Safety Publications Tool

CF-2022-63 : Fuselage – Wing-to-Fuselage Joint – Moisture Ingress Between Front and Rear Spar Frame Segments

Number CF-2022-63
Issued by Canada  Canada
Issue date 2022-11-18
Effective date 2022-12-01
EASA approval number
ATA Chapter 53
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 Service Bulletin (SB) 84-53-81, Initial Revision dated 27 May 2022, Revision A dated 23 August 2022, 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