AD 2021-23-01

72836 Federal Register / Vol. 86, No. 244 / Thursday, December 23, 2021 / Rules and Regulations (C) For each nut installed as required by paragraphs (g)(1)(iii)(A) and (B) of this AD, apply a torque of 5.65–7.90 Nm (50–70 in lb) plus tare torque to each nut, and apply a torque stripe using torque seal lacquer (C– 049) or equivalent lacquer, as shown in Figure 2 of ASB 206L–19–181. (iv) For Bell Textron Canada Limited Model 206L–4 helicopters that have been modified by installing STC SH2750NM: (A) Remove each nut P/N MS21042L4 installed on each TRDS Thomas coupling from service, except for nuts P/N MS21042L4 installed on the forward short TRDS Thomas coupling, and replace with nut P/N NAS9926–4L. The location of nut P/N NAS9926–4L is depicted in Detail A Figure 1 of ASB 206L–19–181. (B) Remove from service each nut P/N MS21042L5 installed on the forward short TRDS Thomas coupling and replace with nut P/N 90–132L5. (C) For each nut installed as required by paragraphs (g)(1)(iv)(A) and (B) of this AD, apply a torque of 5.65–7.90 Nm (50–70 in lb) plus tare torque to each nut, and apply a torque stripe using torque seal lacquer (C– 049) or equivalent lacquer, as shown in Figure 2 of ASB 206L–19–181. (2) Within 25 hours TIS after installation of any nut P/N NAS9926–4L, P/N 90–132L4, or P/N 90–132L5, as required by paragraphs (g)(1)(i)(A), (ii)(A) and (B), (iii)(A) and (B), or (iv)(A) and (B) of this AD, apply a torque of 5.65 Nm (50 in lb) to each nut. (i) If the nut does not move, apply a torque stripe using torque seal lacquer (C–049) or equivalent lacquer, as shown in Figure 2 of ASB 206–19–136 or ASB 206L–19–181, as applicable to your model helicopter. (ii) If any nut moves, inspect each TRDS Thomas coupling and each bolt, nut, and washer for elongated holes and fretting on the fasteners. If any TRDS Thomas coupling has an elongated hole, remove the TRDS Thomas coupling from service. If any bolt, nut, or washer has any fretting, remove the affected part from service. (3) As of the effective date of this AD, do not install nut P/N MS21042L4 or MS21042L5 on any TRDS Thomas coupling. (h) 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 (i)(1) 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. (i) Related Information (1) For more information about this AD, contact Matt Fuller, AD Program Manager, General Aviation & Rotorcraft Unit, Airworthiness Products Section, Operational Safety Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222– 5110; email matthew.fuller@faa.gov. (2) Bell Service Instruction BHT–206–SI– 2052, Revision 1, dated October 14, 2010, which is not incorporated by reference, contains additional information about the subject of this AD. This service information is available at the contact information specified in paragraphs (j)(3) and (4) of this AD. (3) The subject of this AD is addressed in Transport Canada AD CF–2020–15, dated May 13, 2020. You may view the Transport Canada AD at https://www.regulations.gov in Docket No. FAA–2021–0728. (j) 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 the AD specifies otherwise. (i) Bell Alert Service Bulletin 206–19–136, dated August 27, 2019. (ii) Bell Alert Service Bulletin 206L–19– 181, Revision A, dated August 29, 2019. (3) For Bell service information identified in this AD, contact Bell Textron Canada Limited, 12,800 Rue de l’Avenir, Mirabel, Quebec J7J 1R4, Canada; telephone 1–450– 437–2862 or 1–800–363–8023; fax 1–450– 433–0272; email productsupport@ bellflight.com; or at https:// www.bellflight.com/support/contact-support. (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. (5) 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: https://www.archives.gov/federal-register/cfr/ ibr-locations.html. Issued on December 12, 2021. Ross Landes, Deputy Director for Regulatory Operations, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2021–27645 Filed 12–22–21; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2021–0716; Project Identifier 2019–CE–023–AD; Amendment 39–21799; AD 2021–23–01] 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 all Stemme AG Model Stemme S 12 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 an airspeed indicator (ASI) with speed markings inconsistent with the approved and published values. This AD requires inspecting the ASI markings and, depending on findings, either replacing the ASI or amending the existing aircraft flight manual (AFM) until the ASI is replaced. The FAA is issuing this AD to address the unsafe condition on these products. DATES : This AD is effective January 27, 2022. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of January 27, 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 (816) 329–4148. It is also available at https://www.regulations.gov by searching for and locating Docket No. FAA–2021–0716. Examining the AD Docket You may examine the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA–2021–0716; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal VerDate Sep<11>2014 19:16 Dec 22, 2021 Jkt 256001 PO 00000 Frm 00058 Fmt 4700 Sfmt 4700 E:\FR\FM\23DER1.SGM 23DER1 jspears on DSK121TN23PROD with RULES1

