Number |
2017-0132R2 |
Issued by |
Europe |
Issue date |
2021-08-03 |
Effective date |
2021-08-10 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
71 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A318
-
A319
-
A319-111
-
A319-112
-
A319-113
-
A319-114
-
A319-115
-
A320
-
A320-211
-
A320-212
-
A320-214
-
A320-215
-
A320-216
-
A321
-
A321-111
-
A321-112
-
A321-211
-
A321-212
-
A321-213
|
Revision |
This AD revises EASA AD 2017-0132R1 dated 22 November July 2017
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus SB A320-71-1065 original issue dated 01 December 2016, and Revision 01 dated 28 July
2017.
Airbus SB A320-71-1066 original issue dated 01 December 2016.
Goodrich Aerospace SB RA32071-159 original issue dated 20 November 2016.
The use of later approved revisions of these documents is acceptable for compliance with the
requirements of this AD.
|
PAD number |
17-067 |
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 06 June 2017 as PAD 17-067 for consultation until
04 July 2017. The Comment Response Document can be found at https://ad.easa.europa.eu in
the compressed (zipped) file attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification
Directorate, EASA. 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.
|