Number |
2021-0239 |
Issued by |
Europe |
Issue date |
2021-11-05 |
Effective date |
2021-11-19 |
EASA approval number |
|
Contributor |
EASA VTOL Department |
ATA Chapter |
05 |
Approval Holder / Type Designation |
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2018-0272 dated 13 December 2018.
|
Publication(s) and related information |
AH ASB SA330-05.103 original issue dated 20 March 2018, or Revision 1 dated 10 December 2018,
or Revision 2 dated 13 January 2021, or Revision 3 dated 04 October 2021.
AH ASB SA330-65.139 original issue dated 04 October 2021.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
21-142 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 07 October 2021 as PAD 21-142 for consultation until 04 November
2021. 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.
|