If I may enter the thread.
I should declare that I'm not nor never have been involved with scuba tanks, Don't know the full history without spending time reading detailed papers (rather than forum posts) But am an ex materials scientist and Course Director of NDT inspections within aerospace, Nationally and Internationally.
@Wookie is correct
The Sustained load cracking is an intergranular defect generally accepted to be cause by high pressure on the material over prolonged periods. The presence of lead as well as bismouth at the grain boundaries can accelerate this.
6351 Alloy had the most defects, even with the lead content reduced. To be clear while most defect have been found in the neck, there have been many in the shoulder as well as others found in the main cylinder area.
The defect is slow growing with a period of 8 or more years before it becomes critical.
Eddy current testing has been put up there as a way of detecting the defect. Unfortunately the equipment used is the equivalent of a "My first Eddy current tester", and I'm assuming the operator training is limited to a day or 2 just on that technique and nothing else? (Stand to be corrected)
What makes the inspection worthless, is that is a defect is found, the area is cleaned and inspected again. if a defect continues to be located then you confirm by visual aids to prevent false positives. That's a quote (roughly) from the operator guide.
Eddy Current Flaw detection (EFD) is an order of magnitude more sensitive that visual, it need no visual conformation if a correct technique is applied with proper equipment and a fully trained operator. EFD is designed to detect surface and subsurface defects (Find me a sub surface defect with the naked eye)
The fact that The EFD process and (I Presume the visual) was for the neck only when it's obvious that a defect can propagate anywhere in the material just scares me (as a materials scientist)
Given that a Ally tank is apporx 1/2 thick in the thinnest areas, I wouldn't' even used EDF - possibly Ultrasonic inspection (I've devised procedures to find minute defects in thick Ally components) but of course the investment in equipment and training doesn't make it worth it.
Visual inspection is open to interpretation as well as significantly under human influence (training, experience, the state of the person inspecting that day) Ideally in any inspection you should be able to miss a defect on 3 different inspection periods before it goes critical.
Stamping the cylinder (given the wall thickness) isn't going to have an effect unless you're king kong with a super size sledge hammer.
All that said, there is no proof that (yet) that's its a 6351 cylinder. Again as a professional I abhor the practice of "cave fills" and the like as you are eating in to the safety margin calculated for a new cylinder with zero defects. The safety margin has a tolerance to allow for material defects and the like. So if you continually stress a cylinder that was at the lower part of its tolerance bad things can happen.
I know people cite the number of fills vs the number of fails, but that citation doesn't help the person filling a tank when an accident happens by telling then it was a 1:1,000,000 incident.