Number |
2022-0004 |
Issued by |
Europe |
Issue date |
2022-01-11 |
Effective date |
2022-01-25 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A300
-
A300B4-203
-
A300B4-2C
-
A300C4-203
-
A300F4-203
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes paragraph 1.8 of DGAC France AD 1990-222-116(B) R5.
|
Publication(s) and related information |
Airbus SB A300-53-0278 original issue dated 12 November 1990, or Revision 01 dated 17 March 1994, or Revision 02 dated 10 November 1995, or Revision 03 dated 30 June 2021.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
PAD number |
21-174 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 29 November 2021 as PAD 21-174 for consultation until 27 December 2021. 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.
|