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FAA orders · airworthiness directive · current

2025-23-04: Fire Protection

FAA order 2025-23-04 is an airworthiness directive in force since January 13, 2026. The FAA's subject line: Fire Protection. It names Aerospatiale/Aeritalia ATR 42, Aerospatiale ATR 72, Atr-Gie Avions De Trnsp Region ATR42, Atr-Gie Avions De Trnsp Rgnl ATR 72: about 45 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
ATR – GIE Avions de Transport Régional
Models
ATR42-300, ATR42-320, ATR42-500, ATR72-102, ATR72-201, ATR72-202, ATR72-211, ATR72-212, ATR72-212A
On this site
Aerospatiale/Aeritalia ATR 42 16 registered
Aerospatiale ATR 72 9 registered
Atr-Gie Avions De Trnsp Region ATR42 6 registered
Atr-Gie Avions De Trnsp Rgnl ATR 72 14 registered

Dates and paperwork

In force since
January 13, 2026
Published
December 9, 2025 (signed November 7, 2025)
Docket
FAA-2025-2262
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 certain ATR--GIE Avions de Transport R[eacute]gional Model ATR42-300, - 320, -500, ATR72-201, and -212A airplanes and all ATR--GIE Avions de Transport R[eacute]gional Model ATR72-102, -202, -211, and -212 airplanes. This AD was prompted by an inspection on the ATR final assembly line that found a fire extinguishing tube, located on the ceiling of the aft cargo compartment, disconnected from its sleeve. This AD requires a functional check of the aft cargo fire extinguishing system and applicable on-condition actions, if necessary. For certain airplanes, this AD also requires an additional functional check and applicable on-condition actions. 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 (5,148 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: 2025-23-04 ATR-GIE Avions de Transport Régional: Amendment 39-23187; Docket No. FAA-2025-2262; Project Identifier MCAI-2025-00083-T. (a) Effective Date This airworthiness directive (AD) is effective January 13, 2026. (b) Affected ADs None. (c) Applicability This AD applies to the ATR-GIE Avions de Transport Régional airplanes identified in paragraphs (c)(1) and (2) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2025-0080, dated April 11, 2025; corrected April 23, 2025 (EASA AD 2025-0080). (1) ATR42-300, -320, and -500 airplanes. (2) ATR72-102, -201, -202, -211, -212, and -212A airplanes. (d) Subject Air Transport Association (ATA) of America Code 26, Fire Protection. (e) Unsafe Condition This AD was prompted by an inspection on the ATR final assembly line that found a fire extinguishing tube, located on the ceiling of the aft cargo compartment, disconnected from its sleeve. The FAA is issuing this AD to address this condition, which if not detected and corrected, could affect the capability of the aft cargo compartment fire extinguishing system to contain a cargo compartment fire. (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 2025-0080. (h) Exceptions to EASA AD 2025-0080 (1) Where EASA AD 2025-0080 refers to its effective date, this AD requires using the effective date of this AD. (2) Where EASA AD 2025-0080 refers to February 5, 2025 (the effective date of EASA AD 2025-0024, dated January 22, 2025), this AD requires using the effective date of this AD. (3) Where EASA AD 2025-0080 refers to "any discrepancy", this AD requires replacing that text with "any incorrectly installed distribution piping". (4) This AD does not adopt the "Remarks" section of EASA AD 2025-0080. (i) Special Flight Permits Special flight permits may be issued in accordance with 14 CFR 21.197 and 21.199 to operate the airplane to a location where the airplane can be modified, provided no cargo is in the aft cargo compartment. (j) Additional AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): 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 responsible Flight Standards 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: [email protected] . Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (2) Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions must be accomplished using a method approved by the Manager, International Validation Branch, FAA; or EASA; or ATR-GIE Avions de Transport Régional's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (k) Additional Information For more information about this AD, contact Alexis Whitaker, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 516-228-7309; email: [email protected]. (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 this AD specifies otherwise. (i) European Union Aviation Safety Agency (EASA) AD 2025-0080, dated April 11, 2025; corrected April 23, 2025. (ii) [Reserved] (3) For EASA material identified in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email [email protected]. You may find this 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, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (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 November 7, 2025. Steven W. Thompson, Acting Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2025-22346 Filed 12-8-25; 8:45 am]BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2015-04-20NM-15-14 · Propellers/Propulsors
2011-08-01NM-11-45 · Doors: Cargo/Baggage Doors
2011-02-03NM-11-19 · Indicating/Recording System Angle of Attack Sensors
2010-03-04NM-10-18 · Instruments: Redesigned Aileron Sensors for Flight Data Recorder
2010-01-07NM-10-13 · Navigation: Flight Management 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 October 26, 2026. Connections as data: /graph/directive/2025-23-04.json · aircraft systems.