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PAD 25-140 : Fire Protection – Fire Panel – Inspection

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Number 25-140
Issued by Europe  Europe
Issue date 2025-09-10
EASA approval number
ATA Chapter 26
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A318
      • A318-111
      • A318-112
      • A318-121
      • A318-122
    • A319
      • A319-111
      • A319-112
      • A319-113
      • A319-114
      • A319-115
      • A319-131
      • A319-132
      • A319-133
      • A319-151N
      • A319-153N
      • A319-171N
      • A319-173N
    • A320
      • A320-211
      • A320-212
      • A320-214
      • A320-215
      • A320-216
      • A320-231
      • A320-232
      • A320-233
      • A320-251N
      • A320-252N
      • A320-253N
      • A320-271N
      • A320-272N
      • A320-273N
    • A321
      • A321-111
      • A321-112
      • A321-131
      • A321-211
      • A321-212
      • A321-213
      • A321-231
      • A321-232
      • A321-251N
      • A321-251NX
      • A321-252N
      • A321-252NX
      • A321-253N
      • A321-253NX
      • A321-253NY
      • A321-271N
      • A321-271NX
      • A321-271NY
      • A321-272N
      • A321-272NX
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information AIRBUS SB A320-26-1137 original issue dated 20 June 2025 and revision 1 dated 10 July 2025. AIRBUS SB A320-26-1138 original issue dated 20 June 2025 and revision 1 dated 10 July 2025. SAFRAN SB 330TS08Y-26-001 original issue dated 30 September 2024. SAFRAN SB 335TS08Y-26-006 original issue dated 22 October 2024. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. SAFRAN SIL 306-26-001 at original issue dated 03 December 2024.
Remarks 1. This Proposed AD will be closed for consultation on 24 September 2025. 2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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.

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