Safety Publications Tool

F-2004-106 : Rotor - Main rotor blade / Tip cap junction

Number F-2004-106
Issued by Europe  Europe
Issue date 2004-07-07
Effective date 2004-07-17
EASA approval number 2004-7031
ATA Chapter 62
Approval Holder
/ Type Designation
  • AIRBUS HELICOPTERS
    • SA/AS 365 / EC 155
      • EC 155 B
      • EC 155 B1
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes DGAC France AD F-2003-418 dated 24 December 2003, EASA approval 2003-1649, which is also cancelled by its Revision 1.
Publication(s) and related information EUROCOPTER EC 155 Alert Service Bulletin No. 62A006.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu