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  Safety Publications Tool

2021-0281R2 : Aircraft Flight Manual / Engine Bleed Air System – Amendment / Pneumatic – Engine Bleed Air System – Maintenance Tasks

Number 2021-0281R2
Issued by Europe  Europe
Issue date 2025-01-13
Effective date 2025-01-27
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)
Revision This AD revises EASA AD 2021-0281R1 dated 03 August 2023.
Correction Not applicable
Supersedure The original issue of this AD superseded EASA AD 2020-0205 dated 24 September 2020.
Publication(s) and related information Airbus A330 AFM TR 803 issue 1.0, approved by EASA on 15 July 2020. Airbus A330 AFM TR 804 issue 1.0, approved by EASA on 15 July 2020. Airbus A330 AFM TR 805 issue 1.0, approved by EASA on 04 September 2020. Airbus AOT A36L004-20 Revision 01 dated 27 October 2021. Airbus SB A330-31-3279 original issue dated 02 December 2020. Airbus SB 330-31-3028 original issue dated 25 May 1999, or Revision 1 dated 21 February 2000. Airbus SB A330-31-3266 original issue dated 19 December 2019. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 21-168
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The original issue of this AD was posted on 10 November 2021 as PAD 21-168 for consultation until 08 December 2021. 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.