Safety Publications Tool

2009-0243R3 : [Correction 2] Engine – Front Combustion Liner Inner Wall – Inspection

Number 2009-0243R3
Issued by Europe  Europe
Issue date 2012-11-15
Effective date 2012-11-27
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
    • RB211 TRENT 700
      • 768-60
      • 772-60
      • 772B-60
      • 772C-60
    • RB211 TRENT 800
      • 875-17
      • 877-17
      • 884-17
      • 884B-17
      • 892-17
      • 892B-17
      • 895-17
    • RB211-524
      • G2-T-19
      • G3-T-19
      • H-T-36
      • H2-T-19
Revision This AD revises EASA AD 2009-0243R2 dated18 February 2011, including the Correction dated 22 February 2011.
Correction This AD has been republished to correct Service Bulletin number 72-AG705, where the prefix ‘A’ (indicating Alert) was inadvertently removed.
Supersedure None
Publication(s) and related information Rolls-Royce NMSB RB.211-72-AF458 Revision 4 dated 09 March 2009, or Revision 5 dated 20 April 2011. Rolls-Royce SB 72-AG705 dated 13 July 2012. Rolls-Royce SB 72-G706 dated 21 June 2012. Rolls-Royce SB 72-G707 dated 21 June 2012. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 09-114
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 28 September 2009 as PAD 09-114 for consultation until 26 October 2009. The Comment Response Document can be found at https://ad.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[dot]eu.