Rule
Airworthiness Directives; Airbus Helicopters
The full text was pulled automatically from the official source and is not Threadline News reporting; the annotations alongside it are.
Agency
Federal Aviation Administration (FAA), DOT.
Action
Final rule.
Summary
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, EC130B4, and EC130T2 helicopters. This AD was prompted by reports of an incorrectly installed engine flange on the main gear box (MGB) engine coupling. This AD requires inspecting the MGB engine coupling for correct installation and, depending on the results, corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.
Dates
This AD is effective September 10, 2026. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of September 10, 2026.
Addresses
AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-4638; 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, the mandatory continuing airworthiness information (MCAI), 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. Material Incorporated by Reference: For European Union Aviation Safety Agency (EASA) material identified in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 000; email: [email protected]; website: easa.europa.eu. You may find the EASA material on the EASA website at ad.easa.europa.eu. You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 10101 Hillwood Parkway, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222-5110. It is also available at regulations.gov under Docket No. FAA-2026-4638.
For further information contact
Aryanna Sanchez, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (520) 990-9321; email: [email protected].
Supplementary information
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, EC130B4, and EC130T2 helicopters. The NPRM was published in the Federal Register on May 15, 2026 (91 FR 27873). The NPRM was prompted by EASA AD 2023-0127, dated June 27, 2023 (EASA AD 2023-0127) (also referred to as the MCAI), issued by EASA, which is the Technical Agent for the Member States of the European Union. The MCAI states that on the final assembly line, the engine flange on the MGB engine coupling may have been installed inverted.
In the NPRM, the FAA proposed to require inspecting the MGB engine coupling for correct installation and, depending on the results, corrective actions. The FAA is issuing this AD to detect and correct the inverted installation of the engine flange on the MGB engine coupling. The unsafe condition, if not detected and corrected, could result in the loss of power transmission to the MGB and the main rotor and lead to loss of control of the helicopter. You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA-2026-4638.
Discussion of Final Airworthiness Directive
Comments
The FAA received a comment from one commenter, Papillon Airways (Papillon). The following presents the comment received on the NPRM and the FAA's response to the comment.
Request To Change the Applicability
Papillon requested the FAA revise the applicability of the NPRM, to apply not only to the production date of the helicopters but also that the NPRM apply to helicopters with less than 3,500 total flight hours. Papillon stated the date ranges are too broad and they do not address high usage aircraft. Papillon also stated that aircraft with more than 3,500 flight hours have likely already replaced the engine and gearboxes [MGB] and would therefore no longer be affected by the unsafe condition. The FAA disagrees with revising the applicability of this final rule. The FAA is unable to determine how many helicopters may have replaced the MGBs or engines before 3,500 total hours time-in-service (TIS) or how many helicopters may not have replaced the MGB or engine before exceeding 3,500 total hours TIS. The FAA acknowledges that a majority of the MGBs may have been replaced. Thus, adopting the MCAI applicability ensures that all helicopters that may be affected are included in this final rule. The FAA did not change this AD as a result of this comment.
Conclusion
These products have been approved by the civil aviation authority of another country and are approved for operation in the United States. Pursuant to the FAA's bilateral agreement with this State of Design Authority, that authority has notified the FAA of the unsafe condition described in the MCAI referenced above. The FAA reviewed the relevant data, considered any comments received, 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 products. Except for minor editorial changes, this AD is adopted as proposed in the NPRM. None of the changes will increase the economic burden on any operator.
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed EASA AD 2023-0127, which specifies procedures for a one-time inspection of the MGB engine coupling for correct installation. Depending on the results, EASA AD 2023-0127 specifies installing a correctly assembled engine flange or a new engine flange. EASA AD 2023-0127 also specifies reporting the inspection results to the manufacturer. This 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.
Differences Between This AD and the MCAI
The MCAI applies to Airbus Helicopters Model AS350BB helicopter, whereas this AD does not because that model does not have an FAA type certificate.
Costs of Compliance
The FAA estimates that this AD affects 4,102 helicopters of U.S. registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs
Cost per Cost on U.S. Action Labor cost Parts cost product operators
Inspect MGB engine coupling.............. 1 work-hour x $85 per hour $0 $85 $348,670 = $85.
The FAA estimates the following costs to do any corrective actions that would be required based on the results of the inspection. The agency has no way of determining the number of helicopters that might need this corrective action: