Number |
2020-0182R1 |
Issued by |
Europe |
Issue date |
2021-10-29 |
Effective date |
2021-11-05 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
AIRBUS DEFENCE & SPACE S.A.
-
C-212
-
C-212-CB
-
C-212-CC
-
C-212-CD
-
C-212-CE
-
C-212-CF
-
C-212-DD
-
C-212-DE
-
C-212-DF
-
C-212-EE
-
C-212-VA
|
Revision |
This AD revises EASA AD 2020-0182 dated 13 August 2020.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus D&S AOT-C212-53-0001 original issue dated 07 August 2019 or Revision 1 dated 30 January 2020.
Airbus D&S SB-C212-53-0055 original issue dated 19 April 2021.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
EADS-CASA SB-212-53-0054C original issue dated 05 November 2018. |
PAD number |
20-111 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 14 July 2020 as PAD 20-111 for consultation until 11 August 2020. 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@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.
|