Airworthiness Directives; International Aero Engines, LLC Engines

Citation88 FR 74024
Published date30 October 2023
Record Number2023-23929
CourtFederal Aviation Administration
SectionRules and Regulations
Federal Register, Volume 88 Issue 208 (Monday, October 30, 2023)
[Federal Register Volume 88, Number 208 (Monday, October 30, 2023)]
                [Rules and Regulations]
                [Pages 74024-74025]
                From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
                [FR Doc No: 2023-23929]
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                DEPARTMENT OF TRANSPORTATION
                Federal Aviation Administration
                14 CFR Part 39
                [Docket No. FAA-2023-1996; Project Identifier AD-2022-01361-E;
                Amendment 39-22570; AD 2023-20-11]
                RIN 2120-AA64
                Airworthiness Directives; International Aero Engines, LLC Engines
                AGENCY: Federal Aviation Administration (FAA), DOT.
                ACTION: Final rule; request for comment; correction.
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                SUMMARY: The FAA is correcting an airworthiness directive (AD) that was
                published in the Federal Register. That AD applies to certain
                International Aero Engines, LLC (IAE LLC) Model PW1124G1-JM, PW1127G-
                JM, PW1127GA-JM, PW1129G-JM, PW1130G-JM, PW1133G-JM, and PW1133GA-JM
                engines. As published, a part number was inadvertently excluded in the
                regulatory text of the AD. This document corrects that error. In all
                other respects, the original document remains the same.
                DATES: This correction is effective November 1, 2023. The effective
                date of AD 2023-20-11 remains November 1, 2023.
                 The Director of the Federal Register approved the incorporation by
                reference of a certain publication listed in this AD as of November 1,
                2023 (88 FR 71466, October 17, 2023).
                 The date for submitting comments on AD 2023-20-11 remains December
                1, 2023.
                ADDRESSES: You may send comments, using the procedures found in 14 CFR
                11.43 and 11.45, by any of the following methods:
                 Federal eRulemaking Portal: Go to regulations.gov. Follow
                the instructions for submitting comments.
                 Fax: (202) 493-2251.
                 Mail: U.S. Department of Transportation, Docket
                Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
                Jersey Avenue SE, Washington, DC 20590.
                 Hand Delivery: Deliver to Mail address above between 9
                a.m. and 5 p.m., Monday through Friday, except Federal holidays.
                 AD Docket: You may examine the AD docket at regulations.gov under
                Docket No. FAA-2023-1996; 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; request for comment; correction, any
                comments received, and other information. The street address for Docket
                Operations is listed above.
                 Material Incorporated by Reference:
                 For Pratt & Whitney service information identified in this
                final rule, contact International Aero Engines, LLC, 400 Main Street,
                East Hartford, CT 06118; phone: (860) 565-0140; email:
                [email protected]; website: connect.prattwhitney.com.
                 You may view this referenced service information at the
                FAA, Airworthiness Products Section, Operational Safety Branch 1200
                District Avenue, Burlington, MA 01803. For information on the
                availability of this material at the FAA, call (817) 222-5110. It is
                also available at regulations.gov under Docket No. FAA-2023-1996.
                FOR FURTHER INFORMATION CONTACT: Mark Taylor, Aviation Safety Engineer,
                FAA, 2200 South 216th Street, Des Moines, WA 98198; phone: (781) 238-
                7229; email: [email protected].
                SUPPLEMENTARY INFORMATION:
                Comments Invited
                 The FAA invites you to send any written data, views, or arguments
                about this final rule. Send your comments to an address listed under
                ADDRESSES. Include ``Docket No. FAA-2023-1996 and Project Identifier
                AD-2022-01361-E'' at the beginning of your comments. The most helpful
                comments reference a specific portion of the final rule, explain the
                reason for any recommended change, and include supporting data. The FAA
                will consider all comments received by the closing date and may amend
                this final rule because of those comments.
                 Except for Confidential Business Information (CBI) as described in
                the following paragraph, and other information as described in 14 CFR
                11.35, the FAA will post all comments received, without change, to
                regulations.gov, including any personal information you provide. The
                agency will also post a report summarizing each substantive verbal
                contact received about this final rule.
                Confidential Business Information
                 CBI is commercial or financial information that is both customarily
                and actually treated as private by its owner. Under the Freedom of
                Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
                disclosure. If your comments responsive to this AD contain commercial
                or financial information that is customarily treated as private, that
                you actually treat as private, and that is relevant or responsive to
                this AD, it is important that you clearly designate the submitted
                comments as CBI. Please mark each page of your submission containing
                CBI as ``PROPIN.'' The FAA will treat such marked submissions as
                confidential under the FOIA, and they will not be placed in the public
                docket of this AD. Submissions containing CBI should be sent to Mark
                Taylor, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des
                Moines, WA 98198. Any commentary that the FAA receives which is not
                specifically designated as CBI will be placed in the public docket for
                this rulemaking.
                Background
                 AD 2023-20-11, Amendment 39-22570 (88 FR 71466, October 17, 2023),
                requires replacement of the high-pressure compressor (HPC) rear hub
                with a part eligible for installation for certain IAE LLC Model
                PW1124G1-JM, PW1127G-JM, PW1127GA-JM, PW1129G-JM, PW1130G-JM, PW1133G-
                JM, and PW1133GA-JM engines.
