Safety Publications Tool
2019-0282R1 : Engine – Intermediate Pressure Compressor Shaft Assembly – Inspection
EASA approval number
EASA Environment and Propulsion Systems Department
/ Type Designation
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
This AD revises EASA AD 2019-0282 dated 20 November 2019.
Publication(s) and related information
Rolls-Royce TRENT 1000 Alert NMSB 72-AK451 original issue dated 14 November 2019, or Revision 1 dated 15 July 2021. Rolls-Royce TRENT 1000 NMSB 72-K618 original issue dated 08 September 2020, or Revision 1 dated 15 July 2021. Rolls-Royce TRENT 1000 SB 72-K570 original issue dated 15 June 2021. Rolls-Royce TRENT 1000 SB 72-K571 original issue dated 15 June 2021. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. Rolls-Royce TRENT 1000 NMSB 72-K452 original issue dated 21 October 2019.
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 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_2019_0282_R1.pdf (213 kb)
EASA_AD_2019_0282.zip (1 mb)
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