Airworthiness Directives; McCauley Propeller Systems 1A103/TCM Series Propellers
airworthiness · Rule · Final rule; request for comments. · Published 2010-02-23 · Effective 2010-03-10 · 75 FR 7934
Document
Document number
2010-3113
Federal Register citation
75 FR 7934
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
McCauley
Publication date
2010-02-23
Effective date
2010-03-10
FAA docket
Docket No. FAA-2010-0093
Abstract
The FAA is superseding an existing airworthiness directive (AD) for McCauley Propeller Systems 1A103/TCM series propellers. That AD requires, for certain serial numbers (S/Ns) of McCauley Propeller Systems 1A103/TCM series propellers, initial and repetitive visual and dye penetrant inspections for cracks in the propeller hub, replacement of propellers with cracks that do not meet acceptable limits, and rework of propellers with cracks that meet acceptable limits. This AD requires, for all McCauley Propeller Systems 1A103/TCM series propellers, the same actions but at reduced compliance times. This AD also requires inspections of the bolt holes, reaming holes if necessary, and inspections of steel reinforcement plates and gaskets. This AD results from 16 reports received of propeller hubs found cracked since AD 2003-12-05 was issued. We are issuing this AD to prevent propeller separation due to hub fatigue cracking, which can result in loss of control of the airplane.