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  Safety Publications Tool

2006-0182 : Engine - High Pressure Turbine Disc Rim Cooling Air Holes - Inspection

Number 2006-0182
Issued by Europe  Europe
Issue date 2006-06-28
Effective date 2006-07-10
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
    • RB211-535
      • RB211-535C-37
      • RB211-535E4-37
      • RB211-535E4-B-37
      • RB211-535E4-C-37
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Rolls-Royce RB211-535 NMSB 72-AE969, or a later approved revision. For a copy of this service information, or any questions concerning the technical content of the requirements in this AD, please contact Rolls Royce plc, PO Box 31, Derby, DE24 8BJ, United Kingdom. Telephone: +44 (0) 1332 242424, Fax: +44 (0) 1332 249936.
PAD number 06-134
Remarks This AD was posted as PAD 06-134 for consultation on 29 May 2006 with a comment period until 16 June 2006. The Comment Response Document can be found at https://ad.easa.europa.eu/. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu.