Pat wrote:
Airnutz-
To be honest with you, I can't tell you how difficult it would be to R&R a cylinder liner; I've never laid a wrench on an Allison; most of my experience has been with heavy commercial turbine aircraft, with the exception of working on a B-17G infrequently in the past.
According to "Vee's for Victory" (published by Schiffer), a GREAT book on the subject, the liners were installed with an interference shrink fit. The compression nuts on each sleeve were torqued to 2,100 pound-feet.

I doubt they could be easily removed without special tooling.
-Pat
Ahhh, thanks Pat. After my post I continued looking at their photos and found the
answer to my question. In the photo I linked you to, it appeared as if they
were individual cylinder/cooling jacket assemblies bolted to the cylinder head
and then lowered down onto the engine block. Such is not the case inthis photo looking above the wasted piston/liner combo..
www.missthriftway.com/Photos/engine/OOPS.jpg
It wasn't really clear(to me), in Bill G's original explanation, but your detail from the book
and the photo cleared up the answer. Not an easy field fix.
It's been ages since I've seen a blow-up schematic of the Allison and this has
been entertaining and informative. Thanks all!!!
The W-24 from "Yancy Too" was a nice surprise...I'd like to see more of that
project.
Thanks again Pat!