Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes, 50241-50245 [2024-12551]

Download as PDF 50241 Proposed Rules Federal Register Vol. 89, No. 115 Thursday, June 13, 2024 This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The purpose of these notices is to give interested persons an opportunity to participate in the rule making prior to the adoption of the final rules. Federal Aviation Administration James Blyn, Product Policy Management: Airplanes, GA, Emerging Aircraft, and Rotorcraft AIR–62B, Policy and Standards Division, Aircraft Certification Service, Federal Aviation Administration, 10101 Hillwood Parkway, Fort Worth, Texas 76177; telephone (817) 222–5762; email james.blyn@faa.gov. SUPPLEMENTARY INFORMATION: 14 CFR Part 21 Background [Docket No. FAA–2024–1656] Powered-lift are heavier-than-air aircraft capable of vertical takeoff, vertical landing, and low speed flight that depends principally on enginedriven lift devices or engine thrust for lift during these flight regimes and on nonrotating airfoil(s) for lift during horizontal flight. Powered-lift designs vary in size, capability, and performance. These aircraft are intended to perform a wide variety of operations such as urban air mobility, flight training, air ambulance, search and rescue, external-load/utility, firefighting, electronic newsgathering, air tours, and private use. Recognizing that advancements in technology have the potential to enhance safety and recognizing the broad variations in the population of normal category aircraft, the FAA reviewed the safety continuum policies for both normal category airplanes and normal category rotorcraft and developed this proposed policy statement, which applies the FAA’s safety continuum concept to the certification of powered-lift. This proposed policy would provide a balanced approach between the risk and safety benefits for certificating such aircraft. This policy establishes certification levels for powered-lift and establishes a graduated scale of compliance standards for the certification of these aircraft. These certification levels are based on aircraft maximum gross weight, maximum passenger seating configuration, and type of operation (general aviation vs. passenger transportation for compensation or hire) and are used to establish the safety objectives for system safety and aircraft performance. DEPARTMENT OF TRANSPORTATION Draft Policy Statement Regarding Safety Continuum for Powered-Lift Federal Aviation Administration (FAA), DOT. ACTION: Notification of availability; request for comments. AGENCY: The FAA invites public comment on the agency’s draft policy statement that establishes a safety continuum for the certification of powered-lift. DATES: Comments must be received on or before August 12, 2024. ADDRESSES: Send comments identified with ‘‘Safety Continuum for Poweredlift’’ and docket number FAA–2024– 1656, using any of the following methods: • Federal eRulemaking Portal: Go to www.regulations.gov and follow the instructions for submitting comments electronically. • Mail: Send comments to Docket Operations, M–30; U.S. Department of Transportation (DOT), 1200 New Jersey Avenue SE, Room W12–140, West Building Ground Floor, Washington, DC 20590–0001. • Hand Delivery or Courier: Take comments to Docket Operations in Room W12–140 of the West Building Ground Floor at 1200 New Jersey Avenue SE, Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. • Fax: Fax comments to Docket Operations at (202) 493–2251. Privacy: The FAA will post all comments it receives without change to www.regulations.gov, including any personal information the commenter provides. DOT’s complete Privacy Act Statement can be found in the Federal Register published on April 11, 2000 (65 FR 19477–19478), as well as at DocketsInfo.dot.gov. SUMMARY: lotter on DSK11XQN23PROD with PROPOSALS1 FOR FURTHER INFORMATION CONTACT: VerDate Sep<11>2014 16:20 Jun 12, 2024 Jkt 262001 Comments Invited The FAA invites the public to submit comments on the draft policy statement as specified in the ADDRESSES section. PO 00000 Frm 00001 Fmt 4702 Sfmt 4702 Commenters should include the subject line ‘‘Safety Continuum for Poweredlift’’ and docket number FAA–2024– 1656 on all comments submitted to the FAA. The most helpful comments will reference a specific portion of the draft document, explain the reason for any recommended change, and include supporting data. The FAA will also consider all comments received on or before the closing date before issuing the final policy statement. The FAA will also consider late filed comments if it is possible to do so without incurring expense or delay. You may examine the draft policy statement on the agency’s public website and in the docket as follows: • At www.regulations.gov in Docket FAA–2024–1656. • At www.faa.gov/aircraft/draft_docs/ . Issued in Washington, DC, on June 7, 2024. Daniel J. Elgas, Director, Policy and Standards Division, Aircraft Certification Service. [FR Doc. 2024–12860 Filed 6–12–24; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2024–1482; Project Identifier MCAI–2024–00135–T] RIN 2120–AA64 Airworthiness Directives; ATR–GIE Avions de Transport Régional Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: The FAA proposes to supersede Airworthiness Directive (AD) 2023–02–08, which applies to certain ATR–GIE Avions de Transport Régional Model ATR42–500 airplanes. AD 2023– 02–08 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2023–02–08, the FAA has determined that new or more restrictive airworthiness limitations are necessary. This proposed AD would continue to require certain SUMMARY: E:\FR\FM\13JNP1.SGM 13JNP1 lotter on DSK11XQN23PROD with PROPOSALS1 50242 Federal Register / Vol. 89, No. 115 / Thursday, June 13, 2024 / Proposed Rules actions in AD 2023–02–08 and would require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference (IBR). The FAA is proposing this AD to address the unsafe condition on these products. DATES: The FAA must receive comments on this proposed AD by July 29, 2024. 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–2024–1482; 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 NPRM, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The street address for Docket Operations is listed above. Material Incorporated by Reference: • For EASA material, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; website easa.europa.eu. You may find this material on the EASA website ad.easa.europa.eu. • You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th Street, 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–2024–1482. FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206–231–3220; email shahram.daneshmandi@faa.gov. SUPPLEMENTARY INFORMATION: Comments Invited The FAA invites you to send any written relevant data, views, or VerDate Sep<11>2014 16:20 Jun 12, 2024 Jkt 262001 arguments about this proposal. Send your comments to an address listed under ADDRESSES. Include ‘‘Docket No. FAA–2024–1482; Project Identifier MCAI–2024–00135–T’’ at the beginning of your comments. The most helpful comments reference a specific portion of the proposal, 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 proposal 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 NPRM. 