AD 2021-16-06

The FAA is superseding Airworthiness Directive (AD) 2020-19-11 for certain Leonardo S.p.a. Model A119 and AW119 MKII helicopters. AD 2020-19-11 required repetitive borescope inspections of the 90-degree tail rotor gearbox (TGB) and depending on the inspection results, removing the TGB from service. This AD was prompted by the determination that additional parts may be susceptible to the unsafe condition. This AD retains \n\n((Page 46960)) \n\nthe inspection requirements of AD 2020-19-11, and revises the compliance time and applicability. The FAA is issuing this AD to address the unsafe condition on these products.

Final rule.

The Amendment \n\n\n\tAccordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n0 1. The authority citation for part 39 continues to read as follows: \n\n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\n\n\nSec. 39.13 (Amended) \n\n0 2. The FAA amends Sec. 39.13 by: 0 a. Removing Airworthiness Directive 2020-19-11, Amendment 39-21254 (85 FR 59404, September 22, 2020); and 0 b. Adding the following new airworthiness directive: \n\n2021-16-06 Leonardo S.p.a.: Amendment 39-21668; Docket No. FAA-2021- 0373; Project Identifier MCAI-2020-01352-R. \n\n(a) Effective Date \n\n\n\tThis airworthiness directive (AD) is effective September 27, 2021. \n\n(b) Affected ADs \n\n\n\tThis AD replaces AD 2020-19-11, Amendment 39-21254 (85 FR 59404, September 22, 2020). \n\n(c) Applicability \n\n\n\tThis AD applies to Leonardo S.p.a. Model A119 and AW119 MKII helicopters, certificated in any category, with 90-degree tail rotor gearbox (TGB) part number (P/N) 109-0440-06-101 or 109-0440-06-105, and with TGB shaft P/N 109-0443-03-107 having a serial number (S/N) listed in Table 1 of Leonardo Helicopters Alert Service Bulletin No. 119-090, Revision A, dated September 14, 2020 (ASB 119-090), installed. \n\tNote 1 to paragraph (c): A TGB shaft is also referred to as a mast gear assembly. \n\n(d) Subject \n\n\n\tJoint Aircraft Service Component (JASC) Code: 6510, Tail Rotor Drive Shaft. \n\n(e) Unsafe Condition \n\n\n\tThis AD was prompted by two occurrences of corrosion on the internal surface of the TGB shaft. The FAA is issuing this AD to detect corrosion of the TGB shaft. The unsafe condition, if not addressed, could result in failure of the tail rotor, possibly resulting in reduced control of the helicopter. \n\n(f) Compliance \n\n\n\tComply with this AD within the compliance times specified, unless already done. \n\n(g) Required Actions \n\n\n\t(1) Within 25 hours time-in-service (TIS) or 3 months, whichever occurs first after the effective date of this AD, and thereafter at intervals not to exceed 6 months, borescope inspect the entire internal surface of the TGB shaft for corrosion. Refer to Detail A of Figure 1 of ASB 119-090, for a depiction of the entry point for the borescope. If there is corrosion, before further flight, remove the TGB from service. \n\t(2) As of the effective date of this AD, do not install on any helicopter any TGB P/N 109-0440-06-101 or 109-0440-06-105 that has TGB shaft P/N 109-0443-03-107 having an S/N listed in Table 1 of ASB 119-090, unless the actions required by paragraph (g)(1) of this AD have been accomplished. \n\n(h) Special Flight Permits \n\n\n\tA special flight permit may be permitted provided that there are no passengers onboard. \n\n(i) Alternative Methods of Compliance (AMOCs) \n\n\n\t(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 (j)(1) of this AD. Information may be emailed to: 9-AVS-AIR-730-AMOC@faa.gov. \n\t(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. \n\n(j) Related Information \n\n\n\t(1) For more information about this AD, contact Rao Edupuganti, Aerospace Engineer, Dynamic Systems Section, Technical Innovation Policy Branch, Policy & Innovation Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5110; email rao.edupuganti@faa.gov. \n\t(2) The subject of this AD is addressed in European Union Aviation Safety Agency (EASA) AD 2020-0206, dated September 30, 2020. You may view the EASA AD at https://www.regulations.gov in Docket No. FAA-2021-0373. \n\n(k) Material Incorporated by Reference \n\n\n\t(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. \n\t(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. \n\t(i) Leonardo Helicopters Alert Service Bulletin No. 119-090, Revision A, dated September 14, 2020. \n\t(ii) (Reserved) \n\t(3) For service information identified in this AD, 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://customerportal.leonardocompany.com/en-US/. \n\t(4) You may view this service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222-5110. \n\t(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: fedreg.legal@nara.gov, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html. \n\n\n\tIssued on August 16, 2021. Ross Landes, Deputy Director for Regulatory Operations, Compliance & Airworthiness Division, Aircraft Certification Service. (FR Doc. 2021-17951 Filed 8-20-21; 8:45 am) BILLING CODE 4910-13-P

