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        DEPARTMENT OF TRANSPORTATION 
         
        Federal Aviation Administration 
         
        14 CFR Part 39 
         
        [Docket No. FAA-2020-0554; Product Identifier 2016-SW-088-AD; Amendment 
         
        39-21245; AD 2020-19-04] 
        RIN 2120-AA64 
         
        Airworthiness Directives; Leonardo S.p.a. Helicopters 
         
        AGENCY: Federal Aviation Administration (FAA), DOT. 
         
        ACTION: Final rule. 
         
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        SUMMARY: The FAA is adopting a new airworthiness directive (AD) 
        for  
        Leonardo S.p.a. (Leonardo) Model AB139 and AW139 helicopters. This AD 
         
        requires removing certain main gearbox (MGB) input modules from  
        service. This AD was prompted by the discovery that a batch of duplex 
         
        bearings, which are installed on the MGB input modules, are defective. 
         
        The actions of this AD are intended to address an unsafe condition on 
         
        these products. 
         
        DATES: This AD is effective October 15, 2020. 
         
        ADDRESSES: For service information identified in this final rule, 
         
        contact Leonardo S.p.a. Helicopters, Emanuele Bufano, Head of  
        Airworthiness, Viale G.Agusta 520, 21017 C.Costa di Samarate (Va)  
        Italy; telephone +39-0331-225074; fax +39-0331-229046; or at https://www.leonardocompany.com/en/home. 
        You may view this service  
        information at the FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177. For 
         
        information on the availability of this material at the FAA, call 817-222-5110. 
         
        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- 
        0554; 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 AD, the European Aviation Safety Agency (now European Union  
        Aviation Safety Agency) (EASA) AD, 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: Rao Edupuganti, Aviation Safety 
         
        Engineer, Regulations and Policy Section, Rotorcraft Standards Branch, 
         
        FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222- 
        5110; email rao.edupuganti@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 Leonardo Model AB139  
        and AW139 helicopters with certain serial-numbered MGB input modules  
        part number (P/N) 3K6320A00135 or P/N 3K6320A00136 installed. The NPRM 
         
        published in the Federal Register on June 8, 2020 (85 FR 35018). The  
        NPRM proposed to require removing the affected MGB input modules from 
         
        service and prohibit installing the affected MGB input modules. The  
        proposed requirements were intended to address defective duplex  
        bearings on MGB input modules, which could result in damage including 
         
        corrosion and cracking, which could result in excessive heat of the  
        input module duplex ball bearing inner race and subsequent loss of  
        engine power and loss of helicopter control. 
        The NPRM was prompted by EASA AD No. 2016-0255R1, dated January 17,  
        2017 (EASA AD 2016-0255R1), issued by EASA, which is the Technical  
        Agent for the Member States of the European Union, to correct an unsafe 
         
        condition for Leonardo (formerly Finmeccanica S.p.A., AgustaWestland  
        Philadelphia Corporation, Agusta Aerospace Corporation) Model AB139 and 
         
        AW139 helicopters with certain serial-numbered MGB input modules P/N  
        3K6320A00135 or P/N 3K6320A00136 installed. EASA advises that the  
        supplier of a batch of duplex bearings installed on MGB input modules 
         
        reported that the bearings were defective, due to a quality control  
        issue. This condition, if not detected or corrected, could lead to  
        damage of the input module duplex ball bearing inner race, possibly  
        resulting in loss of engine power and reduced control of the  
        helicopter. Accordingly, EASA AD 2016-0255R1 requires removing the  
        affected MGB input modules from service. 
         
        Comments 
         
        The FAA gave the public the opportunity to participate in  
        developing this final rule. The FAA received one comment in support of 
         
        the NPRM. 
         
        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 about the 
         
        unsafe condition described in its AD. The FAA is issuing this AD after 
         
        evaluating all known relevant information and determining that an  
        unsafe condition is likely to exist or develop on other helicopters of 
         
        the same type designs. 
         
        Differences Between This AD and the EASA AD 
         
        The EASA AD requires returning affected parts and sending  
        information to Leonardo; however, this AD does not. 
         
        Related Service Information 
         
        The FAA reviewed Leonardo Helicopters Bollettino Tecnico No. 139- 
        303, dated September 20, 2016, which specifies replacing certain duplex 
         
        bearings on MGB left-hand and right-hand input modules on Model AB139 
         
        and AW139 helicopters. 
         
        Costs of Compliance 
         
        The FAA estimates that this AD affects 71 helicopters of U.S.  
        Registry. The FAA estimates that operators may incur the following  
        costs in order to comply with this AD. Labor costs are estimated at $85 
         
        per work-hour. 
        Replacing one input module takes about 60 work-hours and parts cost  
        about $84,847 for an estimated cost of $89,947 per input module.  
        Replacing two input modules takes about 100 work-hours and parts cost 
         
        about $169,694 for an estimated cost of $178,194 per two input modules. 
         
        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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