AD 2021-16-09

The FAA is adopting a new airworthiness directive (AD) for certain Leonardo S.p.a. Model AW189 helicopters. This AD was prompted by corrosion on the inlet check valve banjo fitting of emergency flotation system (EFS) float assemblies. This AD requires visually inspecting each banjo fitting installed on an affected EFS float assembly, and depending on the results, removing the banjo fitting from service. This AD also requires applying corrosion inhibiting compound and prohibits installing an affected EFS float assembly unless certain requirements have been accomplished as specified in a European Aviation Safety Agency (now European Union Aviation Safety Agency) (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

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 adding the following new airworthiness directive: \n\n2021-16-09 Leonardo S.p.a.: Amendment 39-21671; Docket No. FAA-2021- 0383; Project Identifier 2018-SW-005-AD. \n\n(a) Effective Date \n\n\n\tThis airworthiness directive (AD) is effective October 13, 2021. \n\n(b) Affected ADs \n\n\n\tNone. \n\n(c) Applicability \n\n\n\tThis AD applies to Leonardo S.p.a. Model AW189 helicopters, certificated in any category, as identified in European Aviation Safety Agency (now European Union Aviation Safety Agency) (EASA) AD 2018-0006, dated January 10, 2018 (EASA AD 2018-0006). \n\n(d) Subject \n\n\n\tJoint Aircraft Service Component (JASC)Code: 3212, Emergency Flotation Section. \n\n(e) Unsafe Condition \n\n\n\tThis AD was prompted by corrosion on the inlet check valve banjo fitting of emergency flotation system (EFS) float assemblies. The FAA is issuing this AD to prevent reduced inflation of an EFS float. The unsafe condition, if not addressed, could affect the helicopter's buoyancy during an emergency landing on water. \n\n(f) Compliance \n\n\n\tComply with this AD within the compliance times specified, unless already done. \n\n(g) Requirements \n\n\n\tExcept as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2018-0006. \n\n(h) Exceptions to EASA AD 2018-0006 \n\n\n\t(1) Where EASA AD 2018-0006 refers to December 29, 2017 (the effective date of EASA AD 2017-0256, dated December 22, 2017), this AD requires using the effective date of this AD. \n\t(2) Where the service information referenced in EASA AD 2018- 0006 specifies to return acertain part, this AD requires removing that part from service. \n\t(3) Where the service information referenced in EASA AD 2018- 0006 specifies to discard certain parts, this AD requires removing those parts from service. \n\t(4) The ''Remarks'' section of EASA AD 2018-0006 does not apply to this AD. \n\n(i) No Reporting Requirement \n\n\n\tAlthough the service information referenced in EASA AD 2018-0006 specifies to submit certain information to the manufacturer, this AD does not include that requirement. \n\n(j) 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 \n\n((Page 50237)) \n\nFlight Standards District Office, as appropriate. If sending information directly to the manager of the International Validation Branch, send it to the attentionof the person identified in paragraph (k) 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(k) Related Information \n\n\n\tFor more information about this AD, contact Kristi Bradley, Program Manager, COS Program Management Section, Operational Safety Branch, Compliance & Airworthiness Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5110; email kristin.bradley@faa.gov. \n\n(l) Material Incorporated by Reference \n\n\n\t(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. \n\t(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. \n\t(i) European Aviation Safety Agency (EASA) AD 2018-0006, dated January 10, 2018. \n\t(ii) (Reserved) \n\t(3) For EASA AD 2018-0006, contact the EASA, Konrad-Adenauer- Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find this EASA AD on the EASA website at https://ad.easa.europa.eu. \n\t(4) You may view this service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222-5110. This material may be found in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0383. \n\t(5) You may view this material that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, email fr.inspection@nara.gov, or go to https://www.archives.gov/federal-register/cfr/ibr-locations.html. \n\n\n\tIssued on July 26, 2021. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. (FR Doc. 2021-19249 Filed 9-7-21; 8:45 am) BILLING CODE 4910-13-P