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 NPRM 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 NPRM, 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 NPRM. Submissions containing CBI should be sent to Shahram Daneshmandi, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206– 231–3220; email shahram.daneshmandi@faa.gov. Any commentary that the FAA receives that is not specifically designated as CBI will be placed in the public docket for this rulemaking. Background The FAA issued AD 2023–02–08, Amendment 39–22315 (88 FR 7867, February 7, 2023) (AD 2023–02–08), for certain ATR–GIE Avions de Transport Régional Model ATR42–500 airplanes. AD 2023–02–08 was prompted by an MCAI originated by EASA, which is the Technical Agent for the Member States of the European Union. EASA issued AD 2022–0200, dated September 26, 2022 (EASA AD 2022–0200) (which PO 00000 Frm 00002 Fmt 4702 Sfmt 4702 corresponds to FAA AD 2023–02–08), to correct an unsafe condition. AD 2023–02–08 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. The FAA issued AD 2023– 02–08 to prevent reduced structural integrity of the airplane. Actions Since AD 2023–02–08 Was Issued Since the FAA issued AD 2023–02– 08, EASA superseded AD 2022–0200 and issued EASA AD 2024–0052, dated February 23, 2024 (EASA AD 2024– 0052) (referred to after this as the MCAI), for all ATR–400 and ATR–500 airplanes. Model ATR–400 airplanes are not certificated by the FAA and are not included on the U.S. type certificate data sheet; this proposed AD therefore does not include those airplanes in the applicability. The MCAI states that new or more restrictive airworthiness limitations have been developed. Airplanes with an original airworthiness certificate or original export certificate of airworthiness issued after October 16, 2023, must comply with the airworthiness limitations specified as part of the approved type design and referenced on the type certificate data sheet; this proposed AD therefore does not include those airplanes in the applicability. The FAA is proposing this AD to address among other things, fatigue cracking and damage in principal structural elements. The unsafe condition, if not addressed, could result in reduced structural integrity of the airplane. You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA–2024–1482. Related Service Information Under 1 CFR Part 51 The FAA reviewed EASA AD 2024– 0052 that revises the ATR42–400/-500 Time Limits Document and incorporates EASA AD 2020–0249R1, which required a repetitive operational test for discrepancies of the stall warning system and stick pusher in the flight configuration for ATR–GIE Avions de Transport Régional Model ATR42–500 and ATR72 airplanes. This service information specifies new or more restrictive airworthiness limitations for airplane structures and safe life limits. EASA AD 2020–0249R1 revises EASA AD 2020–0249, which corresponds to FAA AD 2020–26–17, Amendment 39– 21372 (85 FR 81795, December 17, 2020) (AD 2020–26–17). This proposed AD would also require EASA AD 2022–0200, which the Director of the Federal Register E:\FR\FM\13JNP1.SGM 13JNP1 Federal Register / Vol. 89, No. 115 / Thursday, June 13, 2024 / Proposed Rules approved for incorporation by reference as of March 14, 2023 (88 FR 7867, February 7, 2023). 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. FAA’s Determination This product has been approved by the aviation authority of another country and is approved for operation in the United States. Pursuant to the FAA’s bilateral agreement with this State of Design Authority, it has notified the FAA of the unsafe condition described in the MCAI referenced above. The FAA is issuing this NPRM after determining that the unsafe condition described previously is likely to exist or develop in other products of the same type design. lotter on DSK11XQN23PROD with PROPOSALS1 Proposed AD Requirements in This NPRM This proposed AD would retain all requirements of AD 2023–02–08. This proposed AD would require revising the existing maintenance or inspection program, as applicable, to incorporate additional new or more restrictive airworthiness limitations, which are specified in EASA AD 2024–0052 described previously, except for any differences identified as exceptions in the regulatory text of this proposed AD. This proposed AD would require revisions to certain operator maintenance documents to include new actions (e.g., inspections) and Critical Design Configuration Control Limitations (CDCCLs). Compliance with these actions and CDCCLs is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by this proposed AD, the operator may not be able to accomplish the actions described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of compliance (AMOC) according to paragraph (n)(1) of this proposed AD. Explanation of Required Compliance Information In the FAA’s ongoing efforts to improve the efficiency of the AD process, the FAA developed a process to use some civil aviation authority (CAA) ADs as the primary source of information for compliance with requirements for corresponding FAA ADs. The FAA has been coordinating this process with manufacturers and CAAs. As a result, the FAA proposes to retain the IBR of EASA AD 2022–0200 VerDate Sep<11>2014 16:20 Jun 12, 2024 Jkt 262001 and incorporate EASA AD 2024–0052 by reference in the FAA final rule. This proposed AD would, therefore, require compliance with EASA AD 2022–0200 and EASA AD 2024–0052 through that incorporation, except for any differences identified as exceptions in the regulatory text of this proposed AD. Using common terms that are the same as the heading of a particular section in EASA AD 2022–0200 and EASA AD 2024–0052 does not mean that operators need comply only with that section. For example, where the AD requirement refers to ‘‘all required actions and compliance times,’’ compliance with this AD requirement is not limited to the section titled ‘‘Required Action(s) and Compliance Time(s)’’ in EASA AD 2022–0200 and EASA AD 2024–0052. Service information required by EASA AD 2022–0200 and EASA AD 2024– 0052 for compliance will be available at regulations.gov by searching for and locating Docket No. FAA–2024–1482 after the FAA final rule is published. Airworthiness Limitation ADs Using the New Process The FAA’s process of incorporating by reference MCAI ADs as the primary source of information for compliance with corresponding FAA ADs has been limited to certain MCAI ADs (primarily those with service bulletins as the primary source of information for accomplishing the actions required by the FAA AD). However, the FAA is now expanding the process to include MCAI ADs that require a change to airworthiness limitation documents, such as airworthiness limitation sections. For these ADs that incorporate by reference an MCAI AD that changes airworthiness limitations, the FAA requirements are unchanged. Operators must revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in the new airworthiness limitation document. The airworthiness limitations must be followed according to 14 CFR 91.403(c) and 91.409(e). The previous format of the airworthiness limitation ADs included a paragraph that specified that no alternative actions (e.g., inspections), intervals, or CDCCLs may be used unless the actions, intervals, and CDCCLs are approved as an AMOC in accordance with the procedures specified in the AMOCs paragraph under ‘‘Additional AD Provisions.’’ This new format includes a ‘‘New Provisions for Alternative Actions, Intervals, and CDCCLs’’ paragraph that does not specifically refer to AMOCs, but operators may still request an AMOC to PO 00000 Frm 00003 Fmt 4702 Sfmt 4702 50243 use an alternative action, interval, or CDCCL. Costs of Compliance The FAA estimates that this AD, if adopted as proposed, would affect 17 airplanes of U.S. registry. The FAA estimates the following costs to comply with this proposed AD: The FAA estimates the total cost per operator for the retained actions from AD 2023–02–08 to be $7,650 (90 workhours × $85 per work-hour). The FAA has determined that revising the existing maintenance or inspection program takes an average of 90 workhours per operator, although the agency recognizes that this number may vary from operator to operator. Since operators incorporate maintenance or inspection program changes for their affected fleet(s), the FAA has determined that a per-operator estimate is more accurate than a per-airplane estimate. The FAA estimates the total cost per operator for the new proposed actions to be $7,650 (90 work-hours × $85 per work-hour). Authority for This Rulemaking Title 49 of the United States Code specifies the FAA’s authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency’s authority. The FAA is issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: General requirements. Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings The FAA determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify this proposed regulation: E:\FR\FM\13JNP1.SGM 13JNP1 50244 Federal Register / Vol. 89, No. 115 / Thursday, June 13, 2024 / Proposed Rules (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866, (2) Would not affect intrastate aviation in Alaska, and (3) Would not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 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 [Amended] 2. The FAA amends § 39.13 by: a. Removing airworthiness directive 2023–02–08, Amendment 39–22315 (88 FR 7867, February 7, 2023); and ■ b. Adding the following new airworthiness directive: ■ ■ ATR–GIE Avions de Transport Régional: Docket No. FAA–2024–1482; Project Identifier MCAI–2024–00135–T. (a) Comments Due Date The FAA must receive comments on this airworthiness directive (AD) by July 29, 2024. (b) Affected ADs This AD replaces AD 2023–02–08, Amendment 39–22315 (88 FR 7867, February 7, 2023) (AD 2023–02–08). This AD affects AD 2020–26–17, Amendment 39–21372 (85 FR 81795, December 17, 2020) (AD 2020–26–17). (c) Applicability This AD applies to ATR–GIE Avions de Transport Régional Model ATR42–500 airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before October 16, 2023. lotter on DSK11XQN23PROD with PROPOSALS1 (d) Subject Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks. (e) Unsafe Condition This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address among other things, fatigue cracking and damage in principal structural elements. The unsafe condition, if not addressed, could result in reduced structural integrity of the airplane. VerDate Sep<11>2014 16:20 Jun 12, 2024 Jkt 262001 (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Retained Revision of the Existing Maintenance or Inspection Program, With a New Terminating Action This paragraph restates the requirements of paragraph (j) of AD 2023–02–08, with a new terminating action. For airplanes with an original airworthiness certificate or original export certificate of airworthiness dated on or before July 29, 2022: Except as specified in paragraph (h) of this AD, comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2022–0200, dated September 26, 2022 (EASA AD 2022–0200). Accomplishing the revision of the existing maintenance or inspection program required by paragraph (j) of this AD terminates the requirements of this paragraph. (h) Retained Exceptions to EASA AD 2022– 0200, With No Changes This paragraph restates the exceptions specified in paragraph (k) of AD 2023–02–08, with no changes. (1) The requirements specified in paragraph (1) and (2) of EASA AD 2022–0200 do not apply to this AD. (2) Paragraph (3) of EASA AD 2022–0200 specifies revising ‘‘the approved AMP’’ within 12 months after its effective date, but this AD requires revising the existing maintenance or inspection program, as applicable, within 90 days after March 14, 2023 (the effective date of AD 2023–02–08). (3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2022–0200 is at the applicable ‘‘limitations’’ and ‘‘associated thresholds’’ as incorporated by the requirements of paragraph (3) of EASA AD 2022–0200, or within 90 days after March 14, 2023 (the effective date of AD 2023–02–08), whichever occurs later. (4) The provisions specified in paragraphs (4) and (5) of EASA AD 2022–0200 do not apply to this AD. (5) The ‘‘Remarks’’ section of EASA AD 2022–0200 does not apply to this AD. (i) Retained Restrictions on Alternative Actions, Intervals, and Critical Design Configuration Control Limitations (CDCCLs), With New Exception This paragraph restates the requirements of paragraph (l) of AD 2023–02–08, with a new exception. Except as required by paragraph (j) of this AD, after the maintenance or inspection program has been revised as required by paragraph (g) of this AD, no alternative actions (e.g., inspections), intervals, and CDCCLs are allowed unless they are approved as specified in the provisions of the ‘‘Ref. Publications’’ section of EASA AD 2022–0200. (j) New Revision of the Existing Maintenance or Inspection Program Except as specified in paragraph (k) of this AD: Comply with all required actions and compliance times specified in, and in PO 00000 Frm 00004 Fmt 4702 Sfmt 4702 accordance with, EASA AD 2024–0052, dated February 23, 2024 (EASA AD 2024– 0052). Accomplishing the revision of the existing maintenance or inspection program required by this paragraph terminates the requirements of paragraph (g) of this AD. (k) Exceptions to EASA AD 2024–0052 (1) This AD does not adopt the requirements specified in paragraphs (1) and (2) of EASA AD 2024–0052. (2) Paragraph (3) of EASA AD 2024–0052 specifies revising ‘‘the approved AMP,’’ within 12 months after its effective date, but this AD requires revising the existing maintenance or inspection program, as applicable, within 90 days after the effective date of this AD. (3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2024–0052 is at the applicable ‘‘limitations’’ and ‘‘associated thresholds’’ as incorporated by the requirements of paragraph (3) of EASA AD 2024–0052, or within 90 days after the effective date of this AD, whichever occurs later. (4) This AD does not adopt the provisions