Not sure where you got the last sentence.
It has a lot to do with the fact that it took 5 engines to get through the 150 hour test for the V-1710-33 engine during the summer of 1940.
A lot of this was NOT the fault of Allison.
Details are scattered in different parts of "Vee's for Victory"
One of the problems was the change in rating from 1040hp at 14,300ft to 1090hp at 13,200ft at the insistence of the AAF.
As a result of an accelerated service test that was completed July 17th 1940 by 7 planes and 5 of them completed 150 hours. They had one failed crankshaft (a fault with that individual unit) and one cracked nose case.
At as result of this test and problems with the ongoing test stand problems the engines were rated at 950hp for US use at this time.
Some of the engines used for type testing in 1937 and later used different supercharger gears and made their 1000 or 1150 hp at sea level or very low altitudes, They were intended for turbo charged YP-37, Bell FM-1s and the XP-38.
Many or all of the early engines used magnesium intake manifolds (all the British C-33s got magnesium intake manifolds but the British used a different valve clearance).
Vee's for Victory chronicles' the tests of the 5 engines for the -33 type tests. It takes almost 2 pages in the book. Pages 238 and 239. First attempt was 8-11-39 to 8-12-39 and lasted 10 hours. ( a rag had been left in the oil system) several of the engines were rebuilt and tried again but it took the test (#7?) started on August 15th 1940 make the 150 hour mark.
Allison had to take back 228 engines and rebuild them (16 were still outstanding as of March 31 1941 but they were completed shortly after).
The engines in US service in the summer and early fall of 1940 were being operated at
Take-off...................950hp at 2770rpm
Military....................950hp at 2770rpm at 8,000ft
Normal....................838hp at 2600rpm at 8,000ft
Once the engines were repaired/upgraded they were rated at 1040hp for both take-off and at 14,300ft and 930hp at 2600rpm to 12,800ft.
There were changes in intake manifolds and a few other details over the winter.
But that appears to have been the situation in Aug-Sept of 1940.
Allison made many small improvements during these tests and again, a faulty test cell mounting that did not duplicate the mountings of the service aircraft caused some of the crankcase cracking problems (and cracked crankcases can lead to other failures).
British experience was just about 100% after these troubles even though the most or all of their engines did not have all the upgrades. They did have proper engine mounts, they used different valve clearance (they were also different fuel) and since the Melrin engine was tested at over 100 hours they didn't expect the -33 Allisons to last as long as the Americans did anyway. Now throw in that much of the British early P-40 use was in the dessert and engine life (anybody's) wasn't that good anyway?
Allison was making the 1150hp -39 and -35 engines by the late spring/early summer of 1941 anyway.
This was just a blip on the History of the Allison engine and in no way relates to the ability of the engine at a later date or any other version. It does happen to coincide with efforts to get an American manufacturer for the Merlin in the summer of 1940.