| Number |
2022-0061 |
| Issued by |
 Europe |
| Issue date |
2022-04-04 |
| Effective date |
2022-04-18 |
| EASA approval number |
|
| Contributor |
EASA Environment & Propulsion Systems Department |
| ATA Chapter |
61 |
Approval Holder
/ Type Designation |
-
HOFFMANN PROPELLER GmbH & Co. KG
-
HO-V 72
-
HO-V 72 B
-
HO-V 72 F
-
HO-V 72 G
-
HO-V 72 L
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2020-0226R1 dated 31 March 2021.
|
| Publication(s) and related information |
Hoffmann Propeller SB E53 Revision A dated 09 October 2020, or Revision B dated 14 October 2020, or Revision C dated 9 December 2020, or Revision D dated 18 February 2021.
Hoffmann Propeller SB057 Revision B dated 08 February 2022, or Revision C dated 22 February 2022.
Hoffmann Propeller SB058 Revision A dated 02 February 2022.
Hoffmann Propeller SB059 Revision A dated 11 February 2022, or Revision B dated 23 February 2022.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication.
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 aeroplane with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.
|
