|  DEPARTMENT OF TRANSPORTATION
 Federal Aviation Administration
 
 14 CFR Part 39
 
 [Docket No. FAA-2020-0239; Product Identifier 2018-SW-073-AD; Amendment
 39-21136; AD 2020-12-02]
 RIN 2120-AA64
 
 Airworthiness Directives; Airbus Helicopters
 
 AGENCY: Federal Aviation Administration (FAA), Department of
 Transportation (DOT).
 
 ACTION: Final rule.
 
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 SUMMARY: The FAA is adopting a new airworthiness directive (AD) 
        for all
 Airbus Helicopters Model EC120B helicopters. This AD was prompted by a
 report that a changed manufacturing process for the tail rotor blades
 (TRB) was implemented, affecting the structural characteristics of the
 blades and generating a new part number for these blades. This AD
 requires re-identifying each affected TRB having a certain part number
 and serial number and establishing a life limit for the new part
 numbers. This AD also prohibits installation of any affected TRB
 identified with the old part number on any helicopter. The FAA is
 issuing this AD to address the unsafe condition on these products.
 
 DATES: This AD is effective July 13, 2020.
 The Director of the Federal Register approved the incorporation by
 reference of a certain publication listed in this AD as of July 13,
 2020.
 
 ADDRESSES: For service information identified in this final rule,
 contact Airbus Helicopters, 2701 N 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 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-2020-0239.
 
 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-
 0239; 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: Kristi Bradley, Aviation Safety
 Engineer, Safety Management Section, Rotorcraft Standards Branch, FAA,
 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222-5485;
 email Kristin.Bradley@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 Airbus Helicopters
 Model EC120B helicopters. The NPRM published in the Federal Register on
 March 11, 2020 (85 FR 14178). The NPRM was prompted by a report that a
 changed manufacturing process for the TRB was implemented, affecting
 the structural characteristics of the blades and generating a new part
 number for these blades. The NPRM proposed to require re-identifying
 each affected TRB having a certain part number and serial number and
 establishing a life limit for the new part numbers. The NPRM also
 proposed to prohibit installation of any affected TRB identified with
 the old part number on any helicopter. The FAA is issuing this AD to
 ensure the new part number (P/N) TRBs do not exceed their life limit,
 which could lead to loss of the TRB and subsequent loss of control of
 the helicopter.
 The European Aviation Safety Agency (now European Union Aviation
 Safety Agency) (EASA), which is the Technical Agent for the Member
 States of the European Union, has issued EASA AD 2018-0183, dated
 August 28, 2018 (also referred to as the Mandatory Continuing
 Airworthiness Information, or ``the MCAI''), to correct an unsafe
 condition for all Airbus Helicopters Model EC120B 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-2020-0239.
 
 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 Alert Service Bulletin EC120-04A008,
 Revision 0, dated July 18, 2018 (``ASB EC120-04A008''). This service
 information describes procedures for re-identifying a TRB with P/N
 C642A0300103 for certain serial numbers as specified in ASB EC120-
 04A008. 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.
 
 Costs of Compliance
 
 The FAA estimates that this AD affects 94 helicopters of U.S.
 registry. The FAA estimates the following costs to comply with this AD:
 
 
 Estimated Costs for Required Actions *
 
 
         
          | Labor cost | Parts cost | Cost per 
              product | Cost on 
              U.S. operators |   
          | 1 work-hour x $85 per hour = 
            $85 | $0 ** | $85 | $7,990 * |   * The FAA has received no definitive 
        data that would enable providing cost estimates for the additional applicable maintenance instructions specified 
        in
 this AD.
 ** The FAA has received no definitive data on the parts 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.
 
 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:
 (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
 
 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]
 
 2. The FAA amends Sec. 39.13 by adding the following new airworthiness
 directive (AD):
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