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Friedrich Ostertag wrote:
Neil Gould wrote: Recently, Friedrich Ostertag posted: Karl-Heinz Kuenzel wrote: Hi. Here in Germany we had an accident with a brand new DA 42 in Speyer (EDRY) on 3-4-07 during take off. It seems, that the battery was down and both engine were started with remote power. After take off when retracting the gear, the props feathered and both engines stopped. You can read about that accident in German (sorry) in www.pilotundflugzeug.de First hearing about that accident and the background, I could not believe it. I don't even know where to start. How can an aircraft, that depends on electrical power for the operation of it's engines, be airworthy without fully redundant electrical systems? While in this particular case the pilot might have noticed the problem, had he meticuously follow procedures and started the second engine at the plane's own power, it is quite easy to find failure modes that would go unnoticed inflight, yet cause double engine failure at the instant the gear is lowered on final. Lead batteries are known to occasionally go flat suddenly, once the buildup of oxide makes contact between the lead elements. Happened to me in the car once. The engine (a diesel with mechanical injection pump) ran happily without me even noticing the failure until I shut it down. When I turned the power back on again, not even the lights in the dashboard would light up, it was completely and utterly dead. I would never have thought that they cut corners like that at Diamond. I Hope this will not create a lot of mistrust in aerodiesels, as it is not a diesel issue. I guess you could call it a FADEC issue if you wanted, however it really is an issue of redundancy of essential systems, and easily solveable as such. I have a somewhat different take on this event. It appears to me that the pilot didn't sufficiently understand his aircraft or the implications of the symptoms he observed. Knowing that there was insufficient power to start the engines, that the engine & prop controls were dependent on electric power and that the landing gear used an electric motor would have stopped me from taking off until the battery/electrical system problem was addressed. Well said, and I wouldn't disagree. However, the very same potentially deadly failure could occur anytime the battery fails inflight, with no way for the pilot to know about it before he actually hits the button to lower the gear. That alone appears to me to be a major design flaw that would make me pretty uncomfortable, batteries are known to fail suddenly sometimes. I really would expect redundancy in something as critical as the power supply for the fadec to be a requirement for airworthyness. Why have two sets of magnetos on the typical SI-engine? It's just an electrical system, too... Why have a twin engined aircraft? I don't find it surprising that the props feathered in this situation, and would even say that it would be the expected behavior, rather than a fluke of some kind. If you are saying that a shut-down is to be expected when the power supply on a fadec controlled engine fails, you are right. No modern engine will continue running without electrical power. Even on a diesel with common rail fuel supply (as the thielert is) without electricity no fuel injection is possible. regards, Friedrich This is a cut and paste from a AOPA story on the plane There are three batteries. The main battery is a 24-volt 10-amp-hour size. Electrical power is provided by two 24-volt 60-amp alternators — one on each engine. There also is a 24-volt 1.3-amp-hour alternator-excitation battery to provide alternator start-up (excitation) voltage if the main battery is discharged below the required excitation threshold. The third battery is a stand-alone emergency battery that powers the electric artificial horizon and an instrument floodlight for one and a half hours. The question then become if there are 2 60AMP alternators and a single 10AMP-hour battery how could the battery being dead cause the issue. I think there is much more here then meets the eye. Perhaps we should wait for more data before we jump to conclusions. |
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