AD 2022-02-17

3923 Federal Register / Vol. 87, No. 17 / Wednesday, January 26, 2022 / Rules and Regulations supplemental type certificate no. ST01086DE, as modified by Peregrine. In lieu of § 25.1353(b)(1) through (4) at amendment 25–123, or § 25.1353(c)(1) through (4) at earlier amendments, each rechargeable lithium battery installation must: 1. Be designed to maintain safe cell temperatures and pressures under all foreseeable operating conditions to prevent fire and explosion. 2. Be designed to prevent the occurrence of self-sustaining, uncontrollable increases in temperature or pressure, and automatically control the charge rate of each cell to protect against adverse operating conditions, such as cell imbalance, back charging, overcharging and overheating. 3. Not emit explosive or toxic gases, either in normal operation or as a result of its failure that may accumulate in hazardous quantities within the airplane. 4. Meet the requirements of § 25.863. 5. Not damage surrounding structure or adjacent systems, equipment, or electrical wiring from corrosive fluids or gases that may escape in such a way as to cause a major or more-severe failure condition. 6. Have provisions to prevent any hazardous effect on airplane structure or systems caused by the maximum amount of heat it can generate due to any failure of it or its individual cells. 7. Have a failure sensing and warning system to alert the flight crew if its failure affects safe operation of the airplane. 8. Have a monitoring and warning feature that alerts the flightcrew when its charge state falls below acceptable levels if its function is required for safe operation of the airplane. 9. Have a means to automatically disconnect from its charging source in the event of an over-temperature condition, cell failure or battery failure. Note: A battery system consists of the battery, battery charger, and any protective monitoring and alerting circuitry or hardware inside or outside of the battery. It also includes vents (where necessary) and packaging. For the purpose of these special conditions, a battery and the battery system is referred to as a battery. Issued in Kansas City, Missouri, on January 20, 2022. Patrick R. Mullen, Manager, Technical Innovation Policy Branch, Policy and Innovation Division, Aircraft Certification Service. [FR Doc. 2022–01443 Filed 1–25–22; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2022–0009; Project Identifier MCAI–2021–01459–R; Amendment 39–21914; AD 2022–02–17] RIN 2120–AA64 Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final rule; request for comments. SUMMARY : The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Deutschland GmbH (AHD) Model MBB–BK 117 C–2, MBB– BK 117 D–2, and MBB–BK 117 D–3 helicopters. This AD was prompted by reports of engine flame out following prolonged operations in falling snow on helicopters with an inlet barrier filter (IBF) system installed. This AD requires revising the existing Rotorcraft Flight Manual (RFM) for your helicopter, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products. DATES : This AD becomes effective February 10, 2022. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of February 10, 2022. The FAA must receive comments on this AD by March 14, 2022. 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 https://www.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. For EASA material incorporated by reference (IBR) in this final rule, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find this IBR material on the EASA website at https://ad.easa.europa.eu. For Airbus Helicopters service information identified in this final rule, contact Airbus Helicopters, 2701 North Forum Drive, Grand Prairie, TX 75052; telephone (972) 641–0000 or (800) 232– 0323; fax (972) 641–3775; or at https:// www.airbus.com/helicopters/services/ technical-support.html. You may view this material at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N–321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222–5110. Service information that is IBRed is also available in the AD docket at https:// www.regulations.gov by searching for and locating Docket No. FAA–2022– 0009. Examining the AD Docket You may examine the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA–2022–0009; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this final rule, the EASA AD, any comments received, and other information. The street address for Docket Operations is listed above. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT : Hal Jensen, Aerospace Engineer, Operational Safety Branch, Compliance & Airworthiness Division, FAA, 950 L’Enfant Plaza N SW, Washington, DC 20024; telephone (202) 267–9167; email hal.jensen@faa.gov. SUPPLEMENTARY INFORMATION : Background EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA Emergency AD 2021–0289–E, dated December 23, 2021 (EASA AD 2021–0289–E), to correct an unsafe condition for all Airbus Helicopters Deutschland GmbH (AHD), formerly Eurocopter Deutschland GmbH; and Airbus Helicopters Inc., formerly American Eurocopter LLC, Model MBB–BK117 C–2, D–2, D–3, and D–3m helicopters, all variants, all serial numbers. This AD was prompted by reports of engine flame out following prolonged operations in falling snow with the IBF system installed. The FAA is issuing this AD to prevent partial icing of an IBF engine intake and engine flame out. The unsafe condition, if not addressed, could result in engine failure and reduced control of the helicopter, possibly resulting in damage to the VerDate Sep<11>2014 15:49 Jan 25, 2022 Jkt 256001 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 E:\FR\FM\26JAR1.SGM 26JAR1 khammond on DSKJM1Z7X2PROD with RULES

3924 Federal Register / Vol. 87, No. 17 / Wednesday, January 26, 2022 / Rules and Regulations helicopter or injury to occupants. See EASA AD 2021–0289–E for additional background information. Related Service Information Under 1 CFR Part 51 EASA AD 2021–0289–E requires amending the RFM by incorporating the applicable RFM temporary revision (TR), to amend the IBF system limitations and emergency procedures sections, to include a restriction to operation in falling or blowing snow. 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. Other Related Service Information The FAA reviewed Airbus Helicopters Service Bulletin SB MBB–BK117 C–2– 71–005, Revision 5, dated May 31, 2017; and Airbus Helicopters Service Bulletin SB MBB-BK117 D-2–71–001, Revision 1, dated August 2, 2017. This service information specifies procedures for installing an IBF system. FAA’s Determination These helicopters have been approved by EASA and are approved for operation in the United States. Pursuant to the FAA’s bilateral agreement with the European Union, EASA has notified the FAA of the unsafe condition described in its AD. The FAA is issuing this AD after evaluating all pertinent information and determining that the unsafe condition exists and is likely to exist or develop on other helicopters of the same type design. Requirements of This AD This AD requires accomplishing the actions specified in EASA AD 2021– 0289–E, described previously, as IBRed, except for any differences identified as exceptions in the regulatory text of this AD and except as discussed under ‘‘Differences Between this AD and the EASA 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, EASA AD 2021– 0289–E will be IBRed in this FAA final rule. This AD would, therefore, require compliance with EASA AD 2021–0289– E in its entirety through that incorporation, except for any differences identified as exceptions in the regulatory text of this AD. Using common terms that are the same as the heading of a particular section in EASA AD 2021–0289–E 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 2021–0289–E. Service information referenced in EASA AD 2021–0289–E for compliance will be available at https://www.regulations.gov by searching for and locating Docket No. FAA–2022–0009. Differences Between This AD and the EASA AD EASA AD 2021–0289–E applies to Model MBB–BK117 D–3m helicopters, whereas this AD does not because that model is not FAA type-certificated. EASA AD 2021–0289–E defines ‘‘Retrofit SB’’ as, ‘‘AH Service Bulletin (SB) MBB–BK117 C–2–71–005, SB MBB–BK117 D–2–71–001 and SB MBB– BK117 D–3–71–001, as applicable, installing the IBF system,’’ whereas this AD redefines ‘‘Retrofit SB’’ because SB MBB–BK117 D–3–71–001 has not been issued. EASA AD 2021–0289–E requires operators to ‘‘inform all flight crews’’ of revisions to the RFM, and thereafter to ‘‘operate the helicopter accordingly.’’ However, this AD does not specifically require those actions. 