Number |
2021-0115R1 |
Issued by |
Europe |
Issue date |
2021-07-05 |
Effective date |
2021-07-12 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
28 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A318
-
A318-111
-
A318-112
-
A318-121
-
A318-122
-
A319
-
A319-111
-
A319-112
-
A319-113
-
A319-114
-
A319-115
-
A319-131
-
A319-132
-
A319-133
-
A319-151N
-
A319-153N
-
A319-171N
-
A320
-
A320-211
-
A320-212
-
A320-214
-
A320-215
-
A320-216
-
A320-231
-
A320-232
-
A320-233
-
A320-251N
-
A320-252N
-
A320-253N
-
A320-271N
-
A320-272N
-
A320-273N
-
A321
-
A321-111
-
A321-112
-
A321-131
-
A321-211
-
A321-212
-
A321-213
-
A321-231
-
A321-232
-
A321-251N
-
A321-251NX
-
A321-252N
-
A321-252NX
-
A321-253N
-
A321-253NX
-
A321-271N
-
A321-271NX
-
A321-272N
-
A321-272NX
|
Revision |
This AD revises EASA Emergency AD 2021-0115-E dated 23 April 2021.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus AOT A28N009-21 original issue dated 19 April 2021, and Revision 01 dated 04 May 2021.
SAFRAN SB P99C38-28-004 original issue dated 27 April 2021, or Revision 01 dated 25 June 2021.
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.
|