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2024-0133R1 : Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

Number 2024-0133R1
Issued by Europe  Europe
Issue date 2025-06-27
Effective date 2025-07-11
EASA approval number
ATA Chapter 04
Approval Holder
/ Type Designation
  • AIRBUS HELICOPTERS
    • AS 350 / EC 130
      • AS 350 B
      • AS 350 B1
      • AS 350 BA
      • AS 350 BB
      • AS 350 D
Revision This AD revises EASA AD 2024-0133 dated 10 July 2024.
Correction Not applicable
Supersedure The original issue of this AD superseded DGAC France AD F-1984-064-037R3 dated 02 February 1994 and EASA AD 2021-0194R1 dated 08 October 2021.
Publication(s) and related information AH AS 350 B AMM Chapter 04 ALS Revision 009 dated 09 October 2023. AH AS 350 B1 AMM Chapter 04 ALS Revision 009 dated 09 October 2023. AH AS 350 BB AMM Chapter 04 ALS Revision 009 dated 09 October 2023. AH AS 350 BA AMM Chapter 04 ALS Revision 009 dated 09 October 2023. AH AS 350 D AMM Chapter 04 ALS Revision 009 dated 09 October 2023. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 24-068
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The original issue of this AD was posted on 17 June 2024 as PAD 24-068 for consultation until 01 July 2024. 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.