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  Safety Publications Tool

2021-0075 : Fuselage – Splice of Frame X5295 – Inspection / Repair / Modification

Number 2021-0075
Issued by Europe  Europe
Issue date 2021-03-16
Effective date 2021-03-30
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • AIRBUS HELICOPTERS
    • SA 330 / AS 332 / EC 225
      • AS 332 L2
      • EC 225 LP
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA Emergency AD 2014-0098-E dated 25 April 2014.
Publication(s) and related information EC AS332 SB 53.01.52 original issue dated 29 September 2006, or Revision 1 dated 02 March 2007, or Revision 2 dated 21 April 2008, or Revision 3 dated 05 December 2008, or Revision 4 dated 22 February 2010, or Revision 5 dated 23 July 2010. EC EC225 SB 53-003 original issue dated 12 October 2006, or Revision 1 dated 02 March 2007, or Revision 2 dated 05 December 2008, or Revision 3 dated 22 February 2010, or revision 4 dated 23 July 2010. AH AS332 SB 05.00.84 original issue dated 23 February 2010, or Revision 1 dated 15 July 2010, or Revision 2 dated 28 September 2011, or Revision 3 dated 19 July 2012, or Revision 4 dated 22 September 2014. AH EC225 SB 05-019 original issue dated 23 February 2010, or Revision 1 dated 15 July 2010, or Revision 2 dated 28 September 2011, or Revision 3 dated 19 July 2012, or Revision 4 dated 22 September 2014. AH ASB AS332-05.00.97 original issue dated 15 April 2014, or Revision 1 dated 09 February 2021. AH ASB EC225-05A038 original issue dated 15 April 2014, or Revision 1 dated 09 February 2021. AH SB AS332-53.01.97 original issue dated 09 February 2021. AH SB EC225-53-061 original issue dated 09 February 2021. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 21-019
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 11 February 2021 as PAD 21-019 for consultation until 11 March 2021. No comments were received during the consultation period. 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.