Engine failure during flight

[Martin_1970]

Hello,

i was on a flight from BGBW -> CYYR, as my new engine (total about 6.0hrs) failed at 26.000ft. I could do an emergency landing :) and looked in the log file

2018-11-03 16:44:44 TBM900[fail.c:931]: Component compressor has failed due to excessive wear (worn: 0.165200%, slope 1.0, rate: 0.000%/s). You can prevent this by observing performance limitations and servicing the aircraft regularly in the maintenance hangar.
2018-11-03 16:44:44 TBM900[fail.c:934]: Failure impact: tbm900/failures/engine/comp_stall
2018-11-03 16:45:03 TBM900[fail.c:931]: Component compressor has failed due to excessive wear (worn: 4.682590%, slope 0.0, rate: 0.208%/s). You can prevent this by observing performance limitations and servicing the aircraft regularly in the maintenance hangar.
2018-11-03 16:45:03 TBM900[fail.c:934]: Failure impact: sim/operation/failures/rel_seize_0
2018-11-03 16:45:06 TBM900[fail.c:931]: Component turbines has failed due to excessive wear (worn: 100.000000%, slope 0.5, rate: 0.555%/s). You can prevent this by observing performance limitations and servicing the aircraft regularly in the maintenance hangar.
2018-11-03 16:45:06 TBM900[fail.c:934]: Failure impact: sim/operation/failures/rel_hunsta0
2018-11-03 16:45:06 TBM900[fail.c:934]: Failure impact: sim/operation/failures/rel_engfir0

Before everybody says: Don´t exceed the limits...  I was flying in 26.000Ft, Torque about 80-85%, N1 99%,  ITT i dont remember but far away from limits. Everything stable for more than 1,5h´s of flight.

I am wondering about the first defect entry in the log: excessive wear with 0.17% ???

What else could cause such an engine failure, even everything was inside the limits and checked before start ("as new")??

Or is there a random "increase blood pressure of the pilot" function implemented , or maybe a bug in the calculation?

 

 

[Goofy]

Before each flight, it is necessary to go into the maintenance management system and check if there are any items to repair or change....
Wear is implemented in this TBM 900 and there is even a checkbox that speeds up this phenomenon.

[Martin_1970]

Yes, before start everything was "as new", and the accellerated wear option was not selected.

Thats the reason i wonder about the sudden engine failure in flight.

[sdflyer]

I had a similar experience I posted in 1.0.9 update thread. My TBM was newly created per update instruction . 

[N602AC]

I've had numerous cases of this type of thing happening. Take a look for the other threads I've created about it. The worst one was when the fuel nozzles got considered as clogged with less than 1 percent of wear, causing a flameout in flight, and restart attempts were not successful. After that I had to make a deadstick landing at the nearest field. I guess it wasn't fixed in 1.0.9 after all then....?