You are not logged in
  Safety Publications Tool

EAD CF-2025-29 : Tail Rotor Blade Abrasion Strip Cracks

Number CF-2025-29
Issued by Canada  Canada
Issue date 2025-06-09
Effective date 2025-06-09
EASA approval number
ATA Chapter 64
Approval Holder
/ Type Designation
  • BELL TEXTRON CANADA LTD (BTCL)
    • 429
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes TCCA Emergency AD CF-2024-11, issued 22 March 2024.
Publication(s) and related information Bell ASB 429-24-63 Revision B, dated 6 November 2024, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada.
Remarks Comments regarding this EAD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu