Number |
2019-0236R2 |
Issued by |
Europe |
Issue date |
2021-05-07 |
Effective date |
2021-05-14 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
32 |
Approval Holder / Type Designation |
-
ATR
-
ATR72
-
101
-
102
-
201
-
202
-
211
-
212
-
212A
|
Revision |
This AD revises EASA AD 2019-0236R1 dated 31 August 2020.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
ATR AOM 2019/12 Issue 1 dated 30 July 2019, or Issue 2 dated 06 August 2019, or Issue 3 dated 01 October 2019, or Issue 4 dated 03 September 2020.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
PAD number |
19-155 |
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 13 August 2019 as PAD 19-155 for consultation until 27 August 2019. The Comment Response Document 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.
|