Safety Publications Tool
2010-0228R1 : Engine - M01 Compressor - Second Stage Compressor Axial Wheel and Impeller – Inspection
EASA approval number
EASA Propulsion Section
/ Type Designation
SAFRAN HELICOPTER ENGINES
This AD revises EASA AD 2010-0228 dated 03 November 2010, which superseded EASA AD 2010-0114-E dated 14 June 2010.
Publication(s) and related information
ROLLS-ROYCE TURBOMECA Ltd Emergency Mandatory Service Bulletin SBP-M3-A-72-31-00-05A-A-A Issue number 002. ROLLS-ROYCE TURBOMECA Ltd Emergency Mandatory Service Bulletin SBP-M3-A-71-00-00-05A-A-A Issue number 001. The use of later approved revisions of these documents 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 original issue of this AD was posted on 29 September 2010 as PAD 10-105 for consultation until 27 October 2010. No comments were received during the consultation period. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
easa_ad_2010_0228_R1.pdf (71 kb)
easa_pad_10_105.zip (323 kb)
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