Safety Publications Tool

2025-0080 : [Correction] Fire Protection – Aft Cargo Compartment Fire Extinguisher Distribution Piping – Functional Check

Number 2025-0080
Issued by Europe  Europe
Issue date 2025-04-23
Effective date 2025-04-25
EASA approval number
ATA Chapter 26
Approval Holder
/ Type Designation
  • ATR
    • ATR42
      • 300
      • 320
      • 400
      • 500
    • ATR72
      • 102
      • 201
      • 202
      • 211
      • 212
      • 212A
Revision Not applicable
Correction This AD is republished to include the reference to issue 4 of the AOM in paragraph (4) of this AD, which was erroneously omitted in the original publication.
Supersedure This AD supersedes EASA AD 2025-0024 dated 22 January 2025.
Publication(s) and related information ATR AOM: 2024/13 issue 1 dated 25 November 2024, or issue 2 dated 21 January 2025, or issue 3 dated 28 January 2025, issue 4 dated 26 February 2025, or issue 5 dated 10 April 2025. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
Remarks 15 May 2025: The Comment Response Document has been published and notified. No changes have been made to the AD in response to the comments received. 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until 09 May 2025. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed ('zipped') file, attached to the record for this AD. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.