Safety Publications Tool
2012-0071 : Engine – Axial Compressor, Gas Generator Hollow Shaft and Rear Bearing – Identification / Inspection / Cleaning / Replacement
EASA approval number
EASA Propulsion Section
/ Type Designation
SAFRAN HELICOPTER ENGINES
This AD supersedes DGAC France AD 1990-064(A) R1 dated 21 March 2001.
Publication(s) and related information
Turboméca MSB A292 72 0230 Version C dated 29 February 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. This AD was posted on 23 March 2012 as PAD 12-021 for consultation until 20 April 2012. The Comment Response Document can be found at https://ad.easa.europa.eu. 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_0071.pdf (30 kb)
easa_pad_12_021.zip (64 kb)
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