specified in paragraphs (4) and (5) of EASA AD 2024–0052. (5) This AD does not adopt the ‘‘Remarks’’ section of EASA AD 2024–0052. (l) New Provisions for Alternative Actions, Intervals, and Critical Design Configuration Control Limitations (CDCCLs) After the existing maintenance or inspection program has been revised as required by paragraph (j) of this AD, no alternative actions (e.g., inspections), intervals, and CDCCLs are allowed unless they are approved as specified in the provisions of the ‘‘Ref. Publications’’ section of EASA AD 2024–0052. (m) Terminating Action for Certain Tasks Required by AD 2020–26–17 For Model ATR42–500 airplanes only: Accomplishing the actions required by this AD terminates the corresponding requirements of AD 2020–26–17 for the tasks identified in the service information referenced in EASA AD 2024–0052 only. (n) Additional AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, 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 manager of the International Validation Branch, mail it to the address identified in paragraph (o) of this AD. Information may be emailed to: 9-AVS-AIR-730-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 E:\FR\FM\13JNP1.SGM 13JNP1 Federal Register / Vol. 89, No. 115 / Thursday, June 13, 2024 / Proposed Rules by the Manager, International Validation Branch, FAA; or EASA; or ATR–GIE Avions de Transport Régional’s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (o) Additional Information For more information about this AD, contact Shahram Daneshmandi, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206–231–3220; email shahram.daneshmandi@faa.gov. (p) 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 [DATE 35 DAYS AFTER PUBLICATION OF THE FINAL RULE]. (i) European Union Aviation Safety Agency (EASA) AD 2024–0052, dated February 23, 2024. (ii) [Reserved] (4) The following service information was approved for IBR on March 14, 2023 (88 FR 7867, February 7, 2023). (i) EASA AD 2022–0200, dated September 26, 2022. (ii) [Reserved] (5) For EASA AD 2024–0052 and EASA AD 2022–0200, contact EASA, KonradAdenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@ easa.europa.eu; website easa.europa.eu. You may find these EASA ADs on the EASA website ad.easa.europa.eu. (6) You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th Street, Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. (7) 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. lotter on DSK11XQN23PROD with PROPOSALS1 Issued on June 4, 2024. Victor Wicklund, Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2024–12551 Filed 6–12–24; 8:45 am] BILLING CODE 4910–13–P VerDate Sep<11>2014 16:20 Jun 12, 2024 Jkt 262001 ENVIRONMENTAL PROTECTION AGENCY 40 CFR Part 52 [EPA–R09–OAR–2023–0539; FRL–11747– 01–R9] Partial Approval and Partial Disapproval of Air Quality State Implementation Plans; Arizona; Infrastructure Requirements for Fine Particulate Matter Environmental Protection Agency (EPA). ACTION: Proposed rule. AGENCY: The Environmental Protection Agency (EPA) is proposing to partially approve and partially disapprove a revision to the Arizona state implementation plan (SIP) as meeting the requirements of the Clean Air Act (CAA) for the implementation, maintenance, and enforcement of the 2012 fine particulate matter (PM2.5) national ambient air quality standards (NAAQS or ‘‘standards’’). As part of this action, the EPA is proposing to approve regulatory provisions into the Arizona SIP. The EPA is seeking public comment on this proposed action and will accept comments from the public on this proposal for the next 30 days. DATES: Any comments must arrive by July 15, 2024. ADDRESSES: Submit your comments, identified by Docket ID No. EPA–R09– OAR–2023–0539 at https:// www.regulations.gov. For comments submitted at Regulations.gov, follow the online instructions for submitting comments. Once submitted, comments cannot be edited or removed from Regulations.gov. The EPA may publish any comment received to its public docket. Do not submit electronically any information you consider to be Confidential Business Information (CBI) or other information whose disclosure is restricted by statute. Multimedia submissions (audio, video, etc.) must be accompanied by a written comment. The written comment is considered the official comment and should include discussion of all points you wish to make. The EPA will generally not consider comments or comment contents located outside of the primary submission (i.e., on the web, cloud, or other file sharing system). For additional submission methods, please contact the person identified in the FOR FURTHER INFORMATION CONTACT section. For the full EPA public comment policy, information about CBI or multimedia submissions, and general guidance on making effective comments, please visit https://www.epa.gov/dockets/ SUMMARY: PO 00000 Frm 00005 Fmt 4702 Sfmt 4702 50245 commenting-epa-dockets. If you need assistance in a language other than English or if you are a person with a disability who needs a reasonable accommodation at no cost to you, please contact the person identified in the FOR FURTHER INFORMATION CONTACT section. FOR FURTHER INFORMATION CONTACT: Michael Dorantes, Geographic Strategies and Modeling Section (AIR–2–2), EPA Region IX, (415) 972–3934, dorantes.michael@epa.gov. SUPPLEMENTARY INFORMATION: Throughout this document, ‘‘we,’’ ‘‘us,’’ and ‘‘our’’ refer to the EPA. Table of Contents I. The EPA’s Approach To Reviewing Infrastructure SIPs II. Background A. Statutory Framework B. Regulatory Background III. State Submittals A. Infrastructure SIP Submittal B. Revised Rules and Regulations IV. The EPA’s Evaluation and Proposed Action A. Proposed Approvals and Partial Approvals B. Proposed Partial Disapprovals C. Incorporation of Rules Into Arizona’s State Implementation Plan D. Deferred Action E. Revising Air Quality Control Regions and Evaluating Emergency Episode Planning Requirements for PM2.5 in Arizona F. Request for Public Comments V. Incorporation by Reference VI. Statutory and Executive Order Reviews I. The EPA’s Approach To Reviewing Infrastructure SIPs The EPA has historically referred to SIP submittals made for the purpose of satisfying the requirements of CAA sections 110(a)(1) and 110(a)(2) as ‘‘infrastructure SIP’’ submittals. Although the term ‘‘infrastructure SIP’’ does not appear in the CAA, the EPA uses the term to distinguish this particular type of SIP submittal from submittals that are intended to satisfy other SIP requirements under the CAA, such as ‘‘nonattainment SIP’’ or ‘‘attainment SIP’’ submittals to address the nonattainment planning requirements of CAA title I part D, ‘‘regional haze SIP’’ submittals required by EPA rule to address the visibility protection requirements of section 169A, and nonattainment new source review (NSR) permit program submittals to address the permit requirements of CAA title I part D. Section 110(a)(1) of the Act requires that each State adopt and submit an infrastructure SIP for the implementation, maintenance, and enforcement of each NAAQS promulgated by the EPA, and that the E:\FR\FM\13JNP1.SGM 13JNP1

