Not sure why I feel compelled to even answer this, save for the fact that I think your line of thought is just completely off the tracks.
A2C wrote:
Conversely, you know what you know. In saying they "aren't usually looked at", he could be refering to people doing illegal paper sign-offs. (Certainly no one I know). You can't make sweeping generalities.
I'm making sweeping generalities? Hmmm. The article I attached was talking about de-riveting horizontal stabilizers and wing center sections. When was the last time an annual had that required as one of it's checks? I'm not saying that there aren't maintainers out there who pencil-whip maintenance, but that wasn't the point of my post or anybody else's post here -- YOU brought that up.
A2C wrote:
B.S. That can apply to any airplane.
You're right -- that can be applied to any airplane. But that makes the statement FAR from being BS...it makes it even MORE applicable to warbird aircraft.
A2C wrote:
Wrong. Why have B-52's been flying for 10's of thousands of hours and over 50 years w/o cracking? Fatigue cracking occurs in predictible and traceable and specific areas on the aircraft.
Interesting that you say categorically, "WRONG", and then go on to mention something completely un-related to warbirds. Unless, of course, you know about some B-52s that were made during WWII and are still operating that I am not aware of. Last time I checked the currently-flying B-52Hs were made in the 1960s.
I'm talking about airplanes made during WWII -- between, say, 1943 and 1945. A time when raw materials were not readily available. A time that, it's believed, precision in metallurgy was foregone because of the need to crank out airplanes. A time that corrosion control on interior surfaces was foregone because the manufacturer didn't think the airplanes would exist long enough for corrosion in those places to be an issue.
So, I'll entertain it when you say "wrong" so long as you can back it up with an educated discussion about metallurgy and corrosion control at US aircraft manufacturers in the mid 1940s.
A2C wrote:
Non-sense. An airplane can be flown to it's operating limits. If patterns of cracking or anything else emerge over the lifetime of the aircraft it can be taken care of w/ AD's.
This is probably one of the most ignorant and misguided statements I've read on WIX in a long time.
You are right -- in theory. So long as an airplane was built correctly, maintained correctly, and flown correctly. Those are things you just can't be sure of on many warbird aircraft.
Just how much time to do you have flying warbirds?