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CF-2010-30R2 : Cracking of the Nacelle Attachment Fitting(s)

Number CF-2010-30R2
Issued by Canada  Canada
Issue date 2019-08-01
Effective date 2019-08-13
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 Not applicable
Correction Not applicable
Supersedure This revised AD supersedes AD CF-2010-30R1, issued 21 September 2010.
Publication(s) and related information Bombardier Service Bulletin (SB) 84-54-14 Revision K, dated 7 August 2018, SB 84-54-16 Initial Revision, dated 29 April 2011, Revision A, dated 1 August 2011, or Revision C, dated 31 January 2017, Revision D, dated 7 August 2018, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada. SB 84-54-14 Revision J dated 17 September 2010, SB 84-54-15 Initial issue dated 20 August 2010, Revision A dated 25 October 2010, Revision B dated 2 February 2017, or Revision C dated 7 August 2018.
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 Programming and Continued Airworthiness Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu.