EASA SIB 2009-13
WITHDRAWN - SEE FAA AD 2010-04-05
Summary
EASA Safety Information Bulletin SIB No. 2009-13 is an informational bulletin regarding the inspection of McCauley 1A103/TCM propeller hubs for cracking. It applies to all serial numbers of these propellers, commonly installed on Cessna 152/A152 and Reims Aviation F152/FA152 aircraft. The bulletin highlights findings of cracks near mounting bolt holes and references FAA AD 2003-12-05 and McCauley Service Bulletin ASB 221D for inspection and rework procedures.
What Changed
This bulletin informs operators of new crack findings in McCauley 1A103/TCM propeller hubs beyond those covered by the previous ASB 221C and FAA AD 2003-12-05. It introduces the use of McCauley ASB 221D as an approved Alternative Method of Compliance (AMOC) for the FAA AD. The FAA plans to issue a new AD that will supersede AD 2003-12-05, which EASA expects to adopt, leading to the withdrawal of this bulletin.
Why It Matters
This information is critical for aviation professionals to ensure the structural integrity of McCauley 1A103/TCM propellers, preventing potential failures due to cracking. Operators and maintenance organizations must be aware of the expanded scope of affected propellers and the updated inspection and repair guidance. Compliance with these recommendations helps maintain airworthiness and safety of affected aircraft.
What To Do
Owners and operators of aircraft equipped with McCauley 1A103/TCM propellers should inspect propeller hubs for cracks as described in McCauley ASB 221D. They should follow the rework procedures if cracks are found and monitor FAA and EASA communications for forthcoming mandatory AD actions. Copies of the ASB can be obtained from McCauley Propeller Systems for detailed instructions.
Your fleet's weekly compliance brief
AI-summarized regulatory changes, compliance deadlines, and action items — filtered to your aircraft, every Monday.
AI-generated summary from official EASA source document. Always verify against the original.