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2026-20-08: Tail rotor drive system

FAA order 2026-20-08 is an airworthiness directive in force since November 5, 2026. The FAA's subject line: Tail rotor drive system. It names Aerospatiale AS-355, Airbus Helicopters AS355 TwinStar: about 29 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: rotorcraft systems.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Airbus Helicopters
Models
AS355E, AS355F, AS355F1, AS355F2, AS355N
On this site
Aerospatiale AS-355 23 registered
Airbus Helicopters AS355 TwinStar 6 registered

Dates and paperwork

In force since
November 5, 2026
Published
October 1, 2026 (signed September 24, 2026)
Docket
FAA-2026-4657
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model AS355E, AS355F, AS355F1, AS355F2, and AS355N helicopters. This AD was prompted by the determination that the tail rotor drive fan wheels (fan wheels) and the impeller second stage have been incorrectly identified during production. This AD requires verifying the serial number and amendment of the log cards of the affected parts, and depending on the findings, performing a one-time borescope inspection to verify consistency between the log cards and the affected parts. Depending on the results of the inspection, this AD requires replacing or re-identifying certain parts. This AD also prohibits the installation of certain fan wheels and impeller second stages on any helicopter. The FAA is issuing this AD to address the unsafe conditions on these products.

The order itself the regulatory text, as published

Show the full text (4,831 characters)
1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. 2. The FAA amends § 39.13 by adding the following new airworthiness directive: 2026-20-08 Airbus Helicopters: Amendment 39-23481; Docket No. FAA-2026-4657; Project Identifier MCAI-2024-00383-R. (a) Effective Date This airworthiness directive (AD) is effective November 5, 2026. (b) Affected ADs None. (c) Applicability This AD applies to all Airbus Helicopters Model AS355E, AS355F, AS355F1, AS355F2, and AS355N helicopters, certificated in any category. (d) Subject Joint Aircraft System Component (JASC) Code: 6500, Tail rotor drive system. (e) Unsafe Condition This AD was prompted by the determination that the tail rotor drive fan wheel and impeller second stage have been incorrectly identified during production. The FAA is issuing this AD to detect and address incorrect identification of the affected parts. The unsafe condition, if not addressed, may cause the loss of traceability of the affected parts, which could lead to undetected fatigue failure of the affected parts and result in loss of control of the helicopter. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Requirements Except as specified in paragraphs (h) and (i) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency AD 2024-0127, dated July 3, 2024 (EASA AD 2024-0127). (h) Exceptions to EASA AD 2024-0127 (1) Where EASA AD 2024-0127 refers to its effective date, this AD requires using the effective date of this AD. (2) Where EASA AD 2024-0127 requires compliance in terms of flight hours, this AD requires using hours time-in-service. (3) Where EASA AD 2024-0127 defines "affected part", this AD requires replacing that text with "tail rotor drive fan wheel having part number (P/N) 704A33691014 amdt [amendment] C and impeller second stage P/N 704A33691015 amdt [amendment] C, and a serial number (S/N), as identified in the Log Card, listed as 'S/N affected' in section 4.5 or 4.6 of the accomplishment procedure of Airbus Helicopters Alert Service Bulletin ASB AS355-65-00-0001, Issue 001 dated May 27, 2024". (4) This AD does not adopt the "Remarks" section of EASA AD 2024-0127. (i) No Reporting Requirement Although the material referenced in EASA AD 2024-0127 specifies to submit certain information to the manufacturer, this AD does not require that action. (j) 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 (k) of this AD and email 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. (k) Additional Information For more information about this AD, contact Andrew Gronau, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (847) 294-7378; email: andrew.s.gronau@faa.gov. (l) 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 2024-0127, dated July 3, 2024. (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, 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. (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. Issued on September 24, 2026. Steven W. Thompson, Acting Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2026-20098 Filed 9-30-26; 8:45 am]BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2014-11-25SW-15-04 · Cabin Ventilation Air Scoop Draining
2011-05-16SW-11-33 · Eurocopter France Model AS 355 Helicopters; Main Gearbox Cowling Lock Improvement
2010-12-20SW-11-07 · Star Flex Arm Failures on Eurocopter France Model AS350, AS355, and EC130 Helicopters
2007-04-03SW-07-22R1 · Serrated lock washers
2004-12-02SW-05-20 ·

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 5, 2026. Connections as data: /graph/directive/2026-20-08.json · aircraft systems.