Background \n\n\n\tThe FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2020-19-11, Amendment 39-21254 (85 FR 59404, September 22, 2020) (AD 2020-19-11). AD 2020-19-11 applied to Leonardo S.p.a. Model A119 and AW119 MKII helicopters with TGB part number (P/N) 109-0440-06-101 or P/N 109-0440-06-105 having serial number (S/N) 167, 169 through 172 inclusive, 215 through 225 inclusive, 227, 230, 232, 233, AW268, K3, K16, M47, or L29, installed. The NPRM published in the Federal Register on May 21, 2021 (86 FR 27538). In the NPRM, the FAA proposed to retain certain requirements of AD 2020-19-11, revise the compliance time for the repetitive inspections from intervals not to exceed 100 hours time-in-service (TIS) or 6 months to only intervals not to exceed 6 months, and revise the applicability paragraph by adding certain serial-numbered TGB shafts. The NPRM was prompted by EASA AD 2020-0206, dated September 30, 2020 (EASA AD 2020- 0206), issued by EASA, which is the Technical Agent for the Member States of the European Union, to correct an unsafe condition for Leonardo S.p.A. Helicopters, formerly Finmeccanica S.p.A., AgustaWestland S.p.A., Agusta S.p.A.; and AgustaWestland Philadelphia Corporation, formerly Agusta Aerospace Corporation. EASA advises that additional parts may be susceptible to similar occurrences and some TGB shafts could have been reinstalled on a TGB other than the one on which they were initially installed. This condition, if not addressed, could result in failure of the tail rotor, possibly resulting in reduced control of the helicopter. \n\tAccordingly, EASA AD 2020-0206 retains the inspection requirements of EASA AD 2018-0156, dated July 24, 2018, which prompted AD 2020-19- 11, for certain part-numbered TGB shafts and revises the definition of an affected part by adding certain serial-numbered TGB shafts. \n\nDiscussion of Final Airworthiness Directive \n\nComments \n\n\n\tThe FAAreceived no comments on the NPRM or on the determination of the costs. \n\nConclusion \n\n\n\tThese 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 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 helicopters. \n\nRelated Service Information Under 1 CFR Part 51 \n\n\n\tThe FAA reviewed Leonardo Helicopters Alert Service Bulletin No. 119-090, Revision A, dated September 14, 2020. This service information specifies procedures for conducting an endoscope inspection of the internal surface of the TGB output shaft for corrosion. This service information also specifies replacing the TGB if corrosion is found. \n\tThis 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. \n\nInterim Action \n\n\n\tThe FAA considers this AD to be an interim action. \n\nDifferences Between This AD and the EASA AD \n\n\n\tEASA AD 2020-0206 uses flight hours to describe one compliance time, whereas this AD uses hours TIS. EASA AD 2020-0206 requires using an endoscope for inspection, whereas this AD requires inspecting with a borescope. EASA AD 2020-0206 defines the affected part as the 90-degree TGB shaft installed on TGB P/N 109-0440-06-01-101, whereas the applicability paragraph of this AD includes TGB P/N 109-0440-06-101 instead. \n\nCosts of Compliance \n\n\n\tThe FAA estimates that this AD affects 134 helicopters of U.S. Registry. Labor rates are estimated at $85 per work-hour. Based on these numbers, the FAA estimates the following costs to comply with this AD. \n\tBorescope inspecting the TGB output shaft takes about 3 work-hours for an estimatedcost of $255 per helicopter and $34,170 for the U.S. fleet per inspection cycle. \n\tReplacing a TGB takes about 18 work-hours and parts cost about $49,000 (overhauled TGB) for an estimated cost of $50,530 per helicopter. \n\tThe 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. \n\nAuthority for This Rulemaking \n\n\n\tTitle 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. \n\tThe FAA is issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: General requirements. Under \n\n((Page 46961)) \n\nthat 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. \n\nRegulatory Findings \n\n\n\tThis 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. \n\tFor the reasons discussed above, I certify that this AD: \n\t(1) Is not a ''significant regulatory action'' under Executive Order 12866, \n\t(2) Will not affect intrastate aviation in Alaska, and \n\t(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. \n\nList of Subjects in 14 CFR Part 39 \n\n\n\tAir transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.