Agencies

[Federal Register Volume 89, Number 115 (Thursday, June 13, 2024)]
[Proposed Rules]
[Pages 50241-50245]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-12551]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-1482; Project Identifier MCAI-2024-00135-T]
RIN 2120-AA64


Airworthiness Directives; ATR-GIE Avions de Transport 
R[eacute]gional Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD) 
2023-02-08, which applies to certain ATR-GIE Avions de Transport 
R[eacute]gional Model ATR42-500 airplanes. AD 2023-02-08 requires 
revising the existing maintenance or inspection program, as applicable, 
to incorporate new or more restrictive airworthiness limitations. Since 
the FAA issued AD 2023-02-08, the FAA has determined that new or more 
restrictive airworthiness limitations are necessary. This proposed AD 
would continue to require certain

[[Page 50242]]

actions in AD 2023-02-08 and would require revising the existing 
maintenance or inspection program, as applicable, to incorporate new or 
more restrictive airworthiness limitations, as specified in a European 
Union Aviation Safety Agency (EASA) AD, which is proposed for 
incorporation by reference (IBR). The FAA is proposing this AD to 
address the unsafe condition on these products.

DATES: The FAA must receive comments on this proposed AD by July 29, 
2024.

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-2024-1482; 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 NPRM, the mandatory continuing airworthiness 
information (MCAI), any comments received, and other information. The 
street address for Docket Operations is listed above.
    Material Incorporated by Reference:
     For EASA material, contact EASA, Konrad-Adenauer-Ufer 3, 
50668 Cologne, Germany; telephone +49 221 8999 000; email 
[email protected]; website easa.europa.eu. You may find this material 
on the EASA website ad.easa.europa.eu.
     You may view this material at the FAA, Airworthiness 
Products Section, Operational Safety Branch, 2200 South 216th Street, 
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-2024-1482.

FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aviation Safety 
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; 
telephone 206-231-3220; email [email protected].

SUPPLEMENTARY INFORMATION:

Comments Invited

    The FAA invites you to send any written relevant data, views, or 
arguments about this proposal. Send your comments to an address listed 
under ADDRESSES. Include ``Docket No. FAA-2024-1482; Project Identifier 
MCAI-2024-00135-T'' at the beginning of your comments. The most helpful 
comments reference a specific portion of the proposal, 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 proposal 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 NPRM.

