From time to time, in one chart or another, the data gets updated.
For instance, between Mil-Hdbk-5H and AR-MMPDS-01, the allowable shear strength of a MS20470AD4 rivet went from 388 pounds to 389 pounds.
For some, this earth-shattering news may go over with a whimpering "so what"?
For others, such as folks who have to read old stress reports and wonder "where the heck did that number come from", we have to go back to the old book that was used back in the day, and discover that the allowables for common materials were a little different. Watching the evolution of the documents, it's been interesting to see some things "disappear" as the years go by.
Finding a copy of Mil-Hdbk-5 before revision H is bound to be difficult, because before that time, very few documents were scanned or published electronically for distribution. Because it was the '90s.
I started working on aircraft using Mil-Hdbk-5E, on paper of course, and didn't start referring to an electronic copy until after getting the PDF at "J". So I don't have a PDF that goes that far back either. Sorry.
If you find an engineering office with a paper copy in the library, maybe you can buy it, borrow it, or scan it, otherwise you'll have to cough up the cash for IHS.
STF