There was a similar engine failure in Australia with a Rotax 912S that ended much differently with 2 fatalities. There was no obstruction in the field where they TL Sting 2000 tried to land, but the pilot stalled it and crashed.
The Australia Transport Saftey (their FAA) has a written report with pictures. I have the report on a PDF format, but I can't figure out how to post it here.
Well Done, and nice landing BTW.
I love the story a good friend tells once in a while. He had I think over 800 hrs of glider time when he decided to get his power rating. During the check ride the examiner pulled the throttle to simulate a power failure. He of course easily set up for an emergency landing in a field. The examiner commented on how he noticed that my friend relaxed when the power was pulled. He also commented on how well he set up and was really prepared to land in the field. It was at this point my friend pointed out the examiner. "See that line down the middle of the field we are lined up on, That is the wheel track from where I landed my glider last week"<snip>
One of the things that had me the most scared at first when the engine quit and wouldn't restart was the thought that I had only one chance to make a safe landing and I had better not screw it up. After a couple of seconds, it occurred to me that I had done more than forty such landings already without problems. That realization was a HUGE instant confidence boost for me.
I was initially surprised at the slightly different handling of the aircraft with the propeller completely stopped. Aircraft handle differently with the engine dead than they do with the engine at idle. They handle a lot like gliders-imagine that!!.
<snip>
Drastic consequences for such a simple mistake. I presume that it was at an oil change and that just adding a quart of the wrong viscosity wouldn't cause this.I have been told that the wrong viscosity oil was used in the engine, causing oil starvation.
I never thought I should have to sample and check the viscosity of the oil as part of my preflight inspection.
I still don't know why the electrical system failed. I doubt I ever will. That is going to drive me nuts!
The piston rod separated and broke through the crankcase. There was a fifty-cent piece sized hole with the rod poking through. The engine is going to be removed from the plane and sent back to Rotax.
A Rotax doesn't use aircraft oil. Maybe the problem was aircraft oil was used instead of the specified oil? I'm thinking that too high a viscosity oil is a bad thing, a really bad thing since clearances are designed for a specific oil. Basically the bearings would not be receiving the design oil flow and the oil pressure gauge would be reading top of the green (basically at the pressure limit valve opening pressure) even after warm up.
It's a bad sign if oil temperature is high and oil pressure is max...
I would be surprised if you could tell the difference in viscosity between the commonly found aircraft oils just by inspection.
I would be surprised if the difference in viscosity between commonly found aircraft oils would take out a rod bearing.
If the end of the rod punctured the wire to the alternator it would have created a massive short that could have taken out quite a bit of your electrical system.
If the engine needs a low-viscosity oil but gets a high-vis, oil pressure can fall because the oil pump can't suck it up fast enough. It cavitates instead.
Dan