| Number |
2019-0241R1 |
| Issued by |
 Europe |
| Issue date |
2021-11-29 |
| Effective date |
2021-12-06 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
POWERJET S.A.
-
SaM146
-
SaM146-1S17
-
SaM146-1S17C
-
SaM146-1S18
-
SaM146-1S18C
|
| Revision |
This AD revises EASA AD 2019-0241 dated 26 September 2019.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Powerjet S.A. SaM146-1S S/B No. 72-0227 original issue dated 02 August 2019, or Revision 1 dated 27 September 2019, or Revision 2 dated 05 May 2021, or Revision 3 dated 12 October 2021.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
19-160 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 26 August 2019 as PAD 19-160 for consultation until 23 September 2019. No comments were received during the consultation period.
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.
|
