Already 2 pages long & no one have asked for the DAT log yet? The mobile device DAT log ending with FLY031.DAT will clearly show every detail in this, retrieve it and attach it here, then we certainly will be able to tell the reasons for this AC to loose thrust from the front left side. The accelerometer sensor readings there can say if anything hit the AC before loosing thrust, the motor rpm's & motor currents will let us know if it was a prop or a motor failure.
That it was a lost thrust issue is pretty clear & straight forward ... the incident started at 501,3sec.
-Just before the incident moment, the elevator stick was just released from full ... making the pitch in the chart (Green graph) to go heavily positive for breaking.
-During the breaking the OP applied max negative throttle to descend (Light bluish graph)... It's this that starts the initial height loss.
-Meanwhile breaking & commanding loosing height the OP uses a larger command with the rudder stick (Purple graph) to rotate negative (CCW).
-But at 501,3sec ... still applying both throttle & rudder sticks, the AC pitches down (Green) & rolls left (Blue) heavily & abrupt ... the tilt angle (Red) goes in an instant from 33 degrees (about max according to the spec.) to 73 degrees.
All this gives a very strong indication of a failure in the front left corner ...
The discussed message below, comes 2sec after the incident have started ... so it's irrelevant to the incident.
With all this said ... we still can't say for sure if it was a motor or a prop that failed. With a front left corner failing the AC should start to rotate CW (Darker green graph) ... but it doesn't, it continues to rotate CCW (negative) as per the commanded rudder input there. At 501,7sec we see the first CW twitch ... after that we get a more of a oscillation than a rotation. This can be due to a partly damaged prop or a motor that rotates but slowly seizes together. The mobile device DAT log is needed to be able to tell ...