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2022-0083 : Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment |  Print  Download |
| Number | 2022-0083 |
| Issued by |  Europe |
| Issue date | 2022-05-11 |
| Effective date | 2022-05-25 |
| EASA approval number |
| Contributor | EASA Environment & Propulsion Systems Department |
| ATA Chapter | 05 |
| Approval Holder / Type Designation | - SAFRAN HELICOPTER ENGINES
- ARRIEL 2
- ARRIEL 2D
- ARRIEL 2E
- ARRIEL 2H
- ARRIEL 2L2
- ARRIEL 2N
|
| Revision | Not applicable |
| Correction | Not applicable |
| Supersedure | This AD supersedes EASA AD 2018-0273 dated 13 December 2018. |
| Publication(s) and related information | SAFRAN ARRIEL 2 Chapter 05-10 Overhaul Manual X292 R1 500 2 update 23 dated 30 December 2021. SAFRAN ARRIEL 2D Chapter 05-10 MM X292 R1 450 2 update 23 dated 30 December 2021. SAFRAN ARRIEL 2E Chapter 05-10 MM X292 R2 300 2 update 19 dated 30 December 2021. SAFRAN ARRIEL 2H Chapter 05-10 MM X292 2H 450 2 update 8 dated 30 December 2021. SAFRAN ARRIEL 2L2 Chapter 05-10 MM X292 2L 450 2 update 1 dated 30 December 2021. SAFRAN ARRIEL 2N Chapter 05-10 MM X292 N2 450 2 update 14 dated 30 December 2021. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number | 22-042 |
| Remarks | 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was published on 07 April 2022 as PAD 22-042 for consultation until 05 May 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. |
Download attachments:
- EASA_AD_2022_0083.pdf (200 kb)
- EASA_PAD_22_042.zip (377 kb)
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