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CF-2024-40 : Main Rotor – Pitch Link Assembly Clevis Fracture

Number CF-2024-40
Issued by Canada  Canada
Issue date 2024-12-04
Effective date 2024-12-17
EASA approval number
ATA Chapter 62
Approval Holder
/ Type Designation
  • BELL TEXTRON CANADA LTD (BTCL)
    • 430
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes TCCA AD CF-2021-26, issued 26 July 2021.
Publication(s) and related information Bell ASB 430-22-61, Basic Issue, dated 6 November 2023, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada. Bell 430 Maintenance Manual BHT-430-MM-2, Chapter 4, ALS, Revision 23, dated 28 September 2023, or later revisions approved by 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