Number |
2022-0078 |
Issued by |
Europe |
Issue date |
2022-05-04 |
Effective date |
2022-05-18 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A300-600
-
A300B4-603
-
A300B4-605R
-
A300B4-622
-
A300B4-622R
-
A310
-
A310-203
-
A310-222
-
A310-304
-
A310-308
-
A310-322
-
A310-324
-
A310-325
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2014-0202R1 dated 19 September 2014.
|
Publication(s) and related information |
Airbus SB A310-53-2138 original issue dated 28 May 2014, or Revision 01 dated 14 December 2021.
Airbus SB A300-53-6175 original issue dated 28 May 2014, or Revision 01 dated 07 December 2021.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
22-036 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 29 March 2022 as PAD 22-036 for consultation until 26 April 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.
|