Airworthiness Directives; Airbus Helicopters, 12086-12091 [2021-03688]

Download as PDF 12086 Federal Register / Vol. 86, No. 39 / Tuesday, March 2, 2021 / Rules and Regulations thresholds are exemplary only and not suggestive of requirements. The FDIC will continue to use numerical thresholds to tailor, and otherwise make clear, the applicability of supervisory guidance or programs to supervised institutions, and as required by statute. • Examiners will not criticize through supervisory recommendations (including matters requiring board attention) a supervised financial institution for, and the FDIC will not issue an enforcement action on the basis of, a ‘‘violation’’ of or ‘‘noncompliance’’ with supervisory guidance. In some situations, examiners may reference (including in writing) supervisory guidance to provide examples of safe and sound conduct, appropriate consumer protection and risk management practices, and other actions for addressing compliance with laws or regulations. • Supervisory criticisms should continue to be specific as to practices, operations, financial conditions, or other matters that could have a negative effect on the safety and soundness of the financial institution, could cause consumer harm, or could cause violations of laws, regulations, final agency orders, or other legally enforceable conditions. • The FDIC also has at times sought, and may continue to seek, public comment on supervisory guidance. Seeking public comment on supervisory guidance does not mean that the guidance is intended to be a regulation or have the force and effect of law. The comment process helps the FDIC to improve its understanding of an issue, to gather information on institutions’ risk management practices, or to seek ways to achieve a supervisory objective most effectively and with the least burden on institutions. • The FDIC will aim to reduce the issuance of multiple supervisory guidance documents on the same topic and will generally limit such multiple issuances going forward. The FDIC will continue efforts to make the role of supervisory guidance clear in communications to examiners and to supervised financial institutions and encourage supervised institutions with questions about this statement or any applicable supervisory guidance to discuss the questions with their appropriate agency contact. jbell on DSKJLSW7X2PROD with RULES Federal Deposit Insurance Corporation. By order of the Board of Directors. Dated at Washington, DC, on January 19, 2021. James P. Sheesley, Assistant Executive Secretary. [FR Doc. 2021–01537 Filed 3–1–21; 8:45 am] BILLING CODE 6714–01–P VerDate Sep<11>2014 16:15 Mar 01, 2021 Jkt 253001 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2020–0905; Project Identifier 2019–SW–102–AD; Amendment 39–21384; AD 2021–02–01] RIN 2120–AA64 Airworthiness Directives; Airbus Helicopters Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: The FAA is superseding Airworthiness Directive (AD) 2015–26– 01, which applied to certain Airbus Helicopters Model AS332C1, AS332L1, AS332L2, EC225LP, AS–365N2, AS 365 N3, EC 155B, and EC155B1 helicopters with an energy-absorbing seat. AD 2015–26–01 required inspecting for the presence of labels (placards) that prohibit stowing anything under the seat, and if a label (placard) is missing or not clearly visible to each occupant, installing a label (placard). This AD retains all of the requirements of AD 2015–26–01, and also adds helicopters to the applicability and requires a modification (installing new labels (placards)). This AD was prompted by the determination that additional helicopters are affected by the unsafe condition, and that new labels (placards) are required for all affected helicopters. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective April 6, 2021. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of April 6, 2021. The Director of the Federal Register approved the incorporation by reference of certain other publications listed in this AD as of January 26, 2016 (80 FR 79466, December 22, 2015). ADDRESSES: For service information identified in this final rule, contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052; phone: 972–641–0000 or 800–232–0323; fax: 972–641–3775; or at https:// www.airbus.com/helicopters/services/ support.html. You may view this referenced 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, SUMMARY: PO 00000 Frm 00008 Fmt 4700 Sfmt 4700 call 817–222–5110. It is also available on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2020– 0905. Examining the AD Docket You may examine the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2020– 0905; 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, 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: Kathleen Arrigotti, Aviation Safety Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206–231–3218; email: kathleen.arrigotti@faa.gov. SUPPLEMENTARY INFORMATION: Discussion The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2015–26–01, Amendment 39–18349 (80 FR 79466, December 22, 2015) (AD 2015–26–01). AD 2015–26–01 applied to certain Airbus Helicopters Model AS332C1, AS332L1, AS332L2, EC225LP, AS– 365N2, AS 365 N3, EC 155B, and EC155B1 helicopters with an energyabsorbing seat. The NPRM published in the Federal Register on October 7, 2020 (85 FR 63240). The NPRM was prompted by the discovery that required labels (placards) prohibiting stowage of any object under an energy-absorbing seat had not been systematically installed and the determination that additional helicopters are affected by the unsafe condition, and that new labels (placards) are required for all affected helicopters. The NPRM proposed to continue to require inspecting for the presence of labels (placards) that prohibit stowing anything under the seat, and if a label (placard) is missing or not clearly visible to each occupant, installing a label (placard), and also proposed to add helicopters to the applicability and require a modification (installing new labels (placards)). The FAA is issuing this AD to address any object stowed under an energy-absorbing seat, which could reduce the efficiency of the energy-absorbing function of the seat, E:\FR\FM\02MRR1.SGM 02MRR1 Federal Register / Vol. 86, No. 39 / Tuesday, March 2, 2021 / Rules and Regulations resulting in injury to the seat occupants during an accident. See the MCAI for additional background information. The European Union Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2019–0088R1, dated November 8, 2019 (EASA AD 2019–0088R1) (also referred to as the Mandatory Continuing Airworthiness Information, or the MCAI), to correct an unsafe condition for certain Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, EC225LP, AS–365N2, AS 365 N3, EC 155B and EC155B1 helicopters with an energy-absorbing seat. EASA advised that during certification of an energy-absorbing seat with a new part number, the labels (placards) that require keeping the space under the seat free of any object were not systematically installed. EASA stated that this condition, if not corrected, could prompt occupants to stow objects under an energy-absorbing seat, which would reduce the effectiveness of the seat and the occupants’ chance of surviving an accident. EASA consequently issued AD 2014–0204, dated September 11, 2014; corrected September 12, 2014 (which corresponds to FAA AD 2015–26–01) to require a one-time inspection for the presence of labels (placards) and, if they were