AD 2017-09-05

We are adopting a new airworthiness directive (AD) for Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, and EC225LP helicopters. This AD requires repetitively checking screws in the emergency flotation gear. This AD is prompted by a report that a screw ruptured on a Model AS332 helicopter's emergency flotation gear. These actions are intended to correct an unsafe condition on these products.

Final rule; request for comments.

Adoption of 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 (AD): \n\n2017-09-05 Airbus Helicopters: Amendment 39-18867; Docket No. FAA- 2016-6651; Directorate Identifier 2016-SW-015-AD. \n\n(a) Applicability \n\n\n\tThis AD applies to Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, and EC225LP helicopters with emergency flotation gear installed, certificated in any category. \n\n(b) Unsafe Condition \n\n\n\tThis AD defines the unsafe condition as failure of a rear upper screw fitting on the emergency flotation gear. This condition, if not detected and corrected, could result in failure of the emergency flotation system and subsequent capsizing of the helicopter. \n\n(c) Effective Date \n\n\n\tThis AD becomes effective May 26, 2017. \n\n(d) Compliance \n\n\n\tYou are responsible for performing each action required by this AD within the specified compliance time unless it has already been accomplished prior to that time. \n\n(e) Required Actions \n\n\n\tWithin 15 hours time-in-service, and before each flight over water thereafter: \n\n((Page 21915)) \n\n\n\t(1) Visually check each emergency flotation gear left hand and right hand rear upper fitting to determine whether the heads of the lower screws are present. Figure 1 to paragraph (e)(1) of this AD depicts where the lower three screws (noted as B and E) are located. Check each screw for looseness by determining whether it can be rotated by hand. The actions required by paragraph (e)(1) of this AD may be performed by the owner/operator (pilot) holding at least a private pilot certificate and must be entered into the aircraft records showingcompliance with this AD in accordance with Title 14 Code of Federal Regulations (14CFR) Sec. Sec. 43.9(a)(1)-(4) and 14 CFR 91.417(a)(2)(v). The record must be maintained as required by 14 CFR 91.417, 121.380, or 135.439. \n\tBILLING CODE 4910-13-P (GRAPHIC) (TIFF OMITTED) TR11MY17.000 \n\nBILLING CODE 4910-13-C \n\n((Page 21916)) \n\n\n\t(2) If a screw head is missing or if a screw is loose, before further flight over water, replace all screws in the fitting. Replacing the screws is not a terminating action for the repetitive checks required by this AD. \n\n(f) Special Flight Permits \n\n\n\tSpecial flight permits are prohibited for flight over water. \n\n(g) Alternative Methods of Compliance (AMOCs) \n\n\n\t(1) The Manager, Safety Management Group, FAA, may approve AMOCs for this AD. Send your proposal to: Matt Fuller, Senior Aviation Safety Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5110; email 9-ASW-FTW-AMOC-Requests@faa.gov. \n\t(2) For operations conducted under a 14 CFR part 119 operating certificate or under 14 CFR part 91, subpart K, we suggest that you 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. \n\n(h) Additional Information \n\n\n\t(1) Airbus Helicopters Emergency Alert Service Bulletin No. 05.01.06, and Airbus Helicopters Emergency Alert Service Bulletin No. 05A047, both Revision 0, and both dated December 18, 2015, which are not incorporated by reference, contain additional information about the subject of this AD. For service information identified in this AD, 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 http://www.airbushelicopters.com/techpub. You may review a copy of the service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. \n\t(2) The subject of this AD is addressed in European Aviation Safety Agency (EASA) Emergency AD No. 2015-0239-E, dated December 18, 2015. You may view the EASA AD on the Internet at http://www.regulations.gov by searching for and locating it in Docket No. FAA-2016-6651. \n\n(i) Subject \n\n\n\tJoint Aircraft Service Component (JASC) Code: 3212, Emergency Flotation Section.

