I was talking about over-boosting.
An over-boosted V-1710 or the Merlin will still be running at 3000 rpm; an over-boosted BMW 801 or R-2800-21 or -8W will still be running at 2700 rpm.
The Allison usually had an rpm override switch. Flip it up and the rpm went up by 200 for each switch movement. That switch is on every P-40 instrument panel.
So, if you are being chased by an opponent who is static or slightly gaining on you, most pilots would give the override switch a flick or two and go to 3,200 or 3,400 rpm to save their own lives. Since the Allison was designed for 4,000 rpm and limited to 3,000 by factory recommendation, the engine didn't suffer any harm at the higher rpm. I'm not too sure if the propellers were designed for 3,400 rpm and throwing a blade would certainly ruin the flight home. But both the Merlin and Allison could be turn to at least 3,600 rpm without suffering much if any actual engine damage.
The Merin was slightly more susceptible to rpm damage than the Allison, but not by much ... the Allison rods were stronger, but the Merlin's 2-stage supercharger guaranteed its place in history as a superb engine whereas the very few faults, all subsequently corrected, in the early Allisons virtually guaranteed their place in history as a bit flawed. In point of fact, the Merlin was usually first to a new power level, but the Allison was right behind and, by the end of the war, there was little to choose, power-wise, between them. Just to set the record straight, Merlin rods are perfectly good at stock power levels and don't start failing until 2,400 hp or so. Allison rods are good for 3,600 hp+. Neither engine made those kinds of power in military service, so either set of rods was good for WWII combat flight.
Unfortunately, right when the Allison was starting to produce 2,100 hp+ on test stands, the customer was throwing money at jet engines and not at new piston engine development, so these powerhouses never flew much less got produced in any numbers. The best of the Allisons were one-off test stand mules. Such is history anyway. I don't think any stock Allison made more than about 1,750 hp in service, and those were in P-63s that didn't get into combat in U.S. service.
You could get 1,700 hp from a V-1710-99 (P-40N), but not at 57" and 3,000 rpm. You needed 75" and 3,200/3,400 rpm to get the power. That WAS done in service, just not widely and generally not with "permission" from the unit. I've spoken with 3 - 4 people who said they pushed wartime P-40s that hard when the chips were on the line. They all said other people did it, too, when it was indicated. A light P-40 pushed that hard climbed pretty well at 170 mph, according to people who were there and did it.
Edit:
Also according to owners, one engine you can't increase rpm on much is the Bristol Centaurus. It is very reliable at stock power and rpm levels. You CAN increase boost, but as little as 200 rpm increase can precipitate a failure. It can make more power, but not by turning it faster ... just by increasing boost.
The Wright R-3350 can spin faster and do OK, but these are later, post-WWII R-3350s, not the engines that were flying in WWII, which were NOT very reliable when pushed. Heck, they weren't all THAT reliable when operated in cruise!
The R-2800 can do all sorts of crazy boosting and run just fine. But, again, it depends on the R-2800 engine series. Later engines were better than earlier ones, and the 2,800 hp version was never all that reliable when pushed to 2,800 hp. But 2,500 hp? All day long, no problem! ... as long as you watch the temps.