72837 Federal Register / Vol. 86, No. 244 / Thursday, December 23, 2021 / Rules and Regulations 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; fax: (816) 329–4090; email: jim.rutherford@ faa.gov. SUPPLEMENTARY INFORMATION : Discussion The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to all Stemme AG Model Stemme S 12 gliders. The NPRM published in the Federal Register on August 27, 2021 (86 FR 48065). 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 2019– 0082, dated April 12, 2019 (referred to after this as ‘‘the MCAI’’), to address an unsafe condition on Stemme AG Model Stemme S 12 gliders. The MCAI states: During a production inspection of a new powered sailplane, an ASI was found with speed markings inconsistent with the approved and published values (begin[ning] of the white and green arc). Subsequent investigation of the production records for delivered Stemme S 12 powered sailplanes does not exclude that a similar, non- conforming ASI was installed during production. This condition, if not corrected, could lead to erroneous information being provided to the pilot, particularly at the lower speed operation limits, possibly resulting in reduced control of the powered sailplane. To address this unsafe condition, Stemme AG issued the SB [service bulletin] to provide inspections instructions. For the reason described above, this [EASA] AD requires a one-time inspection of the markings of the affected part and, depending on findings, amending the Aircraft Flight Manual (AFM) and replacing the affected part. This [EASA] AD also prohibits installation of affected parts. You may examine the MCAI in the AD docket at https:// www.regulations.gov by searching for and locating Docket No. FAA–2021– 0716. Discussion of Final Airworthiness Directive Comments The FAA received no comments on the NPRM or on the determination of the costs. Conclusion 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 and service information referenced above. The FAA reviewed the relevant data and determined that air safety requires adopting this AD as proposed. Accordingly, the FAA is issuing this AD to address the unsafe condition on these products. This AD is adopted as proposed in the NPRM. Related Service Information Under 1 CFR Part 51 The FAA reviewed Stemme Service Bulletin No. P062–980027, Revision 00, dated December 17, 2018. The service information specifies checking the ASI markings and provides illustrations of correct markings. The service information specifies the procedure to replace an affected ASI with an ASI with correct markings. The service information also includes a temporary page to insert into the AFM until the ASI is replaced. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in ADDRESSES . Costs of Compliance The FAA estimates that this AD affects 20 gliders of U.S. registry. The FAA estimates it would take about 0.5 work-hour per glider to comply with the inspection requirements of this AD. The average labor rate is $85 per work-hour. Based on these figures, the FAA estimates the cost of this AD on U.S. operators to be $850 or $42.50 per glider. The FAA estimates that amending the AFM to insert and then remove the temporary page as a result of the inspection would take about 1 work- hour per glider for a total cost of $85 per glider. The FAA estimates that replacing the ASI would take about 3.5 work- hours and require parts costing $603, for a total cost of $900.50 per glider. The FAA has no way of determining the number of gliders that may need these actions. The FAA has included all known costs in its cost estimate. According to the manufacturer, however, some of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected operators. 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 above, I certify that this AD. For the reasons discussed above, I certify this AD: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866, (2) Will not affect intrastate aviation in Alaska, and (3) Will 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 Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: VerDate Sep<11>2014 19:16 Dec 22, 2021 Jkt 256001 PO 00000 Frm 00059 Fmt 4700 Sfmt 4700 E:\FR\FM\23DER1.SGM 23DER1 jspears on DSK121TN23PROD with RULES1

