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CF-2025-27 : Fuselage – Cracks on Aft Wing to Body Fairing Structure

Number CF-2025-27
Issued by Canada  Canada
Issue date 2025-05-22
Effective date 2025-06-04
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • AIRBUS CANADA LP
    • BD-500 (A220 Series)
      • BD-500-1A10 (A220-100)
      • BD-500-1A11 (A220-300)
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes TCCA AD CF-2020-32R1 issued 23 April 2021.
Publication(s) and related information ACLP SB BD500-538005 Issue 002, dated 22 February 2021, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada (TC). ACLP SB BD500-538008 Issue 003, dated 28 February 2023, or later revisions approved by the Chief, Continuing Airworthiness, TC. ACLP SB BD500-538011 Issue 001, dated 03 December 2024, or later revisions approved by the Chief, Continuing Airworthiness, TC. ACLP SB BD500-538006 Issue 001, dated 22 February 2021, or later revisions approved by the Chief, Continuing Airworthiness, TC. ACLP AMP DM BD500-A-J53-82-55-04AAA-720A-A (Aft fairing strut, Wing To Body Fairing (WTBF) - Install procedure) Issue 006, dated 26 June 2020, or later revisions.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu