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CF-2007-12 : Tail Rotor Pitch Change Mechanism

Number CF-2007-12
Issued by Canada  Canada
Issue date 2007-09-14
Effective date 2007-09-17
EASA approval number
ATA Chapter
Approval Holder
/ Type Designation
  • BELL TEXTRON CANADA LTD (BTCL)
    • 230
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Bell Helicopter Textron Alert Service Bulletin (ASB) 230-07-36 dated 09 January 2007, 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