| Number |
2022-0021 |
| Issued by |
 Europe |
| Issue date |
2022-02-01 |
| Effective date |
2022-02-15 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2017-0189 dated 22 September 2017.
|
| Publication(s) and related information |
AH AS332 Emergency ASB 01.00.86 original issue dated 27 July 2017, or Revision 1 dated 25 August 2017, or Revision 2 dated 02 March 2020, or Revision 3 dated 19 August 2021, or Revision 4 dated 06 January 2022.
AH EC225 Emergency ASB 04A013 original issue dated 27 July 2017, or Revision 1 dated 25 August 2017, or Revision 2 dated 02 March 2020, or Revision 3 dated 19 August 2021, or Revision 4 dated 06 January 2022.
AH SB AS332-53.02.03 original issue dated 19 August 2021, or AH ASB AS332-53.02.03 Revision 1 dated 06 January 2022.
AH SB EC225-53-065 original issue dated 19 August 2021, or AH ASB EC225-53065 Revision 1 dated 06 January 2022.
AH AS332 L2 ALS Revision 009 dated 02 June 2021.
AH EC 225 LP ALS Revision 013 dated 08 March 2021.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
21-126R1 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was initially posted on 20 August 2021 as PAD 21-126 for consultation until 17 September 2021 and republished on 10 January 2022 as PAD 21-126R1 for additional consultation until 31 January 2022. 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.
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