missing or unreadable, making and installing labels (placards) prohibiting the placing of an object under an energy absorbing seat. EASA later advised, in EASA AD 2017–0226, dated November 17, 2017 (EASA AD 2017–0226), which superseded EASA AD 2014–0204, that additional new labels (placards) were required and that additional helicopters were affected by the unsafe condition. In this MCAI, which supersedes EASA AD 2017–0226, EASA advised that additional extended compliance times were necessary for certain helicopters. You may examine the MCAI in the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2020– 0905. Comments The FAA gave the public the opportunity to participate in developing this final rule. The FAA received no comments on the NPRM or on the determination of the cost to the public. Conclusion The FAA reviewed the relevant data and determined that air safety and the public interest require adopting this final rule as proposed, except for minor editorial changes. The FAA has determined that these minor changes: • Are consistent with the intent that was proposed in the NPRM for addressing the unsafe condition; and • Do not add any additional burden upon the public than was already proposed in the NPRM. Related Service Information Under 1 CFR Part 51 Airbus Helicopters has issued the following service information. This service information describes procedures for installing new labels (placards) prohibiting stowage of any object under an energy-absorbing seat. These documents are distinct since they apply to different helicopter models. • Airbus Helicopters Alert Service Bulletin No. AS332–25.03.16, Revision 0, dated September 7, 2017. • Airbus Helicopters Alert Service Bulletin No. AS332–25.03.41, Revision 0, dated September 7, 2017. • Airbus Helicopters Alert Service Bulletin No. AS332–25.03.42, Revision 0, dated September 7, 2017. • Airbus Helicopters Alert Service Bulletin No. AS365–25.01.67, Revision 0, dated February 12, 2019. • Airbus Helicopters Alert Service Bulletin No. EC155–25A144, Revision 0, dated February 12, 2019. • Airbus Helicopters Alert Service Bulletin No. EC225–25A179, Revision 1, dated November 6, 2019. • Airbus Helicopters Alert Service Bulletin No. EC225–25A203, Revision 0, dated September 7, 2017. Airbus Helicopters has also issued the following service information. This service information describes procedures for inspecting for labels, placards, or markings that prohibit stowing anything under certain seats and installing a placard. These documents are distinct since they apply to different helicopter models. • Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85, Revision 1, dated September 7, 2017. 12087 • Airbus Helicopters Alert Service Bulletin No. AS365–01.00.66, Revision 1, dated February 12, 2019. • Airbus Helicopters Alert Service Bulletin No. EC155–04A013, Revision 1, dated February 12, 2019. • Airbus Helicopters Alert Service Bulletin No. EC225–04A012, Revision 2, dated November 6, 2019. This AD also requires the following service information, which the Director of the Federal Register approved for incorporation by reference as of January 26, 2016 (80 FR 79466, December 22, 2015). • Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85, Revision 0, dated August 26, 2014. • Airbus Helicopters Alert Service Bulletin No. AS365–01.00.66, Revision 0, dated August 26, 2014. • Airbus Helicopters Alert Service Bulletin No. EC155–04A013, Revision 0, dated August 26, 2014. • Airbus Helicopters Alert Service Bulletin No. EC225–04A012, Revision 0, dated August 26, 2014. 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 the ADDRESSES section. Other Related Service Information Airbus Helicopters issued Airbus Helicopters Alert Service Bulletin No. EC225–04A012, Revision 1, dated September 7, 2017, which describes procedures for inspecting for labels, placards, or markings that prohibit stowing anything under certain seats and installing a placard. Airbus Helicopters has also issued Airbus Helicopters Alert Service Bulletin No. EC225–25A179, Revision 0, dated September 7, 2017, which describes procedures for installing new labels (placards) prohibiting stowage of any object under an energy-absorbing seat. Costs of Compliance The FAA estimates that this AD affects 90 helicopters of U.S. registry. The FAA estimates the following costs to comply with this AD: jbell on DSKJLSW7X2PROD with RULES ESTIMATED COSTS FOR REQUIRED ACTIONS Cost per product Labor cost Inspection (52 Helicopters) (Retained actions from AD 2015–26–01). Install label (placard) (52 Helicopters) (Retained actions from AD 2015–26–01). Inspection (38 Helicopters) (New actions) ...... 1 work-hour × $85 per hour = $85 ................. $0 $85 $4,420 2 work-hours × $85 per hour = $170 ............. Minimal 170 8,840 1 work-hour × $85 per hour = $85 ................. 0 85 3,230 VerDate Sep<11>2014 16:15 Mar 01, 2021 Jkt 253001 PO 00000 Frm 00009 Fmt 4700 Sfmt 4700 Parts cost Cost on U.S. operators Action E:\FR\FM\02MRR1.SGM 02MRR1 12088 Federal Register / Vol. 86, No. 39 / Tuesday, March 2, 2021 / Rules and Regulations ESTIMATED COSTS FOR REQUIRED ACTIONS—Continued Install label (placard) (38 Helicopters) (New actions). Install new label (placard) (New actions) ....... 2 work-hours × $85 per hour = $170 ............. Minimal 170 6,460 2 work-hours × $85 per hour = $170 ............. Minimal 170 15,300 Regulatory Findings The FAA determined that 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 jbell on DSKJLSW7X2PROD with RULES Cost on U.S. operators Labor cost 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. VerDate Sep<11>2014 16:15 Mar 01, 2021 Jkt 253001 Parts cost Cost per product Action 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: (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. § 39.13 List of Subjects in 14 CFR Part 39 (b) Affected ADs Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. This AD replaces AD 2015–26–01, Amendment 39–18349 (80 FR 79466, December 22, 2015) (AD 2015–26–01). Adoption of the Amendment (c) Applicability Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: This AD applies to Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, EC225LP, AS–365N2, AS 365 N3, EC 155B and EC155B1 helicopters, certificated in any category, equipped with at least one energy-absorbing seat listed in figure 1 to paragraph (c) of this AD, except any helicopter embodying the applicable Airbus Helicopters modifications on all applicable seat positions listed in figure 2 to paragraph (c) of this AD. 