14 CFR 91.9 requires that no person may operate a civil aircraft without complying with the operating limitations specified in the RFM. Therefore, including a requirement in this AD to operate the helicopter according to the revised RFM would be redundant and unnecessary. Additionally, FAA regulations mandate compliance with only the operating limitations section of the flight manual. Some of the flight manual changes required by this AD apply to the emergency procedures section of the existing RFM for your helicopter. Compliance with such requirements in an AD is impracticable to demonstrate or track on an ongoing basis; therefore, requirements to operate the aircraft in such a manner are unenforceable. Nonetheless, the FAA recommends that flight crews of the helicopters listed in the applicability be made aware of the flight manual changes and that they operate in accordance with the revised emergency procedures. In this AD, the existing RFM for your helicopter may be revised and the logbook entry for that action may be made by the owner/operator (pilot) holding at least a private pilot certificate, whereas the EASA AD does not mention this allowance. This action must be entered into the aircraft records showing compliance with this AD in accordance with 14 CFR 43.9(a)(1) through (4) and 14 CFR 91.417(a)(2)(v). The record must be maintained as required by 14 CFR 91.417 or 135.439. Interim Action The FAA considers this AD interim action. If final action is later identified, the FAA might consider further rulemaking then. Justification for Immediate Adoption and Determination of the Effective Date Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5 U.S.C. 551 et seq. ) authorizes agencies to dispense with notice and comment procedures for rules when the agency, for ‘‘good cause,’’ finds that those procedures are ‘‘impracticable, unnecessary, or contrary to the public interest.’’ Under this section, an agency, upon finding good cause, may issue a final rule without providing notice and seeking comment prior to issuance. Further, section 553(d) of the APA authorizes agencies to make rules effective in less than thirty days, upon a finding of good cause. An unsafe condition exists that requires the immediate adoption of this AD without providing an opportunity for public comments prior to adoption. The FAA has found that the risk to the flying public justifies foregoing notice and comment prior to adoption of this rule because the affected component is part of the propulsion system that is critical to the power of the helicopter. Partial icing of the affected component could result in engine flame out, engine failure, reduced control of the helicopter, and subsequent damage to the helicopter or injury to occupants. In light of this, required actions must be accomplished within 14 days or 40 hours time-in-service, whichever occurs first after the effective date of this AD. This compliance time is shorter than the time necessary for the public to comment and for publication of the final rule. Accordingly, notice and opportunity for prior public comment are impracticable and contrary to the public interest pursuant to 5 U.S.C. 553(b)(3)(B). In addition, the FAA finds that good cause exists pursuant to 5 U.S.C. 553(d) for making this amendment effective in less than 30 days, for the same reasons the FAA found good cause to forego notice and comment. VerDate Sep<11>2014 15:49 Jan 25, 2022 Jkt 256001 PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 E:\FR\FM\26JAR1.SGM 26JAR1 khammond on DSKJM1Z7X2PROD with RULES

3925 Federal Register / Vol. 87, No. 17 / Wednesday, January 26, 2022 / Rules and Regulations Comments Invited The FAA invites you to send any written data, views, or arguments about this final rule. Send your comments to an address listed under ADDRESSES . Include ‘‘Docket No. FAA–2022–0009; Project Identifier MCAI–2021–01459–R’’ at the beginning of your comments. The most helpful comments reference a specific portion of the final rule, explain the reason for any recommended change, and include supporting data. The FAA will consider all comments received by the closing date and may amend this final rule because of those comments. Except for Confidential Business Information (CBI) as described in the following paragraph, and other information as described in 14 CFR 11.35, the FAA will post all comments received, without change, to https:// www.regulations.gov, including any personal information you provide. The agency will also post a report summarizing each substantive verbal contact received about this final rule. Confidential Business Information CBI is commercial or financial information that is both customarily and actually treated as private by its owner. Under the Freedom of Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public disclosure. If your comments responsive to this AD contain commercial or financial information that is customarily treated as private, that you actually treat as private, and that is relevant or responsive to this AD, it is important that you clearly designate the submitted comments as CBI. Please mark each page of your submission containing CBI as ‘‘PROPIN.’’ The FAA will treat such marked submissions as confidential under the FOIA, and they will not be placed in the public docket of this AD. Submissions containing CBI should be sent to Hal Jensen, Aerospace Engineer, Operational Safety Branch, Compliance & Airworthiness Division, FAA, 950 L’Enfant Plaza N SW, Washington, DC 20024; telephone (202) 267–9167; email hal.jensen@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. Regulatory Flexibility Act The requirements of the Regulatory Flexibility Act (RFA) do not apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and comment. Because the FAA has determined that it has good cause to adopt this rule without prior notice and comment, RFA analysis is not required. Costs of Compliance The FAA estimates that this AD affects 213 helicopters of U.S. Registry. Labor rates are estimated at $85 per work-hour. Based on these numbers, the FAA estimates the following costs to comply with this AD. Revising the existing RFM for your helicopter takes about 1 work-hour for an estimated cost of about $85 per helicopter and up to about $18,105 for the U.S. fleet. 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 This AD will not have federalism implications under Executive Order 13132. This AD will 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, I certify that this AD: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866, and (2) Will not affect intrastate aviation in Alaska. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. The Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 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 adding the following new airworthiness directive: 2022–02–17 Airbus Helicopters Deutschland GmbH (AHD): Amendment 39–21914; Docket No. FAA–2022–0009; Project Identifier MCAI–2021–01459–R. (a) Effective Date This airworthiness directive (AD) is effective February 10, 2022. (b) Affected ADs None. (c) Applicability This AD applies to Airbus Helicopters Deutschland GmbH (AHD) Model MBB–BK 117 C–2, MBB–BK 117 D–2, and MBB–BK 117 D–3 helicopters, certificated in any category. (d) Subject Joint Aircraft System Component (JASC) Code: 7160, Engine Air Intake System. (e) Unsafe Condition This AD was prompted by reports of engine flame out following prolonged operations in falling snow with the inlet barrier filter (IBF) system installed. The FAA is issuing this AD to prevent partial icing of an IBF engine intake and engine flame out. The unsafe condition, if not addressed, could result in engine failure and reduced control of the helicopter, possibly resulting in damage to the helicopter or injury to occupants. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Requirements Comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) Emergency AD 2021– 0289–E, dated December 23, 2021 (EASA AD 2021–0289–E). (h) Exceptions to EASA AD 2021–0289–E (1) Where EASA AD 2021–0289–E defines Retrofit SB, replace the text ‘‘AH Service Bulletin (SB) MBB–BK117 C–2–71–005, SB MBB–BK117 D–2–71–001 and SB MBB– BK117 D–3–71–001, as applicable, installing the IBF system,’’ with ‘‘AH Service Bulletin (SB) MBB–BK117 C–2–71–005 and SB MBB– BK117 D–2–71–001, as applicable, installing the IBF system; and for Model MBB–BK 117 D–3 helicopters, in accordance with a method approved by the Manager, General Aviation & Rotorcraft Section, International Validation Branch, FAA; or EASA; or Airbus Helicopters’ EASA Design Organization VerDate Sep<11>2014 15:49 Jan 25, 2022 Jkt 256001 PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 E:\FR\FM\26JAR1.SGM 26JAR1 khammond on DSKJM1Z7X2PROD with RULES

3926 Federal Register / Vol. 87, No. 17 / Wednesday, January 26, 2022 / Rules and Regulations Approval (DOA). If approved by the DOA, the approval must include the DOA- authorized signature.’’ (2) Where EASA AD 2021–0289–E requires compliance in terms of flight hours, this AD requires using hours time-in-service. (3) Where EASA AD 2021–0289–E refers to its effective date, this AD requires using the effective date of this AD. (4) Where paragraph (1) of EASA AD 2021– 0289–E specifies to ‘‘inform all flight crews, and, thereafter, operate the helicopter accordingly,’’ this AD does not require those actions. (5) The action required by paragraphs (1) and (2) of EASA AD 2021–0289–E may be performed by the owner/operator (pilot) holding at least a private pilot certificate and must be entered into the aircraft records showing compliance with this AD in accordance with 14 CFR 43.9(a)(1) through (4) and 14 CFR 91.417(a)(2)(v). The record must be maintained as required by 14 CFR 91.417 or 135.439. (6) This AD does not mandate compliance with the ‘‘Remarks’’ section of EASA AD 2021–0289–E. (i) Special Flight Permit Special flight permits may be permitted provided that there are no passengers on board. (j) Alternative Methods of Compliance (AMOCs) (1) 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 local Flight Standards District Office, as appropriate. If sending information directly to the manager of the International Validation Branch, send it to the attention of the person identified in paragraph (k) of this AD. Information may be emailed to: 9-AVS-AIR- 730-AMOC@faa.gov. