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CF-2009-41R1 : Fuselage - Cracking of Tail boom Fitting

Number CF-2009-41R1
Issued by Canada  Canada
Issue date 2016-11-02
Effective date 2016-11-07
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • BELL TEXTRON CANADA LTD (BTCL)
    • 206
      • 206L
      • 206L-1
      • 206L-3
      • 206L-4
Revision This AD revises AD CF-2009-41 issued on 16 November 2009.
Correction Not applicable
Supersedure None
Publication(s) and related information Alert Service Bulletin (ASB) 206L-09-158 Rev. B dated 1 June 2011 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