| Publication(s) and related information |
Airbus Helicopters Deutschland:
ASB MBB-BK117 C-2-85A-038 Revision 5 dated 18 November 2015, or Revision 6 dated 17 March 2016.
ASB MBB-BK117 C-2-85A-045 original issue dated 18 November 2015, or Revision 1 dated 05 May 2022.
ASB EC135-85A-058 Revision 6 dated 19 November 2015, or Revision 7 dated 17 March 2016, or Revision 8 dated 17 May 2016.
ASB EC135-85A-064 original issue dated 19 November 2015, or Revision 1 dated 30 June 2021.
Airbus Helicopters:
ASB AS365-25.01.25 Revision 6 dated 19 November 2015, or Revision 7 dated 17 March 2016.
ASB AS365-25.01.65 original issue dated 19 November 2015, or Revision 1 dated 24 May 2016, or Revision 2 dated 29 October 2018, or Revision 3 dated 25 July 2019, or Revision 4 dated 30 September 2020.
ASB AS332-25.02.70 Revision 6 dated 19 November 2015, or Revision 7 dated 17 March 2016.
ASB AS332-25.03.19 original issue dated 19 November 2015, or Revision 1 dated 24 May 2016, or Revision 2 dated 29 October 2018, or Revision 3 dated 25 July 2019, or Revision 4 dated 22 June 2020.
ASB EC225-25A133 Revision 6 dated 19 November 2015, or Revision 7 dated 17 March 2016.
ASB EC225-25A186 original issue dated 19 November 2015, or Revision 1 dated 17 March 2016.
ASB EC225-25A187 original issue dated 19 November 2015, or Revision 1 dated 24 May 2016, or Revision 2 dated 29 October 2018, or Revision 3 dated 25 July 2019, or Revision 4 dated 22 June 2020.
ASB EC225-25A188 original issued dated 19 November 2015, or Revision 1 dated 29 October 2018 or Revision 2 dated 22 June 2020.
Leonardo, Helicopter Division:
BT 139-443 dated 19 November 2015, or Revision A dated 21 April 2016.
BT 109SP-100 dated 19 September 2015, or Revision A dated 21 April 2016.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
Bell Textron Canada Ltd:
ASB 429-14-15 Revision B dated 10 March 2016 (see Note 4 of this AD);
ASB 429-14-15 Revision E dated 5 September 2023 (Part I only).
Bell Textron, Inc.: None.
MD Helicopters, LLC.: None.
McDermott 214 Holdings, LLC: None.
Sikorsky Aircraft Corporation: None.
Note 4: Where BTCL ASB 429-14-15 Revision B refers to the �most current version� of Goodrich ASB 44301-10-18, only the use of Revision 5 dated 23 February 2016 is acceptable to comply with this AD. Future revisions will need to be accepted by EASA. |
| Remarks |
1.
This Proposed AD will be closed for consultation on 04 June 2026.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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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