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. PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 [Amended] 2. The FAA amends § 39.13 by removing Airworthiness Directive (AD) 2015–26–01, Amendment 39–18349 (80 FR 79466, December 22, 2015), and adding the following new AD: ■ 2021–02–01 Airbus Helicopters: Amendment 39–21384; Docket No. FAA–2020–0905; Project Identifier 2019–SW–102–AD. (a) Effective Date This airworthiness directive (AD) is effective April 6, 2021. BILLING CODE 4910–13–P E:\FR\FM\02MRR1.SGM 02MRR1 (d) Subject Air Transport Association (ATA) of America Code 11, Placards and markings. VerDate Sep<11>2014 16:15 Mar 01, 2021 Jkt 253001 (e) Reason This AD was prompted by the discovery that required labels (placards) prohibiting stowage of any object under an energyabsorbing seat had not been systematically PO 00000 Frm 00011 Fmt 4700 Sfmt 4700 installed. The FAA is issuing this AD to address any object stowed under an energyabsorbing seat which could reduce the efficiency of the energy-absorbing function of E:\FR\FM\02MRR1.SGM 02MRR1 ER02MR21.001</GPH> BILLING CODE 4910–13–C 12089 ER02MR21.000</GPH> jbell on DSKJLSW7X2PROD with RULES Federal Register / Vol. 86, No. 39 / Tuesday, March 2, 2021 / Rules and Regulations 12090 Federal Register / Vol. 86, No. 39 / Tuesday, March 2, 2021 / Rules and Regulations the seat, resulting in injury to the seat occupants during an accident. (f) Compliance Comply with this AD within the compliance times specified, unless already done. jbell on DSKJLSW7X2PROD with RULES (g) Retained Inspection and Corrective Actions With Revised Service Information This paragraph restates the requirements of paragraph (e) of AD 2015–26–01, with revised service information. Within 110 hours time in service after January 26, 2016 (the effective date of AD 2015–26–01), do the actions specified in paragraph (g)(1) or (2) of this AD, as applicable for your model helicopter. (1) For Model AS332C1, AS332L1, AS332L2, and EC225LP helicopters: (i) Inspect the cabin and cockpit for labels, placards, or markings that prohibit stowing anything under the seats in the locations shown in the figure in the Appendix of Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85 or No. EC225–04A012, both Revision 0, dated August 26, 2014; or Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85, Revision 1, dated September 7, 2017, or Airbus Helicopters Alert Service Bulletin No. EC225–04A012, Revision 2, dated November 6, 2019; as applicable for your model helicopter. (ii) If a label, placard, or marking is not located in every location depicted in the figure in the Appendix of Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85 or No. EC225–04A012, both Revision 0, dated August 26, 2014; or Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85, Revision 1, dated September 7, 2017, or Airbus Helicopters Alert Service Bulletin No. EC225–04A012, Revision 2, dated November 6, 2019 or is not visible and legible to every occupant, before further flight, install a placard in accordance with the Accomplishment Instructions, paragraph 3.B., of Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85 or No. EC225– 04A012, both Revision 0, dated August 26, 2014; or Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85, Revision 1, dated September 7, 2017, or Airbus Helicopters Alert Service Bulletin No. EC225–04A012, Revision 2, dated November 6, 2019; as applicable for your model helicopter. (2) For Model AS–365N2, AS 365 N3, EC 155B, and EC155B1 helicopters: (i) Inspect each seat leg in the cabin and cockpit for labels, placards, or markings that prohibit stowing anything under the seats. (ii) If a label, placard, or marking does not exist on one leg of each seat or is not visible and legible, before further flight, install a placard in accordance with the Accomplishment Instructions, paragraph 3.B., and the Appendix of Airbus Helicopters Alert Service Bulletin No. AS365–01.00.66 or No. EC155–04A013, both Revision 0, dated August 26, 2014; or Airbus Helicopters Alert Service Bulletin No. AS365–01.00.66 or No. EC155–04A013, both Revision 1, dated February 12, 2019; as applicable for your model helicopter. VerDate Sep<11>2014 16:15 Mar 01, 2021 Jkt 253001 (h) New Inspection and Corrective Actions for Certain Helicopters (1) For Model AS332C and AS332L helicopters: Within 110 hours time in service or 30 days, whichever occurs first, after the effective date of this AD, inspect the cabin and cockpit for labels, placards, or markings that prohibit stowing anything under the seats in the locations shown in the figure in the Appendix of Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85, Revision 1, dated September 7, 2017. (2) If a label, placard, or marking is not located in every location depicted in the figure in the Appendix of Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85, Revision 1, dated September 7, 2017 or is not visible and legible to every occupant, before further flight, install a placard in accordance with the Accomplishment Instructions, paragraph 3.B., of Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85, Revision 1, dated September 7, 2017. (i) New Requirements of This AD: Modification (Install New Placards) (1) At the applicable times specified in paragraph (i)(2) of this AD, install new placards prohibiting stowage of any object under an energy-absorbing seat in accordance with the Accomplishment Instructions, paragraph 3.B., of the applicable service information specified in paragraphs (i)(1)(i) through (vii) of this AD, except you are not required to discard the old labels (placards). Doing the installation required by this paragraph terminates the requirements of paragraphs (g) and (h) of this AD. (i) Airbus Helicopters Alert Service Bulletin No. AS332–25.03.16, Revision 0, dated September 7, 2017. (ii) Airbus Helicopters Alert Service Bulletin No. AS332–25.03.41, Revision 0, dated September 7, 2017. (iii) Airbus Helicopters Alert Service Bulletin No. AS332–25.03.42, Revision 0, dated September 7, 2017. (iv) Airbus Helicopters Alert Service Bulletin No. AS365–25.01.67, Revision 0, dated February 12, 2019. (v) Airbus Helicopters Alert Service Bulletin No. EC155–25A144, Revision 0, dated February 12, 2019. (vi) Airbus Helicopters Alert Service Bulletin No. EC225–25A179, Revision 1, dated November 6, 2019. (vii) Airbus Helicopters Alert Service Bulletin No. EC225–25A203, Revision 0, dated September 7, 2017; as applicable for your model helicopter. (2) At the applicable times specified in paragraph (i)(2)(i) or (ii) of this AD, do the installation required by paragraph (i)(1) of this AD. (i) For Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, AS–365N2, AS 365 N3, EC 155B, EC155B1, and EC225LP helicopters, all manufacturer serial numbers, except Model EC225LP helicopters, manufacturer serial numbers 2663, 2670, 2854, 2883, 2885, 2901 and 2921: Within 110 hours time in service or 6 months, whichever occurs first after the effective date of this AD. (ii) For Model EC225LP helicopters, manufacturer serial numbers 2663, 2670, 2854, 2883, 2885, 2901 and 2921: Within 50 PO 00000 Frm 00012 Fmt 4700 Sfmt 4700 hours time in service or 2 months, whichever occurs first after the effective date of this AD. (j) No Actions Required for Certain Helicopters For Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, and EC225LP helicopters delivered after September 7, 2017: No actions are required, provided that no energy-absorbing seat, as identified in figure 1 to paragraph (c) of this AD, has been installed on that helicopter since delivery. (k) Credit for Previous Actions (1) This paragraph provides credit for the actions specified in paragraph (g) of this AD, if those actions were performed before the effective date of this AD using Airbus Helicopters Alert Service Bulletin No. EC225–04A012, Revision 1, dated September 7, 2017. (2) This paragraph provides credit for the actions specified in paragraphs (i)(1) and (2) of this AD, if those actions were performed before the effective date of this AD using Airbus Helicopters Alert Service Bulletin No. EC225–25A179, Revision 0, dated September 7, 2017. (l) 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 International Validation Branch, send it to the attention of the person identified in paragraph (m)(2) of this AD. Information may be emailed to: 9-AVS-AIR-730-AMOC@ faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/ certificate holding district office. (2) For operations conducted under a 14 CFR part 119 operating certificate or under 14 CFR part 91, subpart K, notify your principal inspector or lacking a principal inspector, the manager of the local flight standards district office or certificate holding district office, before operating any aircraft complying with this AD through an AMOC. (m) Related Information (1) The subject of this AD is addressed in European Union Aviation Safety Agency (EASA) AD 2019–0088R1, dated November 8, 2019. This EASA AD may be found in the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2020–0905. (2) For more information about this AD, contact Kathleen Arrigotti, Aviation Safety Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206–231–3218; email: kathleen.arrigotti@faa.gov. (3) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (n)(5) and (6) of this AD. E:\FR\FM\02MRR1.SGM 02MRR1 jbell on DSKJLSW7X2PROD with RULES Federal Register / Vol. 86, No. 39 / Tuesday, March 2, 2021 / Rules and Regulations (n) 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 April 5, 2021. (i) Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85, Revision 1, dated September 7, 2017. (ii) Airbus Helicopters Alert Service Bulletin No. AS332–25.03.16, Revision 0, dated September 7, 2017. (iii) Airbus Helicopters Alert Service Bulletin No. AS332–25.03.41, Revision 0, dated September 7, 2017. (iv) Airbus Helicopters Alert Service Bulletin No. AS332–25.03.42, Revision 0, dated September 7, 2017. (v) Airbus Helicopters Alert Service Bulletin No. AS365–01.00.66, Revision 1, dated February 12, 2019. (vi) Airbus Helicopters Alert Service Bulletin No. AS365–25.01.67, Revision 0, dated February 12, 2019. (vii) Airbus Helicopters Alert Service Bulletin No. EC155–04A013, Revision 1, dated February 12, 2019. (viii) Airbus Helicopters Alert Service Bulletin No. EC155–25A144, Revision 0, dated February 12, 2019. (ix) Airbus Helicopters Alert Service Bulletin No. EC225–04A012, Revision 2, dated November 6, 2019. (x) Airbus Helicopters Alert Service Bulletin No. EC225–25A179, Revision 1, dated November 6, 2019. (xi) Airbus Helicopters Alert Service Bulletin No. EC225–25A203, Revision 0, dated September 7, 2017. (4) The following service information was approved for IBR on January 26, 2016 (80 FR 79466, December 22, 2015). (i) Airbus Helicopters Alert Service Bulletin No. AS332–01.00.85, Revision 0, dated August 26, 2014. (ii) Airbus Helicopters Alert Service Bulletin No. AS365–01.00.66, Revision 0, dated August 26, 2014. (iii) Airbus Helicopters Alert Service Bulletin No. EC155–04A013, Revision 0, dated August 26, 2014. (iv) Airbus Helicopters Alert Service Bulletin No. EC225–04A012, Revision 0, dated August 26, 2014. (5) For Airbus Helicopters service information identified in this AD, contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052; phone: 972–641– 0000 or 800–232–0323; fax: 972–641–3775; or at https://www.airbus.com/helicopters/ services/technical-support.html. (6) 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. (7) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on VerDate Sep<11>2014 16:15 Mar 01, 2021 Jkt 253001 the availability of this material at NARA, email fedreg.legal@nara.gov, or go to: https:// www.archives.gov/federal-register/cfr/ibrlocations.html. Issued on January 4, 2021. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2021–03688 Filed 3–1–21; 8:45 am] BILLING CODE 4910–13–P FEDERAL TRADE COMMISSION 16 CFR Part 317 [RIN 3084–AB57] Prohibition of Energy Market Manipulation Rule Review Federal Trade Commission. Confirmation of rule. AGENCY: ACTION: The Federal Trade Commission (‘‘Commission’’) has completed its regulatory review of its Prohibition of Energy Market Manipulation Rule implementing Section 811 of Subtitle B of Title VIII of the Energy Independence and Security Act of 2007. This regulatory review is part of the Commission’s periodic review of all its regulations and guides. The Commission has determined to retain the Rule in its present form. DATES: This action is effective March 2, 2021. ADDRESSES: Relevant portions of the record of this proceeding, including this document, are available at https:// www.ftc.gov. FOR FURTHER INFORMATION CONTACT: Peter Richman (202–326–2563), Assistant Director, Mergers III, Bureau of Competition, Federal Trade Commission, 600 Pennsylvania Avenue NW, Washington, DC 20580. SUPPLEMENTARY INFORMATION: SUMMARY: I. Introduction The Commission reviews its rules and guides periodically to seek information about their benefits and costs, as well as their regulatory and economic impact. This information assists the Commission in identifying rules and guides that warrant modification or rescission. Pursuant to this process, on June 5, 2020, the Commission initiated a regulatory rule review by publishing a document in the Federal Register requesting public comment (‘‘Request’’) on the Prohibition of Energy Market Manipulation Rule (‘‘Rule’’).1 The 1 Federal Trade Commission: Rule Review; Request for Public Comment, 85 FR 34548 (June 5, 2020). PO 00000 Frm 00013 Fmt 4700 Sfmt 4700 12091 Commission sought comment on standard regulatory review questions such as whether the Rule continues to serve a useful purpose; the costs and benefits of the Rule for consumers and businesses; and what effects, if any, technological or economic changes have had on the Rule. In addition to generally requesting comments recommending modifications to the Rule, the Commission also invited comment regarding two specific issues. First, the Commission requested comment identifying any evidence § 317.3 of the Rule does not reach behavior that falls within the scope of acts prohibited by its authorizing statute, 42 U.S.C. 17301, and violates the antitrust or consumer protection laws. Second, the Commission invited comment with respect to the definition of ‘‘knowingly’’ in § 317.2(c) of the Rule, its possible limitations, and the appropriateness of a modification of the definition to capture acts, practices, or courses of business a person ‘‘knew or should have known’’ were fraudulent or deceptive. After considering the comments and evidence, the Commission has determined to retain the Rule without modification. II. Background The Rule, authorized by the Energy Independence and Security Act of 2007 (‘‘EISA’’),2 prohibits market manipulation in connection with the purchase or sale of crude oil or petroleum products. The Rule prohibits fraudulent or deceptive conduct (including making false or misleading statements of material fact) in connection with wholesale purchases or sales of crude oil, gasoline, or petroleum distillates. The Rule separately bans the intentional failure to state a material fact when the omission (1) makes the statement misleading and (2) distorts or is likely to distort market conditions for any product covered by the Rule. The Commission issued the Rule on August 6, 2009, with an effective date of November 4, 2009. III. Regulatory Review Comment and Analysis The Commission received one substantive comment, submitted by Eversheds Sutherland (US) LLP (‘‘ESUS’’). ESUS recommends the Commission rescind the Rule. The comment addresses whether there is a continuing need for the Rule and its benefits and costs, but not any of the other questions in the Request. This rule review summarizes the comment and 2 42 U.S.C. 17301–17305. E:\FR\FM\02MRR1.SGM 02MRR1

