Safety Publications Tool

CF-2026-06 : Landing Gear – Main Landing Gear Aft Door Mechanism – Lock Link Apex Pin/Bolt Fracture

Number CF-2026-06
Issued by Canada  Canada
Issue date 2026-02-05
Effective date 2026-02-17
EASA approval number
ATA Chapter 32
Approval Holder
/ Type Designation
  • DE HAVILLAND AIRCRAFT OF CANADA LTD.
    • DHC-8
      • DHC-8-401
      • DHC-8-402
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information De Havilland Aircraft of Canada SB 84-32-179 Rev: NC dated 30 October 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