Since I have too much spare time on my hands I will relate a story about engine wear.
I had a professor in college (mechanical engineering class) who had worked for Rolls Royce Aero Engines.
He told the story about Rolls Royce Merlin Engines (12 cylinder 27 liter 1000 plus hp) used in the Spitfire during
World War II.
To expand capacity, during the war, these engines were also built under license by Packard in the US.
I gather aircraft engines typically get maintenance based on flying hours.
Engines, both UK assembled and US assembled, would undergo maintenance at the same prescribed number of flying hours.
What was seen when the engines were disassembled and inspected was far more wear, "failure" and replacement components needed in the US engines than the UK engines.
Keep in mind the engines were all built to the same specifications and using identical engineering drawings.
The increased wear factor caused concern so the issue was investigated.
The cause was identified as follows:
All components were designed with the requisite engineering tolerances, so as an example the engine block cylinder bore could be plus or minus 10 thou' - similarly a piston could be plus or minus 10 thou'.
The UK Rolls Royce assemblers had an
unwritten work practice of selecting components that essentially "blue printed" the engine - so for example they would measure the cylinder bore and select and optimize a piston for that cylinder. This had the effect of minimizing assembly tolerances resulting in less engine wear for given hours of flight,
The US assemblers simply assembled an engine with whatever required components were at hand. No one ever told them to selectively choose components to minimize wear.
Interesting story, at the time, for a budding engineer wet behind the ears