Agencies

[Federal Register Volume 86, Number 39 (Tuesday, March 2, 2021)]
[Rules and Regulations]
[Pages 12086-12091]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-03688]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0905; Project Identifier 2019-SW-102-AD; Amendment 
39-21384; AD 2021-02-01]
RIN 2120-AA64


Airworthiness Directives; Airbus Helicopters

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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

SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2015-26-
01, which applied to certain Airbus Helicopters Model AS332C1, AS332L1, 
AS332L2, EC225LP, AS-365N2, AS 365 N3, EC 155B, and EC155B1 helicopters 
with an energy-absorbing seat. AD 2015-26-01 required inspecting for 
the presence of labels (placards) that prohibit stowing anything under 
the seat, and if a label (placard) is missing or not clearly visible to 
each occupant, installing a label (placard). This AD retains all of the 
requirements of AD 2015-26-01, and also adds helicopters to the 
applicability and requires a modification (installing new labels 
(placards)). This AD was prompted by the determination that additional 
helicopters are affected by the unsafe condition, and that new labels 
(placards) are required for all affected helicopters. The FAA is 
issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective April 6, 2021.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of April 6, 
2021.
    The Director of the Federal Register approved the incorporation by 
reference of certain other publications listed in this AD as of January 
26, 2016 (80 FR 79466, December 22, 2015).

ADDRESSES: For service information identified in this final rule, 
contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 
75052; phone: 972-641-0000 or 800-232-0323; fax: 972-641-3775; or at 
https://www.airbus.com/helicopters/services/support.html. You may view 
this referenced 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. It is also available on the internet at 
https://www.regulations.gov by searching for and locating Docket No. 
FAA-2020-0905.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-
0905; 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, 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: Kathleen Arrigotti, Aviation Safety 
Engineer, Large Aircraft Section, International Validation Branch, FAA, 
2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-
3218; email: [email protected].

SUPPLEMENTARY INFORMATION: 

Discussion

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 to supersede AD 2015-26-01, Amendment 39-18349 (80 FR 
79466, December 22, 2015) (AD 2015-26-01). AD 2015-26-01 applied to 
certain Airbus Helicopters Model AS332C1, AS332L1, AS332L2, EC225LP, 
AS-365N2, AS 365 N3, EC 155B, and EC155B1 helicopters with an energy-
absorbing seat. The NPRM published in the Federal Register on October 
7, 2020 (85 FR 63240). The NPRM was prompted by the discovery that 
required labels (placards) prohibiting stowage of any object under an 
energy-absorbing seat had not been systematically installed and the 
determination that additional helicopters are affected by the unsafe 
condition, and that new labels (placards) are required for all affected 
helicopters. The NPRM proposed to continue to require inspecting for 
the presence of labels (placards) that prohibit stowing anything under 
the seat, and if a label (placard) is missing or not clearly visible to 
each occupant, installing a label (placard), and also proposed to add 
helicopters to the applicability and require a modification (installing 
new labels (placards)). The FAA is issuing this AD to address any 
object stowed under an energy-absorbing seat, which could reduce the 
efficiency of the energy-absorbing function of the seat,

