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2025-16-08: Tail Rotor Blades

FAA order 2025-16-08 is an airworthiness directive in force since September 22, 2025. The FAA's subject line: Tail Rotor Blades. It names Airbus Helicopters EC 130 now H130: about 311 aircraft on the U.S. register today, 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
EC130B4, EC130T2
On this site
Airbus Helicopters EC 130 now H130 311 registered

Dates and paperwork

In force since
September 22, 2025
Published
August 18, 2025 (signed August 1, 2025)
Docket
FAA-2024-0765
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 EC 130 B4 and EC 130 T2 helicopters. This AD was prompted by the determination that fatigue cracks may develop at the root section of certain tail rotor blades (TRBs). This AD requires inspecting those TRBs and, depending on the results, replacing the TRB with a serviceable TRB. This AD also prohibits installing those TRBs unless certain actions are accomplished. The FAA is issuing this AD to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (4,656 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: 2025-16-08 Airbus Helicopters: Amendment 39-23106; Docket No. FAA-2024-0765; Project Identifier MCAI-2022-00981-R. (a) Effective Date This airworthiness directive (AD) is effective September 22, 2025. (b) Affected ADs None. (c) Applicability This AD applies to Airbus Helicopters Model EC 130 B4 and EC 130 T2 helicopters, certificated in any category. (d) Subject Joint Aircraft Service Component (JASC) Code: 6410, Tail Rotor Blades. (e) Unsafe Condition This AD was prompted by the determination that fatigue cracks may develop at the root section of a tail rotor blade (TRB). The FAA is issuing this AD to address fatigue cracks on a TRB. The unsafe condition, if not addressed, could result in crack propagation, TRB failure, and consequent 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 2022-0150, dated July 21, 2022 (EASA AD 2022-0150). (h) Exceptions to EASA AD 2022-0150 (1) Where EASA AD 2022-0150 requires compliance in terms of flight hours, this AD requires using hours time-in-service. (2) Where EASA AD 2022-0150 refers to its effective date, this AD requires using the effective date of this AD. (3) This AD does not adopt the "Remarks" section of EASA AD 2022-0150. (i) No Reporting Requirement Although the service information referenced in EASA AD 2022-0150 specifies to submit certain information to the manufacturer, this AD does not include that requirement. (j) Special Flight Permit Special flight permits are prohibited. (k) Optional Terminating Action Revising the Airworthiness Limitations section of your existing helicopter maintenance manual or instructions for continued airworthiness and your existing approved maintenance or inspection program, as applicable, to include the repetitive inspections in paragraph (g) of this AD is terminating action for the repetitive inspections required by this AD. (l) 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 (m) of this AD and email to: [email protected]. (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. (m) Additional Information For more information about this AD, contact C. Jason Franklin, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (817) 222-5291; email: [email protected]. (n) 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 this AD specifies otherwise. (i) European Union Aviation Safety Agency (EASA) AD 2022-0150, dated July 21, 2022. (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: [email protected]; website: easa.europa.eu. You may find this 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 [email protected]. Issued on August 1, 2025. Steven W. Thompson, Acting Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2025-15657 Filed 8-15-25; 8:45 am]BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2019-07-15SW-17-23R2 · Fuel System
2018-03-02SW-17-23R1 · Fuel System
2015-08-13SW-15-20 · Air Conditioning System Wiring
2012-10-03SW-12-45 · Garmin Model 400W/500W Series GPS-WAAS Navigation System
2012-02-03SW-12-17 · Autopilot System

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 November 6, 2026. Connections as data: /graph/directive/2025-16-08.json · aircraft systems.