Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes, 74538-74541 [2022-26468]

Download as PDF 74538 Federal Register / Vol. 87, No. 233 / Tuesday, December 6, 2022 / Proposed Rules DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2022–1245; Project Identifier MCAI–2022–00503–T] RIN 2120–AA64 Airworthiness Directives; ATR—GIE Avions de Transport Re´gional Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: The FAA proposes to supersede Airworthiness Directive (AD) 2021–20–09, which applies to certain ATR—GIE Avions de Transport Re´gional Model ATR72 airplanes. AD 2021–20–09 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2021–20–09, the FAA has determined that new or more restrictive tasks and airworthiness limitations are necessary. This proposed AD would continue to require the actions in AD 2021–20–09 and require revising the existing maintenance or inspection program, as applicable, to incorporate additional new or more restrictive tasks and airworthiness limitations, as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference. 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 January 20, 2023. SUMMARY: 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: U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE, Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For EASA material that that is proposed for IBR in this NPRM, contact lotter on DSK11XQN23PROD with PROPOSALS1 ADDRESSES: VerDate Sep<11>2014 17:01 Dec 05, 2022 Jkt 259001 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 at ad.easa.europa.eu. 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 in the AD docket at regulations.gov by searching for and locating Docket No. FAA–2022–1245. Examining the AD Docket You may examine the AD docket at regulations.gov by searching for and locating Docket No. FAA–2022–1245; 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. FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; 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 arguments about this proposal. Send your comments to an address listed under ADDRESSES. Include ‘‘Docket No. FAA–2022–1245; Project Identifier MCAI–2022–00503–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 PO 00000 Frm 00020 Fmt 4702 Sfmt 4702 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, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 206–231–3220; email shahram.daneshmandi@faa.gov. Any commentary that the FAA receives which is not specifically designated as CBI will be placed in the public docket for this rulemaking. Background The FAA issued AD 2021–20–09, Amendment 39–21747 (86 FR 64805, November 19, 2021) (AD 2021–20–09), which applies to certain ATR—GIE Avions de Transport Re´gional Model ATR72–101, –102, –201, –202, –211, –212, and –212A airplanes. AD 2021– 20–09 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. The FAA issued AD 2021–20–09 to address reduced structural integrity of the airplane. Actions Since AD 2021–20–09 Was Issued Since the FAA issued AD 2021–20– 09, the FAA has determined that new or more restrictive tasks and airworthiness limitations are necessary. EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2022–0201, dated September 26, 2022 (EASA AD 2022–0201) (also referred to as the MCAI), to correct an unsafe condition for all ATR—GIE Avions de Transport Re´gional Model ATR72–101, –102, –201, –202, –211, –212, and –212A airplanes. Airplanes with an original airworthiness certificate or original export certificate of airworthiness issued after February 3, 2022, must comply with the airworthiness limitations specified as part of the approved type design and referenced on E:\FR\FM\06DEP1.SGM 06DEP1 Federal Register / Vol. 87, No. 233 / Tuesday, December 6, 2022 / Proposed Rules the type certificate data sheet; this AD therefore does not include those airplanes in the applicability. This proposed AD was prompted by a determination that new or more restrictive tasks and airworthiness limitations are necessary. The FAA is proposing this AD to address fatigue cracking and damage in principal structural elements, which could result in reduced structural integrity of the airplane. See the MCAI for additional background information. 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 (m)(1) of this proposed AD. Related Service Information Under 1 CFR Part 51 EASA AD 2022–0201 describes new or more restrictive tasks, airworthiness limitations for airplane structures, and safe life limits. This proposed AD would also require EASA AD 2021–0020, dated January 15, 2021 (EASA AD 2021–0020), which the Director of the Federal Register approved for incorporation by reference as of December 27, 2021 (86 FR 64805, November 19, 2021). 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 the ADDRESSES section. 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 2021–0020 and incorporate EASA AD 2022–0201 by reference in the FAA final rule. This proposed AD would, therefore, require compliance with EASA AD 2021–0020 and EASA AD 2022–0201 in their entirety 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 2021– 0020 or EASA AD 2022–0201 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 2021–0020 or EASA AD 2022–0201. Service information required by EASA AD 2021–0020 and EASA AD 2022–0201 for compliance will be available at regulations.gov by searching for and locating Docket No. FAA–2022–1245 after the FAA final rule is published. lotter on DSK11XQN23PROD with PROPOSALS1 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 the 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 the requirements of AD 2021–20–09. This proposed AD would also require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive tasks and airworthiness limitations, which are specified in EASA AD 2022– 0201 described previously, as proposed for incorporation by reference. Any differences with EASA AD 2022–0201 are identified as exceptions in the regulatory text of this AD. This proposed AD would require revisions to certain operator maintenance documents to include new actions (e.g., inspections). Compliance with these actions is required by 14 CFR 91.403(c). For airplanes that have been VerDate Sep<11>2014 17:01 Dec 05, 2022 Jkt 259001 Explanation of Required Compliance Information 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. PO 00000 Frm 00021 Fmt 4702 Sfmt 4702 74539 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), or intervals may be used unless the actions and intervals are approved as an AMOC in accordance with the procedures specified in the AMOCs paragraph under ‘‘Additional FAA Provisions.’’ This new format includes a ‘‘New Provisions for Alternative Actions and Intervals’’ paragraph that does not specifically refer to AMOCs, but operators may still request an AMOC to use an alternative action or interval. Costs of Compliance The FAA estimates that this proposed AD affects 23 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 2021–20–09 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 E:\FR\FM\06DEP1.SGM 06DEP1 74540 Federal Register / Vol. 87, No. 233 / Tuesday, December 6, 2022 / Proposed Rules 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: (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 (AD) 2021–20–09, Amendment 39– 21747 (86 FR 64805, November 19, 2021) (AD 2021–20–09); and ■ b. Adding the following new AD: ■ ■ lotter on DSK11XQN23PROD with PROPOSALS1 ATR—GIE Avions de Transport Re´gional: Docket No. FAA–2022–1245; Project Identifier MCAI–2022–00503–T. (a) Comments Due Date The FAA must receive comments on this airworthiness directive (AD) by January 20, 2023. (b) Affected ADs This AD replaces AD 2021–20–09, Amendment 39–21747 (86 FR 64805, November 19, 2021) (AD 2021–20–09). VerDate Sep<11>2014 17:01 Dec 05, 2022 Jkt 259001 (c) Applicability This AD applies to ATR—GIE Avions de Transport Re´gional Model ATR72–101, –102, –201, –202, –211, –212, and –212A airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before February 3, 2022. 2021–0020, or within 90 days after December 27, 2021 (the effective date of AD 2021–20– 09), whichever occurs later. (5) The provisions specified in paragraphs (4) and (5) of EASA AD 2021–0020 do not apply to this AD. (6) The ‘‘Remarks’’ section of EASA AD 2021–0020 does not apply to this AD. (d) Subject Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks. (i) Retained Restrictions on Alternative Actions and Intervals, With a New Exception This paragraph restates the requirements of paragraph (l) of AD 2021–20–09, with a new exception. Except as required by paragraph (j) of this AD, after the existing maintenance or inspection program has been revised as required by paragraph (g) of this AD, no alternative actions (e.g., inspections) and intervals are allowed unless they are approved as specified in the provisions of the ‘‘Ref. Publications’’ section of EASA AD 2021–0020. (e) Unsafe Condition This AD was prompted by a determination that new or more restrictive tasks and airworthiness limitations are necessary. The FAA is issuing this AD to address fatigue cracking and damage in principal structural elements, which 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 No Changes This paragraph restates the requirements of paragraph (j) of AD 2021–20–09, with no changes. For ATR—GIE Avions de Transport Re´gional Model ATR72–101, –102, –201, –202, –211, –212, and –212A airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before October 9, 2020, 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 2021–0020, dated January 15, 2021 (EASA AD 2021–0020). 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 2021– 0020, With No Changes This paragraph restates the requirements of paragraph (k) of AD 2021–20–09, with no changes. (1) Where EASA AD 2021–0020 refers to its effective date, this AD requires using December 27, 2021 (the effective date of AD 2021–20–09). (2) The requirements specified in paragraphs (1) and (2) of EASA AD 2021– 0020 do not apply to this AD. (3) Paragraph (3) of EASA AD 2021–0020 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 December 27, 2021 (the effective date of AD 2021–20–09). (4) Except as provided by Note 1 of EASA AD 2021–0020, the initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2021–0020 is at the applicable ‘‘thresholds’’ as incorporated by the requirements of paragraph (3) of EASA AD PO 00000 Frm 00022 Fmt 4702 Sfmt 4702 (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 2022–0201, dated September 26, 2022 (EASA AD 2022– 0201). 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 2022–0201 (1) Where EASA AD 2022–0201 refers to its effective date, this AD requires using the effective date of this AD. (2) The requirements specified in paragraphs (1) and (2) of EASA AD 2022– 0201 do not apply to this AD. (3) Paragraph (3) of EASA AD 2022–0201 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. (4) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2022–0201 is at the applicable ‘‘limitations’’ and ‘‘associated thresholds’’ as incorporated by the requirements of paragraph (3) of EASA AD 2022–0201, or within 90 days after the effective date of this AD, whichever occurs later. (5) The provisions specified in paragraphs (4) and (5) of EASA AD 2022–0201 do not apply to this AD. (6) The ‘‘Remarks’’ section of EASA AD 2022–0201 does not apply to this AD. (l) New Provisions for Alternative Actions and Intervals After the existing maintenance or inspection program has been revised as required by paragraph (j) of this AD, no alternative actions (e.g., inspections) and intervals are allowed unless they are approved as specified in the provisions of the ‘‘Ref. Publications’’ section of EASA AD 2022–0201. (m) Additional FAA AD Provisions The following provisions also apply to this AD: E:\FR\FM\06DEP1.SGM 06DEP1 Federal Register / Vol. 87, No. 233 / Tuesday, December 6, 2022 / Proposed Rules (1) Alternative Methods of Compliance (AMOCs): The Manager, Large Aircraft Section, International Validation Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or responsible Flight Standards Office, as appropriate. If sending information directly to the Large Aircraft Section, International Validation Branch, send it to the attention of the person identified in paragraph (n) of this AD. Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (2) Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions must be accomplished using a method approved by the Manager, Large Aircraft Section, International Validation Branch, FAA; or EASA; or ATR—GIE Avions de Transport Re´gional’s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOAauthorized signature. (n) Related Information For more information about this AD, contact Shahram Daneshmandi, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 206–231–3220; email shahram.daneshmandi@faa.gov. (o) 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 2022–0201, dated September 26, 2022. (ii) [Reserved] (4) The following service information was approved for IBR on December 27, 2021 (86 FR 64805, November 19, 2021). (i) European Union Aviation Safety Agency (EASA) AD 2021–0020, dated January 15, 2021. (ii) [Reserved] (5) For EASA AD 2022–0201 and AD 2021– 0020, 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 these EASA ADs on the EASA website at ad.easa.europa.eu. (6) You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. (7) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, email fr.inspection@nara.gov, or go to: www.archives.gov/federal-register/cfr/ibrlocations.html. Issued on December 1, 2022. Christina Underwood, Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022–26468 Filed 12–5–22; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF ENERGY Federal Energy Regulatory Commission 18 CFR Part 40 [Docket No. RM22–12–000] Reliability Standards To Address Inverter-Based Resources Federal Energy Regulatory Commission, Department of Energy (DOE). ACTION: Notice of proposed rulemaking. AGENCY: The Federal Energy Regulatory Commission (Commission) proposes to direct the North American Electric Reliability Corporation (NERC), the Commission-certified Electric Reliability Organization (ERO), to develop new or modified Reliability Standards that address the following reliability gaps related to inverter-based resources (IBR): data sharing; model validation; planning and operational SUMMARY: 74541 studies; and performance requirements. Further, the Commission proposes to direct NERC to submit to the Commission a compliance filing within 90 days of the effective date of the final rule in this proceeding that includes a detailed, comprehensive standards development and implementation plan to ensure all new or modified Reliability Standards necessary to address the IBRrelated reliability gaps identified in the final rule are submitted to the Commission within 36 months of Commission approval of the plan. DATES: Comments are due February 6, 2023 and reply Comments are due March 6, 2023. ADDRESSES: Comments, identified by docket number, may be filed in the following ways. Electronic filing through https://www.ferc.gov, is preferred. • Electronic Filing: Documents must be filed in acceptable native applications and print-to-PDF, but not in scanned or picture format. • For those unable to file electronically, comments may be filed by U.S. Postal Service mail or by hand (including courier) delivery. Æ Mail via U.S. Postal Service only: Addressed to: Federal Energy Regulatory Commission, Office of the Secretary, 888 First Street NE, Washington, DC 20426. Æ For Delivery via Any Other Carrier (including courier): Deliver to: Federal Energy Regulatory Commission, Office of the Secretary, 12225 Wilkins Avenue, Rockville, MD 20852. FOR FURTHER INFORMATION CONTACT: Eugene Blick (Technical Information), Office of Electric Reliability, Federal Energy Regulatory Commission, 888 First Street NE, Washington, DC 20426, (202) 502–8803, Eugene.Blick@ferc.gov. Alan J. Rukin (Legal Information), Office of the General Counsel, Federal Energy Regulatory Commission, 888 First Street NE, Washington, DC 20426, (202) 502–8502, Alan.Rukin@ferc.gov. SUPPLEMENTARY INFORMATION: Table of Contents lotter on DSK11XQN23PROD with PROPOSALS1 Paragraph Nos. I. Introduction ......................................................................................................................................................................................... II. Background ......................................................................................................................................................................................... A. Legal Authority ........................................................................................................................................................................... B. Reliability Impacts of IBR Technologies ................................................................................................................................... C. Actions To Address the Reliability Impact of IBR Technologies ............................................................................................ III. The Need for Reform ........................................................................................................................................................................ A. Recent Events Show IBR-Related Adverse Reliability Impacts on the Bulk-Power System ................................................. B. Reliability Standards Do Not Adequately Address IBR Reliability Risks ............................................................................... 1. Data Sharing ......................................................................................................................................................................... 2. IBR and IBR–DER Data and Model Validation .................................................................................................................. VerDate Sep<11>2014 17:01 Dec 05, 2022 Jkt 259001 PO 00000 Frm 00023 Fmt 4702 Sfmt 4702 E:\FR\FM\06DEP1.SGM 06DEP1 1 10 10 12 17 24 24 27 27 33

Agencies

[Federal Register Volume 87, Number 233 (Tuesday, December 6, 2022)]
[Proposed Rules]
[Pages 74538-74541]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-26468]



[[Page 74538]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-1245; Project Identifier MCAI-2022-00503-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) 
2021-20-09, which applies to certain ATR--GIE Avions de Transport 
R[eacute]gional Model ATR72 airplanes. AD 2021-20-09 requires revising 
the existing maintenance or inspection program, as applicable, to 
incorporate new or more restrictive airworthiness limitations. Since 
the FAA issued AD 2021-20-09, the FAA has determined that new or more 
restrictive tasks and airworthiness limitations are necessary. This 
proposed AD would continue to require the actions in AD 2021-20-09 and 
require revising the existing maintenance or inspection program, as 
applicable, to incorporate additional new or more restrictive tasks and 
airworthiness limitations, as specified in a European Union Aviation 
Safety Agency (EASA) AD, which is proposed for incorporation by 
reference. 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 January 20, 
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: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE, Washington, DC 20590, between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays.
    For EASA material that that is proposed for IBR in this NPRM, 
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 at ad.easa.europa.eu. 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 in the AD docket at regulations.gov by 
searching for and locating Docket No. FAA-2022-1245.

Examining the AD Docket

    You may examine the AD docket at regulations.gov by searching for 
and locating Docket No. FAA-2022-1245; 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.

FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace 
Engineer, Large Aircraft Section, FAA, International Validation Branch, 
2200 South 216th St., Des Moines, WA 98198; 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-2022-1245; Project Identifier 
MCAI-2022-00503-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, Aerospace Engineer, Large Aircraft Section, FAA, 
International Validation Branch, 2200 South 216th St., Des Moines, WA 
98198; telephone 206-231-3220; email [email protected]. Any 
commentary that the FAA receives which is not specifically designated 
as CBI will be placed in the public docket for this rulemaking.

Background

    The FAA issued AD 2021-20-09, Amendment 39-21747 (86 FR 64805, 
November 19, 2021) (AD 2021-20-09), which applies to certain ATR--GIE 
Avions de Transport R[eacute]gional Model ATR72-101, -102, -201, -202, 
-211, -212, and -212A airplanes. AD 2021-20-09 requires revising the 
existing maintenance or inspection program, as applicable, to 
incorporate new or more restrictive airworthiness limitations. The FAA 
issued AD 2021-20-09 to address reduced structural integrity of the 
airplane.