[[Page 12087]]

resulting in injury to the seat occupants during an accident. See the 
MCAI for additional background information.
    The European Union Aviation Safety Agency (EASA), which is the 
Technical Agent for the Member States of the European Union, has issued 
EASA AD 2019-0088R1, dated November 8, 2019 (EASA AD 2019-0088R1) (also 
referred to as the Mandatory Continuing Airworthiness Information, or 
the MCAI), to correct an unsafe condition for certain Airbus 
Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, EC225LP, 
AS-365N2, AS 365 N3, EC 155B and EC155B1 helicopters with an energy-
absorbing seat. EASA advised that during certification of an energy-
absorbing seat with a new part number, the labels (placards) that 
require keeping the space under the seat free of any object were not 
systematically installed. EASA stated that this condition, if not 
corrected, could prompt occupants to stow objects under an energy-
absorbing seat, which would reduce the effectiveness of the seat and 
the occupants' chance of surviving an accident. EASA consequently 
issued AD 2014-0204, dated September 11, 2014; corrected September 12, 
2014 (which corresponds to FAA AD 2015-26-01) to require a one-time 
inspection for the presence of labels (placards) and, if they were 
missing or unreadable, making and installing labels (placards) 
prohibiting the placing of an object under an energy absorbing seat. 
EASA later advised, in EASA AD 2017-0226, dated November 17, 2017 (EASA 
AD 2017-0226), which superseded EASA AD 2014-0204, that additional new 
labels (placards) were required and that additional helicopters were 
affected by the unsafe condition. In this MCAI, which supersedes EASA 
AD 2017-0226, EASA advised that additional extended compliance times 
were necessary for certain helicopters.
    You may examine the MCAI in the AD docket on the internet at 
https://www.regulations.gov by searching for and locating Docket No. 
FAA-2020-0905.

Comments

    The FAA gave the public the opportunity to participate in 
developing this final rule. The FAA received no comments on the NPRM or 
on the determination of the cost to the public.

Conclusion

    The FAA reviewed the relevant data and determined that air safety 
and the public interest require adopting this final rule as proposed, 
except for minor editorial changes. The FAA has determined that these 
minor changes:
     Are consistent with the intent that was proposed in the 
NPRM for addressing the unsafe condition; and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

    Airbus Helicopters has issued the following service information. 
This service information describes procedures for installing new labels 
(placards) prohibiting stowage of any object under an energy-absorbing 
seat. These documents are distinct since they apply to different 
helicopter models.
     Airbus Helicopters Alert Service Bulletin No. AS332-
25.03.16, Revision 0, dated September 7, 2017.
     Airbus Helicopters Alert Service Bulletin No. AS332-
25.03.41, Revision 0, dated September 7, 2017.
     Airbus Helicopters Alert Service Bulletin No. AS332-
25.03.42, Revision 0, dated September 7, 2017.
     Airbus Helicopters Alert Service Bulletin No. AS365-
25.01.67, Revision 0, dated February 12, 2019.
     Airbus Helicopters Alert Service Bulletin No. EC155-
25A144, Revision 0, dated February 12, 2019.
     Airbus Helicopters Alert Service Bulletin No. EC225-
25A179, Revision 1, dated November 6, 2019.
     Airbus Helicopters Alert Service Bulletin No. EC225-
25A203, Revision 0, dated September 7, 2017.
    Airbus Helicopters has also issued the following service 
information. This service information describes procedures for 
inspecting for labels, placards, or markings that prohibit stowing 
anything under certain seats and installing a placard. These documents 
are distinct since they apply to different helicopter models.
     Airbus Helicopters Alert Service Bulletin No. AS332-
01.00.85, Revision 1, dated September 7, 2017.
     Airbus Helicopters Alert Service Bulletin No. AS365-
01.00.66, Revision 1, dated February 12, 2019.
     Airbus Helicopters Alert Service Bulletin No. EC155-
04A013, Revision 1, dated February 12, 2019.
     Airbus Helicopters Alert Service Bulletin No. EC225-
04A012, Revision 2, dated November 6, 2019.
    This AD also requires the following service information, which the 
Director of the Federal Register approved for incorporation by 
reference as of January 26, 2016 (80 FR 79466, December 22, 2015).
     Airbus Helicopters Alert Service Bulletin No. AS332-
01.00.85, Revision 0, dated August 26, 2014.
     Airbus Helicopters Alert Service Bulletin No. AS365-
01.00.66, Revision 0, dated August 26, 2014.
     Airbus Helicopters Alert Service Bulletin No. EC155-
04A013, Revision 0, dated August 26, 2014.
     Airbus Helicopters Alert Service Bulletin No. EC225-
04A012, Revision 0, dated August 26, 2014.
    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 the ADDRESSES section.

Other Related Service Information

    Airbus Helicopters issued Airbus Helicopters Alert Service Bulletin 
No. EC225-04A012, Revision 1, dated September 7, 2017, which describes 
procedures for inspecting for labels, placards, or markings that 
prohibit stowing anything under certain seats and installing a placard.
    Airbus Helicopters has also issued Airbus Helicopters Alert Service 
Bulletin No. EC225-25A179, Revision 0, dated September 7, 2017, which 
describes procedures for installing new labels (placards) prohibiting 
stowage of any object under an energy-absorbing seat.

Costs of Compliance

    The FAA estimates that this AD affects 90 helicopters of U.S. 
registry. The FAA estimates the following costs to comply with this AD:

                                      Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Inspection (52 Helicopters) (Retained   1 work-hour x $85 per                 $0             $85          $4,420
 actions from AD 2015-26-01).            hour = $85.
Install label (placard) (52             2 work-hours x $85 per           Minimal             170           8,840
 Helicopters) (Retained actions from     hour = $170.
 AD 2015-26-01).
Inspection (38 Helicopters) (New        1 work-hour x $85 per                  0              85           3,230
 actions).                               hour = $85.

[[Page 12088]]

 
Install label (placard) (38             2 work-hours x $85 per           Minimal             170           6,460
 Helicopters) (New actions).             hour = $170.
Install new label (placard) (New        2 work-hours x $85 per           Minimal             170          15,300
 actions).                               hour = $170.
----------------------------------------------------------------------------------------------------------------

Authority for This Rulemaking

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

Regulatory Findings

    The FAA determined that this 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:
    (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.

Adoption of 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

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 removing Airworthiness Directive (AD) 
2015-26-01, Amendment 39-18349 (80 FR 79466, December 22, 2015), and 
adding the following new AD:

2021-02-01 Airbus Helicopters: Amendment 39-21384; Docket No. FAA-
2020-0905; Project Identifier 2019-SW-102-AD.

