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F-2004-030R1 : Tail rotor - Tail Rotor Hub Pitch Control Rod

Number F-2004-030R1
Issued by Europe  Europe
Issue date 2005-03-30
Effective date 2005-04-09
EASA approval number 2005-2581
ATA Chapter 64
Approval Holder
/ Type Designation
  • AIRBUS HELICOPTERS
    • SA 330 / AS 332 / EC 225
      • SA 330 J
Revision This AD revises DGAC AD F-2004-030 original issue, EASA Approval Number 2004-1047. The purpose of Revision 1 of this AD is to cover the conversion of EUROCOPTER SA 330 Alert Telex No. 65.111 into an Alert Service Bulletin (ASB) bearing the same reference number, with no change to the technical content.
Correction Not applicable
Supersedure This AD supersedes DGAC AD F-2004-030 original issue
Publication(s) and related information EUROCOPTER SA 330 Alert Service Bulletin No. 65.111. (Any subsequent approved revision of this ASB is acceptable).
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu