Safety Publications Tool
2021-0129R1 : Engine Fuel & Control – Low Pressure Compressor Case Static P30 Air System – Modification
EASA approval number
EASA Environment & Propulsion Systems Department
/ Type Designation
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
RB211 TRENT 900
This AD revises EASA AD 2021-0129 dated 18 May 2021.
Publication(s) and related information
Rolls-Royce Trent 900 SB RB.211-73-K278 original issue dated 30 January 2019, or Alert SB RB.211-73-AK278 Revision 1 dated 14 April 2021. Rolls-Royce Trent 900 SB RB.211-73-J441 original issue dated 09 May 2017, or Revision 1 dated 30 January 2019, or Revision 3 dated 23 May 2022. Rolls-Royce Trent 900 SB RB.211-73-G165 original issued dated 08 September 2009, or Revision 1 dated 19 April 2011, or Revision 2 dated 06 April 2016. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The original issue of this AD was initially posted on 30 April 2021 as PAD 21-062, republished on 07 May 2021 as PAD 21-062R1 and closed for consultation on 14 May 2021. The Comment Response Documents can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this PAD. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.
EASA_AD_2021_0129_R1.pdf (209 kb)
EASA_PAD_21_062.zip (1 mb)
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