They said they just were more comfortable with more margin. The stress group was an independent organization to avoid conflicts of interest with the design group. Our job was to design, their job was to verify. If parts broke, they got the black eye. If the airplane was overweight, design got the black eye. We both had to agree, and it was a system that worked well.
Most design engineers didn't work out the stresses themselves, they just hoped to pass the stress group. It was pass/fail for them. In my not so humble opinion, they were making overweight parts. I was interested in using math to sculpt perfect parts :-)
For example, the inside diameter of the jackscrew was specified to the ten-thousandth of an inch, something like 2.1834..2.2096. So I'd get the "why not make it a nice round 2.19..2.20?" I'd reply because if it came in at 2.205, it would get rejected, even though it was perfectly usable. And I got my way, because the jackscrew forging was a very, very expensive part and rejecting a usable part did not make anyone happy.
(Rejected expensive parts often got bounced back to engineering to find a way to salvage them. I just was doing the math in advance so they wouldn't have to.)