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/ certificate holding district office. (k) Related Information For more information about this AD, contact Hal Jensen, Aerospace Engineer, Operational Safety Branch, Compliance & Airworthiness Division, FAA, 950 L’Enfant Plaza N SW, Washington, DC 20024; telephone (202) 267–9167; email hal.jensen@ faa.gov. (l) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) European Union Aviation Safety Agency (EASA) Emergency AD 2021–0289–E, dated December 23, 2021. (ii) [Reserved] (3) For EASA AD 2021–0289–E, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find the EASA material on the EASA website at https://ad.easa.europa.eu. (4) You may view this service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N–321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222–5110. This material may be found in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA–2022–0009. (5) You may view this material that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, email fr.inspection@nara.gov, or go to: https:// www.archives.gov/federal-register/cfr/ibr- locations.html. Issued on January 13, 2022. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022–01540 Filed 1–24–22; 11:15 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2021–1010; Project Identifier MCAI–2020–00807–G; Amendment 39–21924; AD 2022–03–07] RIN 2120–AA64 Airworthiness Directives; Stemme AG Gliders AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final rule. SUMMARY : The FAA is adopting a new airworthiness directive (AD) for certain Stemme AG TSA–M Model S6 and S6– RT gliders. This AD was prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as a new version of the propeller gearbox tooth belt with a reduced life limit. This AD requires establishing a life limit of 5 years for certain propeller gearbox tooth belts. The FAA is issuing this AD to address the unsafe condition on these products. DATES : This AD is effective March 2, 2022. ADDRESSES : For service information identified in this final rule, contact Stemme AG, Flugplatzstrasse F2, Nr. 6–7, D–15344 Strausberg, Germany; phone: +49 (0) 3341 3612–0; fax: +49 (0) 3341 3612–30; email: airworthiness@ stemme.de ; website: https:// www.stemme.com . You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (817) 222–5110. It is also available at https://www.regulations.gov by searching for and locating Docket No. FAA–2021–1010. Examining the AD Docket You may examine the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA–2021–1010; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this final rule, the MCAI, any comments received, and other information. The address for Docket Operations is U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE, Washington, DC 20590. FOR FURTHER INFORMATION CONTACT : Jim Rutherford, Aviation Safety Engineer, General Aviation & Rotorcraft Section, International Validation Branch, FAA, 901 Locust, Room 301, Kansas City, MO 64106; phone: (816) 329–4165; email: jim.rutherford@faa.gov . SUPPLEMENTARY INFORMATION : Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Stemme AG TSA–M Model S6 and S6–RT gliders. The NPRM published in the Federal Register on November 22, 2021 (86 FR 66229). The NPRM was prompted by MCAI originated by the European Union Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union. EASA issued EASA AD 2020–0140, dated June 23, 2020 (referred to after this as ‘‘the MCAI’’), to address an unsafe condition on Stemme AG (Stemme) TSA–M Model S6 and S6–RT powered sailplanes (gliders) and ASP S15–1 airplanes. The MCAI states: The airworthiness limitations for Stemme TSA–M powered sailplanes and Stemme ASP aeroplanes, which are approved by EASA, are currently defined and published in Chapter 4 of the applicable AMM [aircraft maintenance manual]. These instructions have been identified as mandatory for continued airworthiness. VerDate Sep<11>2014 15:49 Jan 25, 2022 Jkt 256001 PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 E:\FR\FM\26JAR1.SGM 26JAR1 khammond on DSKJM1Z7X2PROD with RULES