Safety Publications Tool

2023-0136R1 : Pneumatic – Overheat Detection System Sensing Elements – Inspection

Number 2023-0136R1
Issued by Europe  Europe
Issue date 2024-04-22
Effective date 2024-04-29
EASA approval number
ATA Chapter 36
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A330
      • A330-201
      • A330-202
      • A330-203
      • A330-223
      • A330-223F
      • A330-243
      • A330-243F
      • A330-301
      • A330-302
      • A330-303
      • A330-321
      • A330-322
      • A330-323
      • A330-341
      • A330-342
      • A330-343
      • A330-743L (BelugaXL)
    • A340
      • A340-211
      • A340-212
      • A340-213
      • A340-311
      • A340-312
      • A340-313
Revision This AD revises EASA AD 2023-0136 dated 12 July 2023.
Correction Not applicable
Supersedure This AD superseded EASA AD 2022-0243 dated 08 December 2022.
Publication(s) and related information Airbus SB A330-36-3052 original issue dated 27 June 2022, and Revision 01 dated 29 May 2023. Airbus SB A340-36-4036 original issue dated 27 June 2022. Kidde Aerospace & Defense SB CFD-26-3 original issue dated 13 January 2022, or Revision 1 dated 29 March 2022. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
Remarks 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 after publication. 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.