PPRuNe Forums - View Single Post - New Cylinder AD's released by FAA
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Old 20th Apr 2014, 22:21
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OZBUSDRIVER
 
Join Date: Dec 2001
Location: YMML
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Interesting problem. Notwithstanding obvious issues of dissimilar metal expansion rates....why would there be changes in metallurgy of a proven process?...and the robustness of a "screw" fit at the junction of head and barrel...why would this assy separate?

Jaba, are there any further clues? Corrosion? Fretting? Stress risers?
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