(a) Effective Date

    This airworthiness directive (AD) is effective April 6, 2021.

(b) Affected ADs

    This AD replaces AD 2015-26-01, Amendment 39-18349 (80 FR 79466, 
December 22, 2015) (AD 2015-26-01).

(c) Applicability

    This AD applies to Airbus Helicopters Model AS332C, AS332C1, 
AS332L, AS332L1, AS332L2, EC225LP, AS-365N2, AS 365 N3, EC 155B and 
EC155B1 helicopters, certificated in any category, equipped with at 
least one energy-absorbing seat listed in figure 1 to paragraph (c) 
of this AD, except any helicopter embodying the applicable Airbus 
Helicopters modifications on all applicable seat positions listed in 
figure 2 to paragraph (c) of this AD.
BILLING CODE 4910-13-P

[[Page 12089]]

[GRAPHIC] [TIFF OMITTED] TR02MR21.000

[GRAPHIC] [TIFF OMITTED] TR02MR21.001

BILLING CODE 4910-13-C

(d) Subject

    Air Transport Association (ATA) of America Code 11, Placards and 
markings.

(e) Reason

    This AD was prompted by the discovery that required labels 
(placards) prohibiting stowage of any object under an energy-
absorbing seat had not been systematically installed. The FAA is 
issuing this AD to address any object stowed under an energy-
absorbing seat which could reduce the efficiency of the energy-
absorbing function of

[[Page 12090]]

the seat, resulting in injury to the seat occupants during an 
accident.

(f) Compliance

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

(g) Retained Inspection and Corrective Actions With Revised Service 
Information

    This paragraph restates the requirements of paragraph (e) of AD 
2015-26-01, with revised service information. Within 110 hours time 
in service after January 26, 2016 (the effective date of AD 2015-26-
01), do the actions specified in paragraph (g)(1) or (2) of this AD, 
as applicable for your model helicopter.
    (1) For Model AS332C1, AS332L1, AS332L2, and EC225LP 
helicopters:
    (i) Inspect the cabin and cockpit for labels, placards, or 
markings that prohibit stowing anything under the seats in the 
locations shown in the figure in the Appendix of Airbus Helicopters 
Alert Service Bulletin No. AS332-01.00.85 or No. EC225-04A012, both 
Revision 0, dated August 26, 2014; or Airbus Helicopters Alert 
Service Bulletin No. AS332-01.00.85, Revision 1, dated September 7, 
2017, or Airbus Helicopters Alert Service Bulletin No. EC225-04A012, 
Revision 2, dated November 6, 2019; as applicable for your model 
helicopter.
    (ii) If a label, placard, or marking is not located in every 
location depicted in the figure in the Appendix of Airbus 
Helicopters Alert Service Bulletin No. AS332-01.00.85 or No. EC225-
04A012, both Revision 0, dated August 26, 2014; or Airbus 
Helicopters Alert Service Bulletin No. AS332-01.00.85, Revision 1, 
dated September 7, 2017, or Airbus Helicopters Alert Service 
Bulletin No. EC225-04A012, Revision 2, dated November 6, 2019 or is 
not visible and legible to every occupant, before further flight, 
install a placard in accordance with the Accomplishment 
Instructions, paragraph 3.B., of Airbus Helicopters Alert Service 
Bulletin No. AS332-01.00.85 or No. EC225-04A012, both Revision 0, 
dated August 26, 2014; or Airbus Helicopters Alert Service Bulletin 
No. AS332-01.00.85, Revision 1, dated September 7, 2017, or Airbus 
Helicopters Alert Service Bulletin No. EC225-04A012, Revision 2, 
dated November 6, 2019; as applicable for your model helicopter.
    (2) For Model AS-365N2, AS 365 N3, EC 155B, and EC155B1 
helicopters:
    (i) Inspect each seat leg in the cabin and cockpit for labels, 
placards, or markings that prohibit stowing anything under the 
seats.
    (ii) If a label, placard, or marking does not exist on one leg 
of each seat or is not visible and legible, before further flight, 
install a placard in accordance with the Accomplishment 
Instructions, paragraph 3.B., and the Appendix of Airbus Helicopters 
Alert Service Bulletin No. AS365-01.00.66 or No. EC155-04A013, both 
Revision 0, dated August 26, 2014; or Airbus Helicopters Alert 
Service Bulletin No. AS365-01.00.66 or No. EC155-04A013, both 
Revision 1, dated February 12, 2019; as applicable for your model 
helicopter.

(h) New Inspection and Corrective Actions for Certain Helicopters

    (1) For Model AS332C and AS332L helicopters: Within 110 hours 
time in service or 30 days, whichever occurs first, after the 
effective date of this AD, inspect the cabin and cockpit for labels, 
placards, or markings that prohibit stowing anything under the seats 
in the locations shown in the figure in the Appendix of Airbus 
Helicopters Alert Service Bulletin No. AS332-01.00.85, Revision 1, 
dated September 7, 2017.
    (2) If a label, placard, or marking is not located in every 
location depicted in the figure in the Appendix of Airbus 
Helicopters Alert Service Bulletin No. AS332-01.00.85, Revision 1, 
dated September 7, 2017 or is not visible and legible to every 
occupant, before further flight, install a placard in accordance 
with the Accomplishment Instructions, paragraph 3.B., of Airbus 
Helicopters Alert Service Bulletin No. AS332-01.00.85, Revision 1, 
dated September 7, 2017.

