Number |
2020-0179R1 |
Issued by |
Europe |
Issue date |
2023-07-28 |
Effective date |
2023-08-04 |
EASA approval number |
|
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
EMBRAER S.A.
-
ERJ 170
-
ERJ 170-100 LR
-
ERJ 170-100 STD
-
ERJ 170-200 LR
-
ERJ 170-200 STD
-
ERJ 190
-
ERJ 190-100 IGW
-
ERJ 190-100 LR
-
ERJ 190-100 SR
-
ERJ 190-100 STD
-
ERJ 190-200 IGW
-
ERJ 190-200 LR
-
ERJ 190-200 STD
|
Revision |
This AD revises EASA AD 2020-0179 dated 12 August 2020.
|
Correction |
Not applicable
|
Supersedure |
For affected aeroplanes operated under EU regulation, the original issue of this AD replaced
ANAC Brazil State of Design AD 2017-03-01, which was not adopted by EASA.
|
Publication(s) and related information |
Embraer 170/175 MRB Report MRB-1621 Revision 13 dated 10 May 2017, Task 53-10-001-0003.
Embraer 190/195 MRB Report MRB-1928 Revision 11 dated 10 May 2017, Task 53-10-001-0003.
Embraer SB 170-53-0051 original issue dated 26 February 2010, or Revision 01 dated 25 May 2011,
or Revision 02 dated 28 May 2012, or Revision 03 dated 21 Augustus 2013, or Revision 04 dated
29 September 2017, or Revision 05 dated 22 February 2018.
Embraer SB 190-53-0019 original issue dated 26 February 2010, or Revision 01 dated 25 May 2011,
or Revision 02 dated 28 May 2012, or Revision 03 dated 21 Augustus 2013, or Revision 04 dated
21 February 2017, or Revision 05 dated 29 September 2017, or Revision 06 dated 22 February 2018. |
PAD number |
20-057 |
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 25 March 2020 as PAD 20-057 for consultation until
22 April 2020. 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 Programming and Continued Airworthiness 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.
|