Safety Publications Tool

2010-0058R1 : Rotor Flight Controls – Tail Rotor, Cyclic and Collective Control Levers – Inspection / Repair

Number 2010-0058R1
Issued by Europe  Europe
Issue date 2017-04-07
Effective date 2017-04-07
EASA approval number
ATA Chapter 67
Approval Holder
/ Type Designation
  • AIRBUS HELICOPTERS DEUTSCHLAND
    • EC135/635
      • EC135 P1
      • EC135 P2
      • EC135 P2+
      • EC135 T1
      • EC135 T2
      • EC135 T2+
      • EC635 P2+
      • EC635 T1
      • EC635 T2+
    • MBB-BK 117
      • MBB-BK 117 C-2
Revision This AD revises EASA AD 2010-0058 dated 30 March 2010, which superseded Luftfahrt-Bundesamt (LBA) Germany AD D-2008-178 and AD D-2008-179, both dated 31 May 2008.
Correction Not applicable
Supersedure The original issue of this AD superseded Luftfahrt-Bundesamt (LBA) Germany AD D-2008-178 and AD D-2008-179, both dated 31 May 2008.
Publication(s) and related information ECD ASB EC135-67A-019 Revision 3 dated 16 December 2009, or Airbus Helicopters ASB EC135-67A-019 Revision 4 dated 03 April 2017. ECD ASB MBB-BK117 C-2-67A-010 Revision 3 dated 08 February 2010, or Airbus Helicopters ASB MBB-BK117 C-2-67A-010 Revision 4 dated 03 April 2017. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 10-025
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The original issue of this AD was posted on 10 March 2010 as PAD 10-025 for consultation until 24 March 2010. No comments were received during the consultation period. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.