Number |
2018-0234R3 |
Issued by |
Europe |
Issue date |
2021-01-22 |
Effective date |
2021-02-05 |
EASA approval number |
|
Contributor |
EASA Large Transport Aeroplanes Section |
ATA Chapter |
78 |
Approval Holder / Type Designation |
|
Revision |
This AD revises EASA AD 2018-0234R2 dated 17 September 2019.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus AOT A78P001-18 Revision 01 dated 16 October 2018, or Revision 02 dated 29 April 2019, or Revision 03 dated 29 July 2019, or Revision 04 dated 17 December 2020.
Airbus A350 MMEL MER dated 22 October 2018.
Airbus FOT Ref. 999.0083/18 original issue dated 22 October 2018.
Goodrich SB RA35078-048 original issue dated 22 June 2018, or Revision 1 dated 26 October 2018, or Revision 2 dated 25 April 2019, or Revision 3 dated 29 July 2019.
MP Task No. A350-A-78-3X-XX-05001-560A-A issue date 02 November 2018.
MP Task No. A350-A-78-3X-XX-03001-560A-A issue date 02 November 2018.
MP Task No. A350-A-78-3X-XX-03001-760A-A issue date 02 November 2018.
Airbus A350 ALS Part 4 Revision 05 issue 2 dated 25 June 2020.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
Remarks |
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.
|