Safety Publications Tool

CF-2011-24R1 : Wings - Wing to Fuselage Attachment Joints - Barrel Nut Cracking

Number CF-2011-24R1
Issued by Canada  Canada
Issue date 2019-01-28
Effective date 2019-02-04
EASA approval number
ATA Chapter 57
Approval Holder
/ Type Designation
  • DE HAVILLAND AIRCRAFT OF CANADA LTD.
    • DHC-8
      • DHC-8-400
      • DHC-8-401
      • DHC-8-402
Revision This AD supersedes Canadian AD CF-2011-24, issued 21 July 2011.
Correction Not applicable
Supersedure None
Publication(s) and related information Bombardier Alert Service Bulletin (ASB) A84-57-25, Initial Issue, dated 20 July 2011, Revision A, dated 16 July 2018, ASB A84-57-19 Initial Issue, dated 1 February 2008; Revision A, dated 8 February 2008; Revision B, dated 6 March 2008; Revision C, dated 20 August 2008; Revision D, dated 12 August 2011, Service Bulletin (SB) 84-57-26 Initial Issue, dated 21 March 2013; Revision A, dated 18 July 2014; or Revision B, dated 26 February 2015, Revision C, dated 16 July 2018, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada
Remarks At the moment of adoption of this AD, the model 400 has not been validated in Europe. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu.