Safety Publications Tool

2013-0042 : Engine – High Pressure Compressor Rotor Discs and Rotor Shafts – Inspection / Replacement

Number 2013-0042
Issued by Europe  Europe
Issue date 2013-02-26
Effective date 2013-03-12
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
    • RB211 TRENT 500
      • RB211 Trent 553-61
      • RB211 Trent 553A2-61
      • RB211 Trent 556-61
      • RB211 Trent 556A2-61
      • RB211 Trent 560A2-61
    • 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 Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2009-0073R1 dated 08 April 2009.
Publication(s) and related information Rolls-Royce NMSB RB.211-72-AF964 Revision 3 dated 11 January 2013. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
PAD number 13-017
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 21 January 2013 as PAD 13-017 for consultation until 18 February 2013. 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.eu.