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CF-2025-62 : Fuselage – Tailboom – Elongated Holes and Gaps on Tailcone Assembly

Number CF-2025-62
Issued by Canada  Canada
Issue date 2025-12-05
Effective date 2025-12-12
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • BELL TEXTRON CANADA LTD (BTCL)
    • 505 (Jet Ranger X)
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Bell 505 Maintenance Planning Information, Chapter 4, ALS, Issue 024, dated 10 June 2025, or later revisions of the ALS approved by Transport Canada. Bell ASB 505-24-41, Revision A, dated 1 July 2025, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu