Some other findings: The SD40-2's in the consist were equipped with an Auto-Start Feature that would've brought a unit online when the air pressure dropped too low. However, they were electrically isolated by the engineer, so the Auto Start wound up being disabled...
There were Reset Safety Controls (alerters?) in the GE's which were retrofitted by a previous owner. The wiring on each was different, and the 5017's was wired directly to the battery. The RSC's were supposed to activate a penalty brake application once the circuit breakers were thrown, but this did not happen due to the wiring configuration on the lead unit, which was provided w/power as long as the battery still had charge. According to the TSB, there was no *requirement* to test the RSC to determine if a penalty application would happen when the breakers were opened. I *suppose* this is because the engineer wouldn't normally take the lead unit off-line if it was the only operating unit in a consist....
The cause of the engine failure and fire on 5017 was traced to a 'non-standard' repair of the boss for one of the cam bearings in Oct. 2012. An epoxy-type material was used to build up a damaged area of the boss (approximately 45 degrees of arc), rather than welding or other repair methods. The bearing is an annular ring and when tightened, the "repaired" area did not have enough compressive strength, so it leaked oil. This led to it being tightened further (in the Derby shop on 15 March 2013), which applied unequal stress on the cam bearing, which affected the lubrication to the adjacent cylinder's valve train. Once the cam bearing failed, a valve broke, dropped into the bore and holed the piston, which allowed engine oil to be propelled into the exhaust system and turbo housing. This was what caused the fire, approximately 10 minutes after the engineer left the scene. (pp30-31 of TSB Report).