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Malta, where Coral dust was so prevalent, it wouldn't make TBO and would be overhaul based on condition rather than overhaul hours.
Very interestingAre those manuals available for download?
EKB raised the whole "Merlin is so-o-o unreliable vs the Allison" schtick;
it's up to EKB to support his own convictions with more than just meaningless, bald statements.
I suggest EKB read Harvey-Bailey, pages 40-45 to find out. The isolated troubles of the Griffon on some Seafires have nothing to do with the Allison V-1710.
The introduction of the Merlin Mustang was a new thing for the 8th AF, with Packard just begining the production of 2-stage V1650s in Spring 1943. As a new outift, it will come with more or less a number of issues. That was true for P-47 (P-47B was unfit for war, the engine problems persisted until mid-1943 with P-47C and D, again engine problems with M), F4U (both engine and airframe, not just for carrier service), P-38 (host of the problems with engines' installation, most notably in the P-38J, insufficient heating prior spring of 1944 when installation of second generator allowed for a redesign of the cockpit heating sytem). P-40 in 1941 with restricted engine power.
Basically everytime the design, either airframe or engine or both, was pushing forwar it encountered issues, some designs (and the design staff) being better in overcoming the issues than another. The fact still stand that Merlin Mustang ranged far and wide against German and other Axis targets, with the unprecedented range and performance - just what and when was needed, even if we account the P-38 history. This, added to the wordwide use of the Merlin will still mean plenty for anyone.
If we talk post-war pistons, let's recall that V-1710 powered P-82 were never as reliable nor as performing as V-1650 powered P-82s.
You need to show us when Mustangs with the Allison engine suffered this many problems:
To make an accurate comparison you need to show us when that many Allison Mustangs were being fielded under the same conditions.
I would guess they would have had the same issues.
The real determination of aircraft reliability considers the number of aircraft assigned to a squadron, minus those grounded for routine maintenance.
A large number of the problems you list were not with the V1650 engine (Its not a Merlin) but with the plane and ancillaries. These were new planes to the unit the ground boys were inexperienced on the new type. Go look at any Unit history covering the period after the changeover between types and you will find the same thing. Go look at any unit logs when the unit had used the new P51 in combat for 6 months and compare.
This thread was about someone asking genuine questions about why the Allison didnt seem to get the fame that other engine types got. You are simply trying to knock down an engine because of its fame and mythology, what people say and think now has no bearing on 70 years ago.
The Merlin/V1650 engines might have had more problems than a V1710 but ask yourself this question would you want to take on the Luftwaffe in their backyard at 30,000ft in a P51 B,C,D or K powered by a 1943 V1710 with a 2 speed 1 stage non Turbo blower or a V1650 with 2 speed intercooled 2 stage blower. You cant say "ahh but the V1710**** series ran on the stand in 1945 for 10 million hours and gave 3,000hp at 50,000ft and had freakin laser beams on the cam boxes" its between a V1650-3 or its May 1943 Allison equivalent.
Oh and by the way yes the Merlin/V1650 is my favourite engine of all time but I am not blind to its many flaws and unsuitability for passenger air use. I dont have a 2nd favourite but a group of engines which I regard as exceptional but just not Merlin/V1650s and in that group of 6 is the V1710.