Safety Publications Tool

CF-2014-45R3 : Nacelle – A-Frame Structure – Insufficient Fillet Radius and Fouling with Main Landing Gear Stabilizer Brace and the Electrical Wiring Harnesses

Number CF-2014-45R3
Issued by Canada  Canada
Issue date 2017-06-19
Effective date 2017-06-28
EASA approval number
ATA Chapter 54
Approval Holder
/ Type Designation
  • DE HAVILLAND AIRCRAFT OF CANADA LTD.
    • DHC-8
      • DHC-8-400
      • DHC-8-401
      • DHC-8-402
Revision Revision 3 of this AD is issued to correct the revision block. In revision 2, the revision block above should have stated that CF-2014-45R1 was issued on 19 September 2016.
Correction Not applicable
Supersedure This AD supersedes TCCA AD CF-2014-45R2, issued 29 March 2017.
Publication(s) and related information Bombardier SB 84-32-114 Initial Issue, dated 06 June 2013, or Revision A, dated 18 September 2013; SB 84-32-147, initial revision, dated 5 August 2016; SB 84-54-19, Initial Issue, dated 18 April 2013; SB 84-54-20 Initial Issue, dated 25 April 2013, or Revision A dated 09 April 2014, or Revision B, dated 2 October 2014; and SB 84-54-21, Initial Issue, dated 9 May 2013; 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.