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 NPRM 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 NPRM, 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 NPRM. Submissions containing CBI should be sent to 
Shahram Daneshmandi, Aviation Safety Engineer, FAA, 1600 Stewart 
Avenue, Suite 410, Westbury, NY 11590; telephone 206-231-3220; email 
[email protected]. Any commentary that the FAA receives that 
is not specifically designated as CBI will be placed in the public 
docket for this rulemaking.

Background

    The FAA issued AD 2023-02-08, Amendment 39-22315 (88 FR 7867, 
February 7, 2023) (AD 2023-02-08), for certain ATR-GIE Avions de 
Transport R[eacute]gional Model ATR42-500 airplanes. AD 2023-02-08 was 
prompted by an MCAI originated by EASA, which is the Technical Agent 
for the Member States of the European Union. EASA issued AD 2022-0200, 
dated September 26, 2022 (EASA AD 2022-0200) (which corresponds to FAA 
AD 2023-02-08), to correct an unsafe condition.
    AD 2023-02-08 requires revising the existing maintenance or 
inspection program, as applicable, to incorporate new or more 
restrictive airworthiness limitations. The FAA issued AD 2023-02-08 to 
prevent reduced structural integrity of the airplane.

Actions Since AD 2023-02-08 Was Issued

    Since the FAA issued AD 2023-02-08, EASA superseded AD 2022-0200 
and issued EASA AD 2024-0052, dated February 23, 2024 (EASA AD 2024-
0052) (referred to after this as the MCAI), for all ATR-400 and ATR-500 
airplanes. Model ATR-400 airplanes are not certificated by the FAA and 
are not included on the U.S. type certificate data sheet; this proposed 
AD therefore does not include those airplanes in the applicability. The 
MCAI states that new or more restrictive airworthiness limitations have 
been developed.
    Airplanes with an original airworthiness certificate or original 
export certificate of airworthiness issued after October 16, 2023, must 
comply with the airworthiness limitations specified as part of the 
approved type design and referenced on the type certificate data sheet; 
this proposed AD therefore does not include those airplanes in the 
applicability.
    The FAA is proposing this AD to address among other things, fatigue 
cracking and damage in principal structural elements. The unsafe 
condition, if not addressed, could result in reduced structural 
integrity of the airplane. You may examine the MCAI in the AD docket at 
regulations.gov under Docket No. FAA-2024-1482.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed EASA AD 2024-0052 that revises the ATR42-400/-500 
Time Limits Document and incorporates EASA AD 2020-0249R1, which 
required a repetitive operational test for discrepancies of the stall 
warning system and stick pusher in the flight configuration for ATR-GIE 
Avions de Transport R[eacute]gional Model ATR42-500 and ATR72 
airplanes. This service information specifies new or more restrictive 
airworthiness limitations for airplane structures and safe life limits. 
EASA AD 2020-0249R1 revises EASA AD 2020-0249, which corresponds to FAA 
AD 2020-26-17, Amendment 39-21372 (85 FR 81795, December 17, 2020) (AD 
2020-26-17).
    This proposed AD would also require EASA AD 2022-0200, which the 
Director of the Federal Register

[[Page 50243]]

approved for incorporation by reference as of March 14, 2023 (88 FR 
7867, February 7, 2023).
    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.

FAA's Determination

    This product has been approved by the aviation authority of another 
country and is approved for operation in the United States. Pursuant to 
the FAA's bilateral agreement with this State of Design Authority, it 
has notified the FAA of the unsafe condition described in the MCAI 
referenced above. The FAA is issuing this NPRM after determining that 
the unsafe condition described previously is likely to exist or develop 
in other products of the same type design.

Proposed AD Requirements in This NPRM

    This proposed AD would retain all requirements of AD 2023-02-08. 
This proposed AD would require revising the existing maintenance or 
inspection program, as applicable, to incorporate additional new or 
more restrictive airworthiness limitations, which are specified in EASA 
AD 2024-0052 described previously, except for any differences 
identified as exceptions in the regulatory text of this proposed AD.
    This proposed AD would require revisions to certain operator 
maintenance documents to include new actions (e.g., inspections) and 
Critical Design Configuration Control Limitations (CDCCLs). Compliance 
with these actions and CDCCLs is required by 14 CFR 91.403(c). For 
airplanes that have been previously modified, altered, or repaired in 
the areas addressed by this proposed AD, the operator may not be able 
to accomplish the actions described in the revisions. In this 
situation, to comply with 14 CFR 91.403(c), the operator must request 
approval for an alternative method of compliance (AMOC) according to 
paragraph (n)(1) of this proposed AD.

Explanation of Required Compliance Information

    In the FAA's ongoing efforts to improve the efficiency of the AD 
process, the FAA developed a process to use some civil aviation 
authority (CAA) ADs as the primary source of information for compliance 
with requirements for corresponding FAA ADs. The FAA has been 
coordinating this process with manufacturers and CAAs. As a result, the 
FAA proposes to retain the IBR of EASA AD 2022-0200 and incorporate 
EASA AD 2024-0052 by reference in the FAA final rule. This proposed AD 
would, therefore, require compliance with EASA AD 2022-0200 and EASA AD 
2024-0052 through that incorporation, except for any differences 
identified as exceptions in the regulatory text of this proposed AD. 
Using common terms that are the same as the heading of a particular 
section in EASA AD 2022-0200 and EASA AD 2024-0052 does not mean that 
operators need comply only with that section. For example, where the AD 
requirement refers to ``all required actions and compliance times,'' 
compliance with this AD requirement is not limited to the section 
titled ``Required Action(s) and Compliance Time(s)'' in EASA AD 2022-
0200 and EASA AD 2024-0052. Service information required by EASA AD 
2022-0200 and EASA AD 2024-0052 for compliance will be available at 
regulations.gov by searching for and locating Docket No. FAA-2024-1482 
after the FAA final rule is published.

Airworthiness Limitation ADs Using the New Process

    The FAA's process of incorporating by reference MCAI ADs as the 
primary source of information for compliance with corresponding FAA ADs 
has been limited to certain MCAI ADs (primarily those with service 
bulletins as the primary source of information for accomplishing the 
actions required by the FAA AD). However, the FAA is now expanding the 
process to include MCAI ADs that require a change to airworthiness 
limitation documents, such as airworthiness limitation sections.
    For these ADs that incorporate by reference an MCAI AD that changes 
airworthiness limitations, the FAA requirements are unchanged. 
Operators must revise the existing maintenance or inspection program, 
as applicable, to incorporate the information specified in the new 
airworthiness limitation document. The airworthiness limitations must 
be followed according to 14 CFR 91.403(c) and 91.409(e).
    The previous format of the airworthiness limitation ADs included a 
paragraph that specified that no alternative actions (e.g., 
inspections), intervals, or CDCCLs may be used unless the actions, 
intervals, and CDCCLs are approved as an AMOC in accordance with the 
procedures specified in the AMOCs paragraph under ``Additional AD 
Provisions.'' This new format includes a ``New Provisions for 
Alternative Actions, Intervals, and CDCCLs'' paragraph that does not 
specifically refer to AMOCs, but operators may still request an AMOC to 
use an alternative action, interval, or CDCCL.

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would 
affect 17 airplanes of U.S. registry. The FAA estimates the following 
costs to comply with this proposed AD:
    The FAA estimates the total cost per operator for the retained 
actions from AD 2023-02-08 to be $7,650 (90 work-hours x $85 per work-
hour).
    The FAA has determined that revising the existing maintenance or 
inspection program takes an average of 90 work-hours per operator, 
although the agency recognizes that this number may vary from operator 
to operator. Since operators incorporate maintenance or inspection 
program changes for their affected fleet(s), the FAA has determined 
that a per-operator estimate is more accurate than a per-airplane 
estimate.
    The FAA estimates the total cost per operator for the new proposed 
actions to be $7,650 (90 work-hours x $85 per work-hour).

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to 
issue rules on aviation safety. Subtitle I, section 106, describes the 
authority of the FAA Administrator. Subtitle VII: Aviation Programs, 
describes in more detail the scope of the Agency's authority.
    The FAA is issuing this rulemaking under the authority described in 
Subtitle VII, Part A, Subpart III, Section 44701: General requirements. 
Under that section, Congress charges the FAA with promoting safe flight 
of civil aircraft in air commerce by prescribing regulations for 
practices, methods, and procedures the Administrator finds necessary 
for safety in air commerce. This regulation is within the scope of that 
authority because it addresses an unsafe condition that is likely to 
exist or develop on products identified in this rulemaking action.

Regulatory Findings

    The FAA determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would not 
have a substantial direct effect on the States, on the relationship 
between the national Government and the States, or on the distribution 
of power and responsibilities among the various levels of government.
    For the reasons discussed above, I certify this proposed 
regulation:

[[Page 50244]]

    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Would not affect intrastate aviation in Alaska, and
    (3) Would not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

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

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 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   [Amended]

0
2. The FAA amends Sec.  39.13 by:
0
a. Removing airworthiness directive 2023-02-08, Amendment 39-22315 (88 
FR 7867, February 7, 2023); and
0
b. Adding the following new airworthiness directive:

ATR-GIE Avions de Transport R[eacute]gional: Docket No. FAA-2024-
1482; Project Identifier MCAI-2024-00135-T.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by July 29, 2024.

 (b) Affected ADs

    This AD replaces AD 2023-02-08, Amendment 39-22315 (88 FR 7867, 
February 7, 2023) (AD 2023-02-08).
    This AD affects AD 2020-26-17, Amendment 39-21372 (85 FR 81795, 
December 17, 2020) (AD 2020-26-17).

 (c) Applicability

    This AD applies to ATR-GIE Avions de Transport R[eacute]gional 
Model ATR42-500 airplanes, certificated in any category, with an 
original airworthiness certificate or original export certificate of 
airworthiness issued on or before October 16, 2023.

 (d) Subject

    Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.

 (e) Unsafe Condition

    This AD was prompted by a determination that new or more 
restrictive airworthiness limitations are necessary. The FAA is 
issuing this AD to address among other things, fatigue cracking and 
damage in principal structural elements. The unsafe condition, if 
not addressed, could result in reduced structural integrity of the 
airplane.

 (f) Compliance

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

 (g) Retained Revision of the Existing Maintenance or Inspection 
Program, With a New Terminating Action

    This paragraph restates the requirements of paragraph (j) of AD 
2023-02-08, with a new terminating action. For airplanes with an 
original airworthiness certificate or original export certificate of 
airworthiness dated on or before July 29, 2022: Except as specified 
in paragraph (h) of this AD, comply with all required actions and 
compliance times specified in, and in accordance with, European 
Union Aviation Safety Agency (EASA) AD 2022-0200, dated September 
26, 2022 (EASA AD 2022-0200). Accomplishing the revision of the 
existing maintenance or inspection program required by paragraph (j) 
of this AD terminates the requirements of this paragraph.

