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2025-17-03: Emergency Equipment

FAA order 2025-17-03 is an airworthiness directive in force since September 8, 2025. The FAA's subject line: Emergency Equipment. It names Airbus Helicopters AS332, Airbus Helicopters EC 225: about 32 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Airbus Helicopters
Models
AS332L, AS332L1, AS332L2, EC225LP
On this site
Airbus Helicopters AS332 8 registered
Airbus Helicopters EC 225 24 registered

Dates and paperwork

In force since
September 8, 2025
Published
August 22, 2025 (signed August 14, 2025)
Docket
FAA-2025-1737
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 AS332L, AS 332L1, AS 332L2, and EC 225LP helicopters. This AD was prompted by a report of a corroded emergency sea anchor pin. This AD requires inspecting the emergency sea anchor and, depending on the result, replacing the emergency sea anchor. 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 (4,671 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: 2025-17-03 Airbus Helicopters: Amendment 39-23113; Docket No. FAA-2025-1737; Project Identifier MCAI-2025-01210-R. (a) Effective Date This airworthiness directive (AD) is effective September 8, 2025. (b) Affected ADs None. (c) Applicability This AD applies to Airbus Helicopters Model AS332L, AS 332L1, AS 332L2, and EC 225LP helicopters, certificated in any category. (d) Subject Joint Aircraft System Component (JASC) Code 2560, Emergency Equipment. (e) Unsafe Condition This AD was prompted by a report of a corroded emergency sea anchor pin (anchor pin). The FAA is issuing this AD to detect and correct corrosion on the anchor pin. The unsafe condition, if not addressed, could lead to failure of the anchor pin and release the emergency sea anchor in flight, which could result in damage to the rotors 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 Emergency AD 2025-0146-E, dated July 10, 2025 (EASA AD 2025-0146-E). (h) Exceptions to EASA AD 2025-0146-E (1) Where EASA AD 2025-0146-E refers to its effective date, this AD requires using the effective date of this AD. (2) Where EASA AD 2025-0146-E refers to flight hours, this AD requires using hours time-in-service. (3) Where paragraph (2) of EASA AD 2025-0146-E specifies "any discrepancy as defined in the EASB is detected", this AD requires replacing that text with "any anchor pin that has corrosion, a crack, or a diameter that is less than or equal to 8.0 mm (.315 in) is detected". (4) This AD does not adopt paragraph (3) of EASA AD 2025-0146-E. (5) This AD does not adopt the "Remarks" section of EASA AD 2025-0146-E. (i) No Reporting Requirement Although the material referenced in EASA AD 2025-0146-E specifies to submit certain information to the manufacturer, this AD does not require that action. (j) Special Flight Permit Special flight permits are prohibited. (k) 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 (l) 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. (l) Additional Information For more information about this AD, contact David Enns, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (316) 946-4147; email: [email protected]. (m) 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) Emergency AD 2025-0146-E, dated July 10, 2025. (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 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 [email protected] . Issued on August 14, 2025. Steven W. Thompson, Acting Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2025-16082 Filed 8-20-25; 11:15 am]BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2008-07-01SW-08-30R2 · Inadvertent Deployment of Crash Position Indicator (CPI) Beacon
2008-06-30SW-08-30R1 · Inadvertent Deployment of Crash Position Indicator (CPI) Beacon

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/2025-17-03.json · aircraft systems.