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2011-0168R1 : Lights – Instrument Lighting Display Brightness – Modification

Number 2011-0168R1
Issued by Europe  Europe
Issue date 2018-03-23
Effective date 2018-03-23
EASA approval number
ATA Chapter 33
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 2011-0168 dated 02 September 2011.
Correction Not applicable
Supersedure The original issue of this AD superseded EASA Emergency AD 2010-0247-E dated 26 November 2010.
Publication(s) and related information ECD ASB EC135-33A-009 Revision 2 dated 30 June 2011. ECD ASB MBB BK117 C-2-33A-013 Revision 2 dated 30 June 2011. ECD SB MBB-BK117 C-2-33-006 original issue dated 04 October 2007, or Revision 1 dated 15 September 2008, or Revision 2 dated 12 April 2011, or Airbus Helicopter Deutschland SB MBB-BK117 C-2-33-006 Revision 3 dated 24 April 2014. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 11-080
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 02 August 2011 as PAD 11-080 for consultation until 30 August 2011. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa.eu.