Thanks.
I spent much of the evening yesterday reading old logbook entries - many of them written in scribble. But, it was more enjoyable than episode 32 of: "Who's worse, the Bears, Lions, Packers, or Vikings?" I found a few pertinent 337s, along with some drawings and letters from Piper, so I guess that answers my questions as to the A-65-8, shock struts and 1150 lbs. gross weight.
So the papers that say PA-15 are likely correct and those that say -17 likely in error. Plus, the moment on the computed W&B has been 52-1/2 low for most of the airplane's life. That's 0.05" at gross!!!
PS: I love the cryptic quality of some of the old paperwork. It was obviously written by people who knew what they were doing and didn't feel a need to go into too much boring detail.
PPS: Someone on the SWP blog sent me a pic of his data plate. The "15" and last "0" of 800 had been "X"d over with "17" and "5" being new-ish-ly stamped. But his s/n was still 15-something.