Number |
2019-0069R1 |
Issued by |
Europe |
Issue date |
2023-08-08 |
Effective date |
2023-08-15 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
25 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A318
-
A318-112
-
A318-121
-
A318-122
-
A319
-
A319-111
-
A319-112
-
A319-115
-
A319-131
-
A319-132
-
A319-133
-
A320
-
A320-214
-
A320-216
-
A320-232
-
A320-233
-
A320-251N
-
A320-271N
-
A321
-
A321-211
-
A321-212
-
A321-213
-
A321-231
-
A321-232
-
A321-251N
-
A321-253N
-
A321-271N
-
A321-272N
|
Revision |
This AD revises EASA AD 2019-0069 dated 28 March 2019.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus SB A320-25-1BGJ original issue dated 19 December 2017, or Revision 01 dated 21 August
2018.
Airbus SB A320-25-1BGK original issue dated 13 October 2017, or Revision 01 dated 24 August 2018,
Airbus SB A320-25-1BGL original issue dated 13 October 2017, or Revision 01 dated 21 August 2018,
Airbus SB A320-25-1BKW original issue dated 19 February 2018, or Revision 01 dated 21 August
2018
Airbus SB A320-25-1BKT original issue dated 23 September 2019, Revision 01 dated 03 April 2020,
Revision 02 dated 06 May 2020, Revision 03 dated 16 December 2020, or Revision 04 dated 07
March 2022.
Airbus SB A320-25-1BKM original issue dated 04 February 2019, Revision 01 dated 04 June 2019,
Revision 02 dated 29 April 2020, Revision 03 dated 11 January 2021, or Revision 04 dated 08 July
2022.
Airbus SB A320-25-1BKS original issue dated 06 February 2019, Revision 01 dated 11 July 2019,
Revision 02 dated 06 April 2020, Revision 03 dated 05 October 2020, Revision 04 dated 02 June
2021, or Revision 05 dated 18 May 2022.
Airbus SB A320-25-1CDB original issue dated 09 June 2023, or Revision 01 dated 06 July 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
18-013 |
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 29 January 2018 as PAD 18-013 for consultation
until 26 February 2018, and republished on 28 January 2019 as PAD 18-013R1 for additional
consultation until 25 February 2019. The Comment Response Documents 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 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.
|