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CF-2001-05R1 : Main Rotor to Horizontal Stabilizer Endplate Clearance - Auxiliary Fin Size Modification

Number CF-2001-05R1
Issued by Canada  Canada
Issue date 2002-02-13
Effective date 2002-03-29
EASA approval number
ATA Chapter 62
Approval Holder
/ Type Designation
  • BELL TEXTRON CANADA LTD (BTCL)
    • 427
Revision This AD revises TCCA AD CF-2001-05 issued January 2001, to introduce an auxiliary fin size modification. In addition, AD CF-2001-25R1 is no longer required due to the change in end plate size imposed by this revision to AD CF-2001-05.
Correction Not applicable
Supersedure This revised AD supersedes and cancels TCCA AD CF-2001-05 issued January 2001.
Publication(s) and related information BHTC ASB 427-01-07 dated 16 November 2001, and RFM BHT-427-FM-2, Rev 3 dated 31 October 2001, or BHT-427-FM-3, Rev 1 dated 9 November 2001, as appropriate, or later revisions approved by 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

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