72838 Federal Register / Vol. 86, No. 244 / Thursday, December 23, 2021 / Rules and Regulations 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: 2021–23–01 Stemme AG: Amendment 39– 21799; Docket No. FAA–2021–0716; Project Identifier 2019–CE–023–AD. (a) Effective Date This airworthiness directive (AD) is effective January 27, 2022. (b) Affected ADs None. (c) Applicability This AD applies to Stemme AG Model Stemme S 12 gliders, all serial numbers, certificated in any category. (d) Subject Joint Aircraft System Component (JASC) Code 3414, Airspeed/Mach Indicator. (e) Unsafe Condition 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 an airspeed indicator (ASI) with speed markings inconsistent with the approved and published values (beginning of the white and green arc). The FAA is issuing this AD to prevent erroneous information being provided to the pilot, particularly at the lower speed operation limits. The unsafe condition, if not addressed, could result in reduced control of the glider. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions (1) Within 30 days after the effective date of this AD, inspect ASI part number (P/N) IF– W230 or IF–W190 for incorrect markings in accordance with the table in the Appendix, ‘‘2.3. Airspeed Indicator Markings,’’ of Stemme Service Bulletin No. P062–980027, Revision 00, dated December 17, 2018 (the SB). If an ASI marking is incorrect, before further flight, perform one of the following: (i) Replace the ASI by following the Actions, Action 2, of the SB; or (ii) Amend the existing aircraft flight manual (AFM) for your glider by inserting the Appendix, temporary page 2–3 SB, ‘‘2.3. Airspeed Indicator Markings,’’ of the SB. Within 3 months after amending the AFM, replace the ASI by following the Actions, Action 2, of the SB and remove temporary page 2–3 SB, ‘‘2.3. Airspeed Indicator Markings,’’ from the AFM. (2) As of the effective date of this AD, do not install ASI P/N IF–W230 or IF–W190 on any glider unless it has passed the inspection required by this AD. (h) 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 certification office, send it to the attention of the person identified in paragraph (i)(1) of this AD or email: 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. (i) Related Information (1) For more information about this AD, 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; fax: (816) 329–4090; email: jim.rutherford@faa.gov. (2) Refer to European Union Aviation Safety Agency (EASA) AD 2019–0082, dated April 12, 2019, for more information. You may examine the EASA AD in the AD docket at https://www.regulations.gov by searching for and locating it in Docket No. FAA–2021– 0716. (j) 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 the AD specifies otherwise. (i) Stemme Service Bulletin No. P062– 980027, Revision 00, dated December 17, 2018. Note 1 to paragraph (j)(2)(i): This service information has Feb-29 and July 14, 2017, in the footer of every page on the document. Feb-29 refers to the form number and July 14, 2017, is the revision date of the form used to write the service information. The signature block on the bottom of page 1 contains a release date and an approval date. For enforceability purposes, the FAA will cite the Stemme AG service information using the release date of December 17, 2018, that is used in EASA AD 2019–0082, dated April 12, 2019. Note 2 to paragraph (j)(2)(i): This service information contains German to English translation. EASA used the English translation in referencing the document from Stemme AG. For enforceability purposes, the FAA will cite the Stemme AG service information in English as it appears on the document. (ii) [Reserved] (3) For service information identified in this AD, 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. (4) You may view this service information at 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 (816) 329–4148. (5) 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: https://www.archives.gov/federal-register/cfr/ ibr-locations.html. Issued on October 25, 2021. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2021–27774 Filed 12–22–21; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2021–0827; Project Identifier MCAI–2021–00617–T; Amendment 39–21841; AD 2021–24–20] RIN 2120–AA64 Airworthiness Directives; Airbus SAS Airplanes AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final rule. SUMMARY : The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A350–941 and –1041 airplanes. This AD was prompted by reports of slat transmission jams caused by frozen slat geared rotary actuators (SGRAs) at slat 5 track 12. This AD requires repetitive water drainage and plug cleaning of the left- and right-hand SGRAs having a certain part number installed on slat 5 track 12 with certain functional item numbers, 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 is effective January 27, 2022. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of January 27, 2022. ADDRESSES : For material incorporated by reference (IBR) in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 VerDate Sep<11>2014 19:16 Dec 22, 2021 Jkt 256001 PO 00000 Frm 00060 Fmt 4700 Sfmt 4700 E:\FR\FM\23DER1.SGM 23DER1 jspears on DSK121TN23PROD with RULES1