90 FR 104 pgs. 23267-23269 - Airworthiness Directives; Airbus Helicopters
Type: RULEVolume: 90Number: 104Pages: 23267 - 23269
Pages: 23267, 23268, 23269Docket number: [Docket No. FAA-2025-0006; Project Identifier MCAI-2023-00803-R; Amendment 39-23034; AD 2025-09-13]
FR document: [FR Doc. 2025-09889 Filed 5-30-25; 8:45 am]
Agency: Transportation Department
Sub Agency: Federal Aviation Administration
Official PDF Version: PDF Version
[top]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2025-0006; Project Identifier MCAI-2023-00803-R; Amendment 39-23034; AD 2025-09-13]
RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters
AGENCY:
Federal Aviation Administration (FAA), DOT.
ACTION:
Final rule.
SUMMARY:
The FAA is adopting a new airworthiness directive (AD) for Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters. This AD was prompted by a report of a sliding door that was locked in the open position detaching from the helicopter during flight. This AD requires modifying certain upper rail rollers, installing a label on each sliding door, and prohibits installing affected upper rail rollers or a door having an affected upper rail roller. These actions are specified in a 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.
DATES:
This AD is effective July 7, 2025.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of July 7, 2025.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under Docket No.FAA-2025-0006; 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 EASA material identified in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 000; email: ADs@easa.europa.eu; 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, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Parkway, Room 6N-321, 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-2025-0006.
FOR FURTHER INFORMATION CONTACT:
Adam Hein, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (316) 946-4116; email: Adam.Hein@faa.gov.
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 Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters. The NPRM was published in the Federal Register on January 17, 2025 (90 FR 5759). The NPRM was prompted by EASA AD 2023-0131, dated July 3, 2023 (EASA AD 2023-0131) (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 a left-hand (LH) sliding door of a Model AS 350 B3 helicopter was lost while flying with the door locked in the open position. Design review by Airbus determined that the upper rail roller had a single locking device instead of two separate locking devices, which is required for that type of fastener.
In the NPRM, the FAA proposed to require modifying certain upper rail rollers, installing a label on each sliding door, and prohibit installing affected upper rail rollers or a door having an affected upper rail roller. The FAA is issuing this AD to address the insufficient upper rail roller locking mechanism of the sliding door. The unsafe condition, if not addressed, could lead to the sliding door detaching from the helicopter during flight, and subsequent damage to the helicopter and injury to persons on the ground.
You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA-2025-0006.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of the costs.
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 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 2023-0131, which requires modifying affected upper rail rollers and installing a label on each sliding door. EASA AD 2023-0131 also prohibits installing an affected upper rail roller, or a door having an affected upper rail roller installed, on any helicopter. 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
[top] EASA AD 2023-0131 applies to Model AS350BB helicopters, whereas this AD does not because that model is not FAA-type certificated.
Costs of Compliance
The FAA estimates that this AD affects 972 helicopters of U.S. registry. Labor rates are estimated at $85 per work-hour. Based on these numbers, the FAA estimates that operators may incur the following costs in order to comply with this AD.
Modifying the upper rail rollers and installing a label on the sliding doors (up to two doors per helicopter) takes up to 8 work-hours and parts cost $2,668 for an estimated cost of up to $3,348 per helicopter and $3,254,256 for the U.S. fleet.
The 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.
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.
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.
§?39.13 [Amended]
2. The FAA amends §?39.13 by adding the following new airworthiness directive:
2025-09-13 Airbus Helicopters: Amendment 39-23034; Docket No. FAA-2025-0006; Project Identifier MCAI-2023-00803-R.
(a) Effective Date
This airworthiness directive (AD) is effective July 7, 2025.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters, certificated in any category, as identified in European Union Aviation Safety Agency AD 2023-0131, dated July 3, 2023 (EASA AD 2023-0131).
(d) Subject
Joint Aircraft System Component (JASC): Code 5200, Doors.
(e) Unsafe Condition
This AD was prompted by a report of a sliding door that was locked in the open position detaching from the helicopter during flight. The FAA is issuing this AD to address the insufficient upper rail roller locking mechanism of the sliding door. The unsafe condition, if not addressed, could lead to the sliding door detaching from the helicopter during flight, and subsequent damage to the helicopter and injury to persons on the ground.
(f) Compliance
Comply with this AD within the compliance times specified, unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2023-0131.
(h) Exceptions to EASA AD 2023-0131
(1) Where EASA AD 2023-0131 refers to its effective date, this AD requires using the effective date of this AD.
(2) Where EASA AD 2023-0131 requires compliance in terms of flight hours, this AD requires using hours time-in-service.
(3) Where the service information referenced in EASA AD 2023-0131 specifies to discard parts, this AD requires removing those parts from service.
(4) Where the service information referenced in EASA AD 2023-0131 specifies to submit certain information to the manufacturer, this AD does not require that action.
(5) This AD does not adopt the "Remarks" section of EASA AD 2023-0131.
(i) Alternative Methods of Compliance (AMOCs)
(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) of this AD. Information may be emailed to: AMOC@faa.gov.
(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.
(j) Related Information
For more information about this AD, contact Adam Hein, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (316) 946-4116; email: Adam.Hein@faa.gov.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the incorporation by reference of the material listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this material as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2023-0131, dated July 3, 2023.
(ii) [Reserved]
(3) For EASA material identified in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 000; email: ADs@easa.europa.eu; website: easa.europa.eu. You may find the EASA material on the EASA website at ad.easa.europa.eu.
(4) You may view this material at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Parkway, Room 6N-321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222-5110.
(5) You may view this material at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email fr.inspection@nara.gov.
[top]
Steven W. Thompson,
Acting Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service.
[FR Doc. 2025-09889 Filed 5-30-25; 8:45 am]
BILLING CODE 4910-13-P