Just for informational purposes, I should not have surprised anyone that 6351T6 aluminum alloys might be subject to sustained load cracking. Aluminum alloys with high silicon (SI) content (above 0.5%-0.7%) have always been known to be subject to SLC. 6351T6 alloy has almost 1% silicon. These alloys were widely used in aircraft construction, because of the good tensile strength and yield strength characteristics. Unfortunately, these same characteristics make them less than great for applications where a sustained load is exerted. Numerous aircraft accidents in the early 1965-1985 were thought to be caused by SLC with these alloys. Add to that the stress of cold thread cutting, and there might have been a pretty good idea that sustain loads might cause a problem at the cylinder neck area. They presumably continued to use this alloy because of the other very beneficial characteristics previously discussed.
Note: I am not a material engineer, so I could be wrong.
Phil Ellis
Note: I am not a material engineer, so I could be wrong.
Phil Ellis