drag fittings, which could lead to a compromised upper 
link and reduced structural integrity of the engine strut, and 
possible separation of a strut and engine from the airplane during 
flight.

(f) Compliance

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

(g) Required Actions

    Except as specified by paragraph (h) of this AD: At the 
applicable times specified in the ``Compliance'' paragraph of Boeing 
Alert Requirements Bulletin 757-57A0073 RB, Revision 3, dated May 5, 
2023, do all applicable actions identified in, and in accordance 
with, the Accomplishment Instructions of Boeing Alert Requirements 
Bulletin 757-57A0073 RB, Revision 3, dated May 5, 2023.
    Note 1 to paragraph (g): Guidance for accomplishing the actions 
required by this AD can be found in Boeing Alert Service Bulletin 
757-57A0073, Revision 3, dated May 5, 2023, which is referred to in 
Boeing Alert Requirements Bulletin 757-57A0073 RB, Revision 3, dated 
May 5, 2023.

(h) Exceptions to Service Information Specifications

    (1) Where the Compliance Time columns of the tables in the 
``Compliance'' paragraph of Boeing Alert Requirements Bulletin 757-
57A0073 RB, Revision 3, dated May 5, 2023, use the phrase ``the 
Original Issue date of Requirements Bulletin 757-57A0073 RB,'' this 
AD requires using ``September 10, 2018 (the effective date of AD 
2018-16-05, Amendment 39-19345 (83 FR 38250, August 6, 2018))'' (AD 
2018-16-05).
    (2) Where the Compliance Time columns and notes of the tables in 
the ``Compliance'' paragraph of Boeing Alert Requirements Bulletin 
757-57A0073 RB, Revision 3, dated

[[Page 63815]]

May 5, 2023, use the phrase ``the Revision 1 date of Requirements 
Bulletin 757-57A0073 RB,'' this AD requires using ``January 14, 2021 
(the effective date of AD 2020-21-17, Amendment 39-21290 (85 FR 
79418, December 10, 2020))'' (AD 2020-21-17).
    (3) Where the Compliance Time columns and notes of the tables in 
the ``Compliance'' paragraph of Boeing Alert Requirements Bulletin 
757-57A0073 RB, Revision 3, dated May 5, 2023, use the phrase ``the 
Revision 2 date of Requirements Bulletin 757-57A0073 RB,'' this AD 
requires using ``June 10, 2022 (the effective date of AD 2022-08-
12).''
    (4) Where the Compliance Time columns and notes of the tables in 
the ``Compliance'' paragraph of Boeing Alert Requirements Bulletin 
757-57A0073 RB, Revision 3, dated May 5, 2023, use the phrase ``the 
Revision 3 date of Requirements Bulletin 757-57A0073 RB,'' this AD 
requires using the effective date of this AD.
    (5) Where Boeing Alert Requirements Bulletin 757-57A0073 RB, 
Revision 3, dated May 5, 2023, specifies contacting Boeing for 
repair instructions or for alternative inspections: This AD requires 
doing the repair, or doing the alternative inspections and 
applicable on-condition actions using a method approved in 
accordance with the procedures specified in paragraph (j) of this 
AD.

(i) Credit for Previous Actions

    (1) This paragraph provides credit for the actions specified in 
paragraph (g) of this AD, except for the open-hole high frequency 
eddy current inspections at fastener locations 11-18, if those 
actions were performed before January 14, 2021 (the effective date 
of AD 2020-21-17) using Boeing Alert Requirements Bulletin 757-
57A0073 RB, dated July 14, 2017.
    (2) This paragraph provides credit for the actions specified in 
paragraph (g) of this AD, if those actions were performed before 
June 10, 2022 (the effective date of AD 2022-08-12) using Boeing 
Alert Requirements Bulletin 757-57A0073 RB, Revision 1, dated August 
1, 2019.
    (3) This paragraph provides credit for the actions specified in 
paragraph (g) of this AD, if those actions were performed before the 
effective date of this AD using Boeing Alert Requirements Bulletin 
757-57A0073 RB, Revision 2, dated March 1, 2021.

(j) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, AIR-520, Continued Operational Safety 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 manager of the certification office, 
send it to the attention of the person identified in paragraph 
(k)(1) of this AD. Information may be emailed to: [email protected].
    (2) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspector, the manager 
of the responsible Flight Standards Office.
    (3) An AMOC that provides an acceptable level of safety may be 
used for any repair, modification, or alteration required by this AD 
if it is approved by The Boeing Company Organization Designation 
Authorization (ODA) that has been authorized by the Manager, AIR-
520, Continued Operational Safety Branch, FAA, to make those 
findings. To be approved, the repair method, modification deviation, 
or alteration deviation must meet the certification basis of the 
airplane, and the approval must specifically refer to this AD.

(k) Related Information

    (1) For more information about this AD, contact Wayne Ha, 
Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 
98198; telephone 562-627-5238; email [email protected].
    (2) Service information identified in this AD that is not 
incorporated by reference is available at the address specified in 
paragraph (l)(3) of this AD.

(l) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the material listed in this 
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this material as applicable to do the actions 
required by this AD, unless this AD specifies otherwise.
    (3) The following material was approved for IBR on August 22, 
2024 (89 FR 58257, July 18, 2024).
    (i) Boeing Alert Requirements Bulletin 757-57A0073 RB, Revision 
3, dated May 5, 2023.
    (ii) [Reserved]
    (4) For Boeing material identified in this AD, 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; website myboeingfleet.com.
    (5) You may view this 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.
    (6) You may view this material at the National Archives and 
Records Administration (NARA). For information on the availability 
of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].

    Issued on August 1, 2024.
Peter A. White,
Deputy Director, Integrated Certificate Management Division, Aircraft 
Certification Service.
[FR Doc. 2024-17338 Filed 8-5-24; 8:45 am]
BILLING CODE 4910-13-P
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