Safety Publications Tool
2012-0195-E : [Correction] Tail Rotor – Tail Rotor Duplex Bearing Ring Nut – Inspection
EASA approval number
EASA Rotorcraft Section
/ Type Designation
LEONARDO S.p.A. HELICOPTERS
This AD has been republished to correct a typographical mistake with the applicable TCDS number (EASA.R.005 is correct instead of EASA.A.005).
Publication(s) and related information
AgustaWestland BT 109-134 dated 21 September 2012. AgustaWestland BT 109SP-051 dated 21 September 2012. AgustaWestland BT 109S-48 dated 21 September 2012. AgustaWestland BT 109L-051 dated 21 September 2012. AgustaWestland BT 109EP-121 dated 21 September 2012. AgustaWestland BT 109K-54 dated 21 September 2012. AgustaWestland A109E MM “A109E-MM” second issue, Revision 2 dated 29 June 2012. AgustaWestland A109LUH MM “09-A/AM-00-X” Issue 1.0, Change 15 dated 15 December 2011. AgustaWestland A109S & AW109SP MM “0B-A-AMP-00-X” dated 08 June 2012. AgustaWestland A109C MM “A109C-MM” Basic Issue, Rev. 15 dated 14 July 2010 and Temporary Revisions 64-1 and 64-2 dated 25 May 2012. AgustaWestland A109K2 MM “A109K2-MM” Basic Issue, Rev. 15 dated 15 September 2010 and Temporary Revisions 64-1 and 64-2 dated 25 May 2012. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The results of the safety assessment have indicated the need for immediate publication and notification, without the full public consultation process. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.
easa_ad_2012_0195_E_Correction.pdf (146 kb)
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