Here is one for yourr light reading - names are A and B to protect the incompetent. Kinda like an internal VFD problem.
3 phase high speed motor drives for a space launch vehicle, drives powered the re-entry control surfaces. Kinda narrows down the companies, eh?
Made and designed by company A , 3 delivered and functioned fine, 2 space flight completed successfully.
4th and 5th units burned up on extensive thermal/vacuum/operational tests.
After 3rd unit, Company A bought by company B on east coast. Hot shot QC guys from B visit A and proclaim some wires are routed incorrectly, insist on changes for units 4 and on.
Units 4 and 5 fail.
Unit 4 wired up to 15 each Tek windows based 4 channel scopes, 2 weeks of looking at waveforms, at least 12 engineers involved. .
Hotshot reroute of wires added 5 nH to inductance (yes, nano, E-9) which resulted when PWM signals turned off motor drive FET the L*di/dt caused an internal current in IR2113 full bridge drivers to burn open an internal trace.
Fix was to change timing to avoid the di/dt. Note not nmentioned befroe was that company A had psent alot of time for the originalwire routing to avoid that scenario, but the company B 'hotshots' insisted and had authority to insist on change. Cost company B a few hundred K to find the problem and implement solution. NASA, company C vehicle contractor, and others involved.
Never have heard if the 'hotshots' got their next pay raise, hah.