Number |
2020-0203 |
Issued by |
Europe |
Issue date |
2020-09-23 |
Effective date |
2020-10-07 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
31 |
Approval Holder / Type Designation |
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2020-0090R1 dated 21 July 2020.
|
Publication(s) and related information |
Airbus A350 AFM TR 123 Issue 1 dated 05 February 2020.
Airbus A350 AFM TR 124 Issue 1 dated 02 April 2020.
Airbus SB A350-31-P038 original issue dated 17 April 2020.
Airbus SB A350-31-P039 original issue dated 04 August 2020.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
Airbus FOT Ref. 999.0006/20 Revision 02 dated 16 April 2020.
Airbus A350 MMEL MER dated 09 April 2020, EASA approval reference D20008466, which is available at AirbusWorld. |
PAD number |
20-131 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 03 September 2020 as PAD 20-131 for consultation until 17 September 2020. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness 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.
|