Safety Publications Tool
2022-0222 : Engine Exhaust – Thrust Reverser Lower Beam – Inspection / Repair
EASA approval number
EASA Large Aeroplanes Department
/ Type Designation
This AD supersedes EASA AD 2018-0148R1 dated 05 April 2019.
Publication(s) and related information
Airbus SB A330-78-3023 original issue dated 12 December 2017, or Revision 01 dated 27 September 2022. Rolls-Royce NMSB RB211-78-AH677 original issue dated 18 December 2017. Safran Nacelles SB 78-AH677 dated 18 December 2017. 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. This AD was posted on 28 September 2022 as PAD 22-130 for consultation until 26 October 2022. No comments were received during the consultation period. 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_2022_0222.pdf (222 kb)
EASA_PAD_22_130.zip (420 kb)
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