Background \n\n\n\tEASA, which is the Technical Agent for the Member States of the European Union, has issued a series of ADs, the most recent being EASA AD 2018-0006, dated January 10, 2018 (EASA AD 2018-0006), to correct an unsafe condition for Leonardo S.p.A. Helicopters (formerly Finmeccanica S.p.A., AgustaWestland S.p.A.) Model AW189 helicopters with certain part-numbered and serial-numbered Aero Sekur EFS float assemblies installed, except those float assemblies marked with SB-189-25-004. EASA initially issued EASA AD 2017-0256, dated December 22, 2017 (EASA AD 2017-0256), to address the unsafe condition. EASA issued EASA AD 2018-0006 to supersede EASA AD 2017-0256 to revise the compliance time based on the EFS float assembly condition. \n\tThe FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Leonardo S.p.a. Model AW189 helicopters. The NPRM published in the Federal Register on May 28, 2021 (86 FR 28714). The NPRM was prompted by corrosion on the inlet check valve banjo fitting of EFS float assemblies. The NPRM proposed to require visually inspecting each banjo fitting installed on an affected EFS float assembly, and depending on the results, removing the banjo fitting from service. The NPRM also proposed to require applying corrosion inhibiting compound to each banjo fitting installed on an affected EFS float assembly and prohibit installing an affected EFS float assembly unless the banjo fitting inspection, banjo fitting replacement, and corrosion inhibiting compound application requirements have been accomplished, as specified in an EASA AD. \n\tThe FAA is issuing this AD to prevent reduced inflation of an EFS float. The unsafe condition, if not addressed, could affect the helicopter's buoyancy during an emergency landing on water. See EASA AD 2018-0006 for additional background information. \n\nDiscussion of Final Airworthiness Directive \n\nComments \n\n\n\tTheFAA 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. \n\nConclusion \n\n\n\tThe FAA reviewed the relevant data and determined that air safety and the public interest require adopting this final rule as proposed. \n\nRelated Service Information Under 1 CFR Part 51 \n\n\n\tEASA AD 2018-0006 requires visually inspecting the banjo fittings installed on an affected EFS float assembly. If there is corrosion on a banjo fitting, EASA AD 2018-0006 requires replacing the banjo fitting. EASA AD 2018-0006 also requires applying corrosion inhibiting compound to each banjo fitting installed on an affected EFS float assembly. EASA AD 2018-0006 prohibits installing an affected EFS float assembly unless the banjo fitting inspection, banjo fitting replacement, and corrosion inhibiting compound application requirements have been accomplished. EASA AD 2018-0006 also allows credit for actions accomplished previously with a prior revision of the Leonardo Helicopters service information. \n\tThis material 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\nOther Related Service Information \n\n\n\tThe FAA reviewed Leonardo Helicopters Alert Service Bulletin No. 189-174, original issue, dated December 22, 2017 (ASB 189-174 original issue), and Revision A, dated January 5, 2018 (ASB 189-174 Rev A). The FAA also \n\n((Page 50236)) \n\nreviewed Aero Sekur Service Bulletin SB-189-25-004, original issue, dated November 22, 2017 (SB-189-25-004), which is attached as Annex A to ASB 189-174 original issue and ASB 189-174 Rev A. \n\tASB 189-174 Rev A and ASB 189-174 original issue specify the same procedures, except the compliance time specified by ASB 189-174 Rev A has been revised by adding affected EFS float assemblies that have been inspected using procedures in the maintenance manual within the previous 12 months. ASB 189-174 original issue and ASB 189-174 Rev A specify accomplishing the Visual Inspection and Corrosion Prevention, and Record Instruction procedures specified in SB-189-25-004. ASB 189- 174 original issue and ASB 189-174 Rev A also specify emailing photographical evidence of each corroded banjo fitting to Leonardo Helicopters PSE Division and returning replaced banjo fittings to Leonardo Helicopters Customer Support Division. \n\tSB-189-25-004 specifies procedures for cleaning and visually inspecting each banjo fitting for evidence of corrosion. If there is corrosion, SB-189-25-004 specifies procedures for discarding the banjo fitting and its O-rings, and installing a new banjo fitting. SB-189-25- 004 also specifies procedures for applying corrosion inhibiting compound (JC5A or Mastinox 6856) on all banjo fittings. When SB-189-25- 004 is accomplished, SB-189-25-004 specifies procedures for marking the identification label of the EFS float assembly. \n\nDifferences Between This AD and the EASA AD \n\n\n\tEASA AD 2018-0006 requires returning and discarding certain parts, whereas this AD requires removing those parts from service instead. \n\nCosts of Compliance \n\n\n\tThe FAA estimates that this AD affects 4 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\tInspecting the banjo fittings takes about 8.5 work-hours for an estimated cost of $723 per helicopter and $2,892 for the U.S. fleet. Applying corrosion inhibiting compound takes about 1.5 work-hours for an estimated cost of $128 per helicopter and $512 for the U.S. fleet. If required, replacing a banjo fitting takes a minimal additional amount of time after inspecting it and parts cost about $550 for an estimated cost of $550 per helicopter. \n\nAuthority for This Rulemaking \n\n\n\tTitle 49 of the United States Code specifies the FAA's authorityto 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 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. \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.