Actions Since AD 2021-20-09 Was Issued

    Since the FAA issued AD 2021-20-09, the FAA has determined that new 
or more restrictive tasks and airworthiness limitations are necessary.
    EASA, which is the Technical Agent for the Member States of the 
European Union, has issued EASA AD 2022-0201, dated September 26, 2022 
(EASA AD 2022-0201) (also referred to as the MCAI), to correct an 
unsafe condition for all ATR--GIE Avions de Transport R[eacute]gional 
Model ATR72-101, -102, -201, -202, -211, -212, and -212A airplanes.
    Airplanes with an original airworthiness certificate or original 
export certificate of airworthiness issued after February 3, 2022, must 
comply with the airworthiness limitations specified as part of the 
approved type design and referenced on

[[Page 74539]]

the type certificate data sheet; this AD therefore does not include 
those airplanes in the applicability.
    This proposed AD was prompted by a determination that new or more 
restrictive tasks and airworthiness limitations are necessary. The FAA 
is proposing this AD to address fatigue cracking and damage in 
principal structural elements, which could result in reduced structural 
integrity of the airplane. See the MCAI for additional background 
information.

Related Service Information Under 1 CFR Part 51

    EASA AD 2022-0201 describes new or more restrictive tasks, 
airworthiness limitations for airplane structures, and safe life 
limits.
    This proposed AD would also require EASA AD 2021-0020, dated 
January 15, 2021 (EASA AD 2021-0020), which the Director of the Federal 
Register approved for incorporation by reference as of December 27, 
2021 (86 FR 64805, November 19, 2021).
    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 the ADDRESSES section.

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 the 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 the requirements of AD 2021-20-09. 
This proposed AD would also require revising the existing maintenance 
or inspection program, as applicable, to incorporate new or more 
restrictive tasks and airworthiness limitations, which are specified in 
EASA AD 2022-0201 described previously, as proposed for incorporation 
by reference. Any differences with EASA AD 2022-0201 are identified as 
exceptions in the regulatory text of this AD.
    This proposed AD would require revisions to certain operator 
maintenance documents to include new actions (e.g., inspections). 
Compliance with these actions 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 (m)(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 2021-0020 and incorporate 
EASA AD 2022-0201 by reference in the FAA final rule. This proposed AD 
would, therefore, require compliance with EASA AD 2021-0020 and EASA AD 
2022-0201 in their entirety 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 2021-0020 or EASA AD 2022-0201 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 2021-0020 or EASA AD 2022-0201. Service information required by 
EASA AD 2021-0020 and EASA AD 2022-0201 for compliance will be 
available at regulations.gov by searching for and locating Docket No. 
FAA-2022-1245 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), or intervals may be used unless the actions and intervals 
are approved as an AMOC in accordance with the procedures specified in 
the AMOCs paragraph under ``Additional FAA Provisions.'' This new 
format includes a ``New Provisions for Alternative Actions and 
Intervals'' paragraph that does not specifically refer to AMOCs, but 
operators may still request an AMOC to use an alternative action or 
interval.

Costs of Compliance

    The FAA estimates that this proposed AD affects 23 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 2021-20-09 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

[[Page 74540]]

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:
    (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 (AD) 2021-20-09, Amendment 39-21747 
(86 FR 64805, November 19, 2021) (AD 2021-20-09); and
0
b. Adding the following new AD:

ATR--GIE Avions de Transport R[eacute]gional: Docket No. FAA-2022-
1245; Project Identifier MCAI-2022-00503-T.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by January 20, 2023.

(b) Affected ADs

    This AD replaces AD 2021-20-09, Amendment 39-21747 (86 FR 64805, 
November 19, 2021) (AD 2021-20-09).

(c) Applicability

    This AD applies to ATR--GIE Avions de Transport R[eacute]gional 
Model ATR72-101, -102, -201, -202, -211, -212, and -212A airplanes, 
certificated in any category, with an original airworthiness 
certificate or original export certificate of airworthiness issued 
on or before February 3, 2022.

(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 tasks and airworthiness limitations are necessary. The 
FAA is issuing this AD to address fatigue cracking and damage in 
principal structural elements, which 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 No Changes

    This paragraph restates the requirements of paragraph (j) of AD 
2021-20-09, with no changes. For ATR--GIE Avions de Transport 
R[eacute]gional Model ATR72-101, -102, -201, -202, -211, -212, and -
212A airplanes, certificated in any category, with an original 
airworthiness certificate or original export certificate of 
airworthiness issued on or before October 9, 2020, 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 2021-0020, dated 
January 15, 2021 (EASA AD 2021-0020). 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 2021-0020, With No Changes

    This paragraph restates the requirements of paragraph (k) of AD 
2021-20-09, with no changes.
    (1) Where EASA AD 2021-0020 refers to its effective date, this 
AD requires using December 27, 2021 (the effective date of AD 2021-
20-09).
    (2) The requirements specified in paragraphs (1) and (2) of EASA 
AD 2021-0020 do not apply to this AD.
    (3) Paragraph (3) of EASA AD 2021-0020 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 December 27, 2021 (the effective 
date of AD 2021-20-09).
    (4) Except as provided by Note 1 of EASA AD 2021-0020, the 
initial compliance time for doing the tasks specified in paragraph 
(3) of EASA AD 2021-0020 is at the applicable ``thresholds'' as 
incorporated by the requirements of paragraph (3) of EASA AD 2021-
0020, or within 90 days after December 27, 2021 (the effective date 
of AD 2021-20-09), whichever occurs later.
    (5) The provisions specified in paragraphs (4) and (5) of EASA 
AD 2021-0020 do not apply to this AD.
    (6) The ``Remarks'' section of EASA AD 2021-0020 does not apply 
to this AD.

(i) Retained Restrictions on Alternative Actions and Intervals, With a 
New Exception

    This paragraph restates the requirements of paragraph (l) of AD 
2021-20-09, with a new exception. Except as required by paragraph 
(j) of this AD, after the existing maintenance or inspection program 
has been revised as required by paragraph (g) of this AD, no 
alternative actions (e.g., inspections) and intervals are allowed 
unless they are approved as specified in the provisions of the 
``Ref. Publications'' section of EASA AD 2021-0020.

(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 2022-0201, dated September 26, 2022 (EASA 
AD 2022-0201). 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 2022-0201

    (1) Where EASA AD 2022-0201 refers to its effective date, this 
AD requires using the effective date of this AD.
    (2) The requirements specified in paragraphs (1) and (2) of EASA 
AD 2022-0201 do not apply to this AD.
    (3) Paragraph (3) of EASA AD 2022-0201 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.
    (4) The initial compliance time for doing the tasks specified in 
paragraph (3) of EASA AD 2022-0201 is at the applicable 
``limitations'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2022-0201, or within 90 
days after the effective date of this AD, whichever occurs later.
    (5) The provisions specified in paragraphs (4) and (5) of EASA 
AD 2022-0201 do not apply to this AD.
    (6) The ``Remarks'' section of EASA AD 2022-0201 does not apply 
to this AD.

(l) New Provisions for Alternative Actions and Intervals

    After the existing maintenance or inspection program has been 
revised as required by paragraph (j) of this AD, no alternative 
actions (e.g., inspections) and intervals are allowed unless they 
are approved as specified in the provisions of the ``Ref. 
Publications'' section of EASA AD 2022-0201.

(m) Additional FAA AD Provisions

    The following provisions also apply to this AD:

[[Page 74541]]

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

(n) Related Information

    For more information about this AD, contact Shahram Daneshmandi, 
Aerospace Engineer, Large Aircraft Section, FAA, International 
Validation Branch, 2200 South 216th St., Des Moines, WA 98198; 
telephone 206-231-3220; email [email protected].

(o) 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 2022-0201, 
dated September 26, 2022.
    (ii) [Reserved]
    (4) The following service information was approved for IBR on 
December 27, 2021 (86 FR 64805, November 19, 2021).
    (i) European Union Aviation Safety Agency (EASA) AD 2021-0020, 
dated January 15, 2021.
    (ii) [Reserved]
    (5) For EASA AD 2022-0201 and AD 2021-0020, 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 at ad.easa.europa.eu.
    (6) You may view this service information at the FAA, 
Airworthiness Products Section, Operational Safety Branch, 2200 
South 216th St., Des Moines, WA. For information on the availability 
of this material at the FAA, call 206-231-3195.
    (7) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on December 1, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2022-26468 Filed 12-5-22; 8:45 am]
BILLING CODE 4910-13-P

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