the post quoting R-2800 procedures shows turning starter-on ignition-off was used as a check on hydraulic lock (due to any pooling engine-off)
presumably oil scavenge layout was arranged out to prevent pooling in running
http://www.airliners.net/forum/viewtopic.php?t=761365
http://forum.keypublishing.com/showthre ... il-systems
this includes mention of kits for recirculating oil from low cylinders
http://www.pprune.org/archive/index.php/t-257627.html
btw some might learn from the incidental examples of 3000-4000 hr TBO (TBO the actual on-condition figure not the 'book' figure that now gets quoted)
an airforce (regulator-exempt of course) wanting to keep engines can do a lot, an airline that wants new engines or aircraft can do the opposite
and this (post by Walter Atkinson)http://www.pprune.org/archive/index.php/t-533489.html
elsewhere a poster says his employers ordered QECs (quick engine change ?) when plugs needed renewal on 28 cyl R 4360s
and some Centaurus photos
http://www.practicalmachinist.com/vb/an ... =centaurus