(i) New Requirements of This AD: Modification (Install New Placards)

    (1) At the applicable times specified in paragraph (i)(2) of 
this AD, install new placards prohibiting stowage of any object 
under an energy-absorbing seat in accordance with the Accomplishment 
Instructions, paragraph 3.B., of the applicable service information 
specified in paragraphs (i)(1)(i) through (vii) of this AD, except 
you are not required to discard the old labels (placards). Doing the 
installation required by this paragraph terminates the requirements 
of paragraphs (g) and (h) of this AD.
    (i) Airbus Helicopters Alert Service Bulletin No. AS332-
25.03.16, Revision 0, dated September 7, 2017.
    (ii) Airbus Helicopters Alert Service Bulletin No. AS332-
25.03.41, Revision 0, dated September 7, 2017.
    (iii) Airbus Helicopters Alert Service Bulletin No. AS332-
25.03.42, Revision 0, dated September 7, 2017.
    (iv) Airbus Helicopters Alert Service Bulletin No. AS365-
25.01.67, Revision 0, dated February 12, 2019.
    (v) Airbus Helicopters Alert Service Bulletin No. EC155-25A144, 
Revision 0, dated February 12, 2019.
    (vi) Airbus Helicopters Alert Service Bulletin No. EC225-25A179, 
Revision 1, dated November 6, 2019.
    (vii) Airbus Helicopters Alert Service Bulletin No. EC225-
25A203, Revision 0, dated September 7, 2017; as applicable for your 
model helicopter.
    (2) At the applicable times specified in paragraph (i)(2)(i) or 
(ii) of this AD, do the installation required by paragraph (i)(1) of 
this AD.
    (i) For Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, AS-
365N2, AS 365 N3, EC 155B, EC155B1, and EC225LP helicopters, all 
manufacturer serial numbers, except Model EC225LP helicopters, 
manufacturer serial numbers 2663, 2670, 2854, 2883, 2885, 2901 and 
2921: Within 110 hours time in service or 6 months, whichever occurs 
first after the effective date of this AD.
    (ii) For Model EC225LP helicopters, manufacturer serial numbers 
2663, 2670, 2854, 2883, 2885, 2901 and 2921: Within 50 hours time in 
service or 2 months, whichever occurs first after the effective date 
of this AD.

(j) No Actions Required for Certain Helicopters

    For Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, and EC225LP 
helicopters delivered after September 7, 2017: No actions are 
required, provided that no energy-absorbing seat, as identified in 
figure 1 to paragraph (c) of this AD, has been installed on that 
helicopter since delivery.

(k) Credit for Previous Actions

    (1) This paragraph provides credit for the actions specified in 
paragraph (g) of this AD, if those actions were performed before the 
effective date of this AD using Airbus Helicopters Alert Service 
Bulletin No. EC225-04A012, Revision 1, dated September 7, 2017.
    (2) This paragraph provides credit for the actions specified in 
paragraphs (i)(1) and (2) of this AD, if those actions were 
performed before the effective date of this AD using Airbus 
Helicopters Alert Service Bulletin No. EC225-25A179, Revision 0, 
dated September 7, 2017.

(l) 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 International Validation Branch, send it to the 
attention of the person identified in paragraph (m)(2) 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 
local flight standards district office/certificate holding district 
office.
    (2) For operations conducted under a 14 CFR part 119 operating 
certificate or under 14 CFR part 91, subpart K, notify your 
principal inspector or lacking a principal inspector, the manager of 
the local flight standards district office or certificate holding 
district office, before operating any aircraft complying with this 
AD through an AMOC.

(m) Related Information

    (1) The subject of this AD is addressed in European Union 
Aviation Safety Agency (EASA) AD 2019-0088R1, dated November 8, 
2019. This EASA AD may be found in the AD docket on the internet at 
https://www.regulations.gov by searching for and locating Docket No. 
FAA-2020-0905.
    (2) For more information about this AD, contact Kathleen 
Arrigotti, Aviation Safety Engineer, Large Aircraft Section, 
International Validation Branch, FAA, 2200 South 216th St., Des 
Moines, WA 98198; phone and fax: 206-231-3218; email: 
[email protected].
    (3) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (n)(5) and (6) of this AD.

[[Page 12091]]

(n) 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 
April 5, 2021.
    (i) Airbus Helicopters Alert Service Bulletin No. AS332-
01.00.85, Revision 1, dated September 7, 2017.
    (ii) Airbus Helicopters Alert Service Bulletin No. AS332-
25.03.16, Revision 0, dated September 7, 2017.
    (iii) Airbus Helicopters Alert Service Bulletin No. AS332-
25.03.41, Revision 0, dated September 7, 2017.
    (iv) Airbus Helicopters Alert Service Bulletin No. AS332-
25.03.42, Revision 0, dated September 7, 2017.
    (v) Airbus Helicopters Alert Service Bulletin No. AS365-
01.00.66, Revision 1, dated February 12, 2019.
    (vi) Airbus Helicopters Alert Service Bulletin No. AS365-
25.01.67, Revision 0, dated February 12, 2019.
    (vii) Airbus Helicopters Alert Service Bulletin No. EC155-
04A013, Revision 1, dated February 12, 2019.
    (viii) Airbus Helicopters Alert Service Bulletin No. EC155-
25A144, Revision 0, dated February 12, 2019.
    (ix) Airbus Helicopters Alert Service Bulletin No. EC225-04A012, 
Revision 2, dated November 6, 2019.
    (x) Airbus Helicopters Alert Service Bulletin No. EC225-25A179, 
Revision 1, dated November 6, 2019.
    (xi) Airbus Helicopters Alert Service Bulletin No. EC225-25A203, 
Revision 0, dated September 7, 2017.
    (4) The following service information was approved for IBR on 
January 26, 2016 (80 FR 79466, December 22, 2015).
    (i) Airbus Helicopters Alert Service Bulletin No. AS332-
01.00.85, Revision 0, dated August 26, 2014.
    (ii) Airbus Helicopters Alert Service Bulletin No. AS365-
01.00.66, Revision 0, dated August 26, 2014.
    (iii) Airbus Helicopters Alert Service Bulletin No. EC155-
04A013, Revision 0, dated August 26, 2014.
    (iv) Airbus Helicopters Alert Service Bulletin No. EC225-04A012, 
Revision 0, dated August 26, 2014.
    (5) For Airbus Helicopters service information identified in 
this AD, contact Airbus Helicopters, 2701 N Forum Drive, Grand 
Prairie, TX 75052; phone: 972-641-0000 or 800-232-0323; fax: 972-
641-3775; or at https://www.airbus.com/helicopters/services/technical-support.html.
    (6) 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.
    (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: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on January 4, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2021-03688 Filed 3-1-21; 8:45 am]
BILLING CODE 4910-13-P
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