Comments Invited \n\n\n\tThis AD is a final rule that involves requirements affecting flight safety, and we did not provide you with notice and an opportunity to provide your comments prior to it becoming effective. However, we invite you to participate in this rulemaking by submitting written comments, data, or views. We also invite comments relating to the economic, environmental, energy, or federalism impacts that resulted from adopting this AD. The most helpful comments reference a specific portion of the AD, explain the reason for any recommended change, and include supporting data. To ensure the docket does not contain duplicate comments, commenters should send only one copy of written comments, or if comments are filed electronically, commenters should submit them only one time. We will file in the docket all comments that we receive, as well as a report summarizing each substantive public contact with FAA personnel concerning this rulemaking duringthe comment period. We will consider all the comments we receive and may conduct additional rulemaking based on those comments. \n\nDiscussion \n\n\n\tEASA, which is the Technical Agent for the Member States of the European Union, has issued EASA Emergency AD No. 2015-0239-E, dated December 18, 2015, to correct an unsafe condition for Airbus Helicopters Model AS 332 C, AS 332 C1, AS 332 L, AS 332 L1, AS 332 L2, and EC 225 LP helicopters with emergency flotation gear. EASA advises that a screw ruptured on the rear upper fitting on the left-hand (LH) emergency flotation gear of an AS332 helicopter. EASA states that this condition, if not detected and corrected, could result in the failure of an emergency flotation system when ditching and unstable floating of the helicopter, possibly resulting in injury to the occupants. EASA consequently requires repetitive inspections of the lower attachment screws of rear upper fitting on the rear LH and right-hand (RH) emergency flotation gears. According to EASA, the root cause of the failure has not yet been identified. \n\nFAA's Determination \n\n\n\tThese helicopters have been approved by the aviation authority of France and are approved for operation in the United States. Pursuant to our bilateral agreement with France, EASA, its technical representative, has notified us of the unsafe condition described in the EASA AD. We are issuing this AD because we evaluated all information provided by EASA and determined the unsafe condition exists and is likely to exist or develop on other helicopters of these same type designs. \n\nRelated Service Information \n\n\n\tWe have reviewed Airbus Helicopters Emergency Alert Service Bulletin (EASB) No. 05.01.06, Revision 0, dated December 18, 2015, for Model AS332C, AS332C1, AS332L, AS332L1, and AS332L2 helicopters and for military Model AS332B, AS332B1, AS332F1, AS332M, and AS332M1 helicopters, and EASB No. 05A047, Revision 0, dated December 18, 2015, for Model EC225LP helicopters. This service information specifies repetitively \n\n((Page 21914)) \n\ninspecting the lower screws of the rear upper fitting on the rear LH and RH emergency floating gears for the presence of the heads and stressing the screw heads using a tool to make sure that the screw head does not move. If all screw heads are present, the service information requires no further action. If at least one screw head is missing or moves, the service information specifies replacing the two lower screws and the upper screw and informing Airbus Helicopters. \n\nAD Requirements \n\n\n\tThis AD requires, within 15 hours time-in-service (TIS) and thereafter before each flight over water, visually checking the rear upper fittings of the LH and RH emergency flotation gears for the presence of screw heads and looseness. An owner/operator (pilot) may perform the required visual check and must enter compliance with the applicable paragraph of the AD into the helicopter maintenance records in accordance with 14 CFR 43.9(a)(1) through (4) and 91.417(a)(2)(v). A pilot may perform this check because it involves visually checking the rear upper fittings of the LH and RH emergency flotation gears for the presence of screw heads and twisting the screws by hand, which can be performed equally well by a pilot or a mechanic. This check is an exception to our standard maintenance regulations. If any screw heads are missing, loose, or twist off with hand pressure, this AD requires replacing all screws in the fitting before the next flight over water. \n\nDifferences Between This AD and the EASA AD \n\n\n\tThe EASA AD allows using tools for the inspection, while this AD requires checking by hand. The EASA AD requires that repetitive inspections occur at intervals not to exceed 15 hours TIS, while this AD requires the repetitive checks before each flight over water. The EASA AD requires contacting Airbus Helicopters if a screw is missing or loose, while this AD does not. \n\nInterim Action \n\n\n\tWe consider this AD interim action. The design approval holder is currently investigating the root cause for this unsafe condition and may develop a modification that will address this unsafe condition. If this modification is developed, approved and available, we might consider additional rulemaking. \n\nCosts of Compliance \n\n\n\tWe estimate that this AD affects 24 helicopters of U.S. Registry and that labor costs average $85 per work-hour. Based on these estimates, we expect the following costs: \n\tChecking the screws requires about 1/10 of a work-hour and no parts are needed, for a cost of $9 per helicopter and $216 for the U.S. fleet. \n\tReplacing the screws requires 8 work-hours for a labor cost of $680. Parts cost $150 for a total cost of $830 per helicopter. \n\nFAA's Justification and Determination of the Effective Date \n\n\n\tProviding an opportunity for public comments prior to adopting these AD requirements would delay implementing the safety actions needed to correct this known unsafe condition. Therefore, we find that the risk to the flying public justifies waiving notice and comment prior to the adoption of this rule because the required corrective actions must be accomplished within 15 hours TIS. \n\tSince an unsafe condition exists that requires the immediate adoption of this AD, we determined that notice and opportunity for public comment before issuing this AD are impracticable and that good cause exists for making this amendment effective in less than 30 days. \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\tWe are 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 promotingsafe 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\tWe 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. \n\tFor the reasons discussed, I certify that this AD: \n\t1. Is not a ''significant regulatory action'' under Executive Order 12866; \n\t2. Is not a ''significant rule'' under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); \n\t3. Will not affect intrastate aviation in Alaska to the extent that it justifies making a regulatory distinction; and \n\t4. 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\tWe prepared an economic evaluation of the estimated costs to comply with this AD and placed it in the AD docket. \n\nList of Subjects in 14 CFR Part 39 \n\n\n\tAir transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.