Safety Publications Tool

PAD 26-002 : Equipment/Furnishings – Evacuation Slide/Inflation Hose Assemblies – Replacement

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Number 26-002
Issued by Europe  Europe
Issue date 2026-01-08
EASA approval number
ATA Chapter 25
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 Ref. Publications: Airbus SB A320-25-1CML original issue dated 17 October 2025. Airbus SB A320-25-1CMM original issue dated 17 October 2025. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. Safran Aerosystems Evacuation VSB A320 004-25-130 original issue dated 22 February 2024 or revision 01 dated 01 August 2025.
Remarks Remarks: 1. This Proposed AD will be closed for consultation on 05 February 2026. 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. 4. For any question concerning the technical content of the requirements in this PAD, please contact: AIRBUS � Airworthiness Office � 1IASA; E-mail: account.airworth-eas[at]airbus.com.

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