                Need for Correction
                 As published, paragraph (c) in the regulatory text of AD 2023-20-11
                is incorrect. Paragraph (c) of AD 2023-20-11 refers to part number
                ``30G4008.'' The correct reference is part number ``30G4008 or
                30G8208.''
                Related Service Information Under 1 CFR Part 51
                 The FAA reviewed Pratt & Whitney Service Bulletin PW1000G-C-72-00-
                0209-00A-930A-D, Issue No: 002, dated June 20, 2023, which provides the
                list of affected serial numbers for the HPC rear hub.
                 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 ADDRESSES.
                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 November 1, 2023.
                [[Page 74025]]
                 Since this action only corrects the mention of an affected part
                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 adding the following airworthiness
                directive:
                2023-20-11 International Aero Engines, LLC: Amendment 39-22570;
                Docket No. FAA-2023-1996; Project Identifier AD-2022-01361-E.
                (a) Effective Date
                 This airworthiness directive (AD) is effective November 1, 2023.
                (b) Affected ADs
                 None.
                (c) Applicability
                 This AD applies to International Aero Engines, LLC Model
                PW1124G1-JM, PW1127G-JM, PW1127GA-JM, PW1129G-JM, PW1130G-JM,
                PW1133G-JM, and PW1133GA-JM engines with an installed high-pressure
                compressor (HPC) rear hub, part number 30G4008 or 30G8208, with a
                serial number (S/N) listed in Table 2 or Table 3 of Pratt & Whitney
                Service Bulletin PW1000G-C-72-00-0209-00A-930A-D, Issue No: 002,
                dated June 20, 2023 (PW1000G-C-72-00-0209-00A-930A-D, Issue No:
                002).
                (d) Subject
                 Joint Aircraft System Component (JASC) Code 7230, Turbine Engine
                Compressor Section.
                (e) Unsafe Condition
                 This AD was prompted by a manufacturer investigation which
                revealed that Maintenance, Repair, and Overhaul shops were
                misinterpreting accepted knife edge coating wear limits. The FAA is
                issuing this AD to prevent heat-induced cracking at the forward and
                aft knife edge seals and uncontained separation of the HPC rear hub.
                The unsafe condition, if not addressed, could result in uncontained
                debris release, damage to the engine, damage to the airplane, in-
                flight shutdown, and loss of the airplane.
                (f) Compliance
                 Comply with this AD within the compliance times specified,
                unless already done.
                (g) Required Actions
                 At the next engine shop visit after the effective date of this
                AD, replace the HPC rear hub with a part eligible for installation.
                (h) Definitions
                 (1) For the purpose of this AD, a ``part eligible for
                installation'' is:
                 (i) Any HPC rear hub with an S/N that does not appear in Table 2
                or Table 3 of PW1000G-C-72-00-0209-00A-930A-D, Issue No: 002; or
                 (ii) Any HPC rear hub that has been serviced in accordance with
                Pratt & Whitney Service Bulletin PW1000G-C-72-00-0209-00A-930A-D
                (any revision).
                 (2) For the purpose of this AD, an ``engine shop visit'' is the
                induction of an engine into the shop for maintenance involving the
                separation of major mating engine flange H. The separation of engine
                flanges solely for the purpose of transportation without subsequent
                engine maintenance does not constitute an engine shop visit.
                (i) Credit for Previous Actions
                 You may take credit for the actions required by paragraph (g) of
                this AD if you performed those actions before the effective date of
                this AD using Pratt & Whitney Service Bulletin PW1000G-C-72-00-0209-
                00A-930A-D, Issue No: 001, dated September 13, 2022.
                (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 local
                Flight Standards District Office, as appropriate. If sending
                information directly to the manager of the AIR-520 Continued
                Operational Safety Branch, send it to the attention of the person
                identified in paragraph (k) of this AD and email to: [email protected].
                 (2) Before using any approved AMOC, notify your appropriate
                principal inspector, or lacking a principal inspector, the manager
                of the local flight standards district office/certificate holding
                district office.
                (k) Related Information
                 For more information about this AD, contact Mark Taylor,
                Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines,
                WA 98198; phone: (781) 238-7229; 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.
                 (i) Pratt & Whitney Service Bulletin PW1000G-C-72-00-0209-00A-
                930A-D, Issue No: 002, dated June 20, 2023.
                 (ii) [Reserved]
                 (3) For Pratt & Whitney service information identified in this
                AD, contact International Aero Engines LLC, 400 Main Street, East
                Hartford, CT 06118; phone: (860) 565-0140; email:
                [email protected]; website: connect.prattwhitney.com.
                 (4) You may view this service information at the FAA,
                Airworthiness Products Section, Operational Safety Branch, 1200
                District Avenue, Burlington, MA 01803. For information on the
                availability of this material at the FAA, call (817) 222-5110.
                 (5) 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 October 25, 2023.
                Caitlin Locke,
                Director, Compliance & Airworthiness Division, Aircraft Certification
                Service.
                [FR Doc. 2023-23929 Filed 10-26-23; 11:15 am]
                BILLING CODE 4910-13-P
                

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