 (h) Retained Exceptions to EASA AD 2022-0200, With No Changes

    This paragraph restates the exceptions specified in paragraph 
(k) of AD 2023-02-08, with no changes.
    (1) The requirements specified in paragraph (1) and (2) of EASA 
AD 2022-0200 do not apply to this AD.
    (2) Paragraph (3) of EASA AD 2022-0200 specifies revising ``the 
approved AMP'' within 12 months after its effective date, but this 
AD requires revising the existing maintenance or inspection program, 
as applicable, within 90 days after March 14, 2023 (the effective 
date of AD 2023-02-08).
    (3) The initial compliance time for doing the tasks specified in 
paragraph (3) of EASA AD 2022-0200 is at the applicable 
``limitations'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2022-0200, or within 90 
days after March 14, 2023 (the effective date of AD 2023-02-08), 
whichever occurs later.
    (4) The provisions specified in paragraphs (4) and (5) of EASA 
AD 2022-0200 do not apply to this AD.
    (5) The ``Remarks'' section of EASA AD 2022-0200 does not apply 
to this AD.

 (i) Retained Restrictions on Alternative Actions, Intervals, and 
Critical Design Configuration Control Limitations (CDCCLs), With New 
Exception

    This paragraph restates the requirements of paragraph (l) of AD 
2023-02-08, with a new exception. Except as required by paragraph 
(j) of this AD, after the maintenance or inspection program has been 
revised as required by paragraph (g) of this AD, no alternative 
actions (e.g., inspections), intervals, and CDCCLs are allowed 
unless they are approved as specified in the provisions of the 
``Ref. Publications'' section of EASA AD 2022-0200.

 (j) New Revision of the Existing Maintenance or Inspection Program

    Except as specified in paragraph (k) of this AD: Comply with all 
required actions and compliance times specified in, and in 
accordance with, EASA AD 2024-0052, dated February 23, 2024 (EASA AD 
2024-0052). Accomplishing the revision of the existing maintenance 
or inspection program required by this paragraph terminates the 
requirements of paragraph (g) of this AD.

 (k) Exceptions to EASA AD 2024-0052

    (1) This AD does not adopt the requirements specified in 
paragraphs (1) and (2) of EASA AD 2024-0052.
    (2) Paragraph (3) of EASA AD 2024-0052 specifies revising ``the 
approved AMP,'' within 12 months after its effective date, but this 
AD requires revising the existing maintenance or inspection program, 
as applicable, within 90 days after the effective date of this AD.
    (3) The initial compliance time for doing the tasks specified in 
paragraph (3) of EASA AD 2024-0052 is at the applicable 
``limitations'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2024-0052, or within 90 
days after the effective date of this AD, whichever occurs later.
    (4) This AD does not adopt the provisions specified in 
paragraphs (4) and (5) of EASA AD 2024-0052.
    (5) This AD does not adopt the ``Remarks'' section of EASA AD 
2024-0052.

 (l) New Provisions for Alternative Actions, Intervals, and Critical 
Design Configuration Control Limitations (CDCCLs)

    After the existing maintenance or inspection program has been 
revised as required by paragraph (j) of this AD, no alternative 
actions (e.g., inspections), intervals, and CDCCLs are allowed 
unless they are approved as specified in the provisions of the 
``Ref. Publications'' section of EASA AD 2024-0052.

 (m) Terminating Action for Certain Tasks Required by AD 2020-26-17

    For Model ATR42-500 airplanes only: Accomplishing the actions 
required by this AD terminates the corresponding requirements of AD 
2020-26-17 for the tasks identified in the service information 
referenced in EASA AD 2024-0052 only.

 (n) Additional AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
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 manager of the 
International Validation Branch, mail it to the address identified 
in paragraph (o) 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

[[Page 50245]]

by the Manager, International Validation Branch, FAA; or EASA; or 
ATR-GIE Avions de Transport R[eacute]gional's EASA Design 
Organization Approval (DOA). If approved by the DOA, the approval 
must include the DOA-authorized signature.

 (o) Additional Information

    For more information about this AD, contact Shahram Daneshmandi, 
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, 
Westbury, NY 11590; telephone 206-231-3220; email 
[email protected].

 (p) 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 
[DATE 35 DAYS AFTER PUBLICATION OF THE FINAL RULE].
    (i) European Union Aviation Safety Agency (EASA) AD 2024-0052, 
dated February 23, 2024.
    (ii) [Reserved]
    (4) The following service information was approved for IBR on 
March 14, 2023 (88 FR 7867, February 7, 2023).
    (i) EASA AD 2022-0200, dated September 26, 2022.
    (ii) [Reserved]
    (5) For EASA AD 2024-0052 and EASA AD 2022-0200, contact EASA, 
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 
8999 000; email [email protected]; website easa.europa.eu. You may 
find these EASA ADs on the EASA website ad.easa.europa.eu.
    (6) You may view this material at the FAA, Airworthiness 
Products Section, Operational Safety Branch, 2200 South 216th 
Street, Des Moines, WA. For information on the availability of this 
material at the FAA, call 206-231-3195.
    (7) 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 June 4, 2024.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2024-12551 Filed 6-12-24; 8:45 am]
BILLING CODE 4910-13-P
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