You are not logged in
  Safety Publications Tool

2024-0110 : Rotors Flight Controls – Upper Ball Bearing End of the Main Rotor Servo-Controls – Inspection

Number 2024-0110
Issued by Europe  Europe
Issue date 2024-06-06
Effective date 2024-06-20
EASA approval number
Contributor EASA VTOL Department
ATA Chapter 67
Approval Holder
/ Type Designation
  • AIRBUS HELICOPTERS
    • SA/AS 365 / EC 155
      • AS 365 N2
      • AS 365 N3
      • EC 155 B
      • EC 155 B1
      • SA 365 N
      • SA 365 N1
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus Helicopters ASB AS365-67-30-0001 Revision 01 dated 18 April 2024. Airbus Helicopters ASB EC155-67-30-0001 Revision 01 dated 18 April 2024. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 24-050
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 08 May 2024 as PAD 24-050 for consultation until 05 June 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@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.