Thanks for that. I perform underwater Ultrasonic Testing of ships hulls for a good time. Although I am not a metallurgist, and am merely a lowly technician, I understand the importance of procedures as it comes to performing NDT, and the problems you can run into when using the wrong procedures or tools to test the wrong materials.
The Visual Plus machine is perfectly capable of detecting sustained load cracking defects in 6351 cylinders. As 6061 cylinders are not subject to sustained load cracking, the test is worthless unless a manufacturing defect is present in the cylinder, one that was missed by the manufacturer.
But thanks for man'splaining NDE to me.
This is a bit of a rabbit hole, but lets stat down it, if only to clarify and add to people's understanding.
Sustain load cracking, is basically an inter-granular defect. Simply put, a weakness of the grain boundaries. In this case a mild load as normally encountered by day to day use of the cylinder can cause a defect to initiate. Generally in the threads and neck area but not exclusively so.
With a change of the alloy composition that weakness was eradicated, and thus the stresses and loads the materiel under goes in its daily life aren't enough to trigger a defect (because the material is stronger). But those stresses and loads are still there.
As you correctly pointed out, a defect and be triggered by having a weakness caused by a material defect (inclusions in the raw material) or an issue during manufacture not picked up by QA - normally this would be chemical or heat treatment, which would require the natural ageing of the materiel to become apparent.
Back to Eddy current. With aluminium, differing alloys have no real impact on the Eddy current inspection (EFD). As far as EDF goes, as long as it doesn't have a surface coating(clad or anodized) its pretty much the same. People don't EFD 6026 because it's unlikely it will crack - you're generally looking for corrosion or mechanical damage. If however you did inspect it and see a crack indication you'd be unwise to dismiss it.
When you get to Steel and its alloys, as far as EFD is concerned its a whole different ball game, because different materials, alloys and heat treatments all have a major impact. So an EFD procedure for one isn't' transferable on another. On the other hand as you well know, UT is - as long as you adjust for the slight differences in sound velocity and get a back wall echo (on compression wave) you're good to go
I am fairly sure that different materials are subject to different failure modes when subject to different stresses, such as neutron flux or heat. Austenitic Stainless Steel is subject to chloride stress corrosion, where inconel is subject to chloride pitting corrosion. Hint. The failure modes are different, and the methods for testing are also different.
But this isn't in anyway the same or comparable as finding defects in aluminium - yes I've written procedures for the nuclear industry (I enjoyed them as they were the most challenging)