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![]() "Cary" wrote in message oups.com... The problem, as I understand it, was the battery was dead. According to the POH, the battery is used to start the engine and is used as a backup during flight for all the electronic gear (including the FADEC). Although the investigation is still ongoing and other answers may be forthcoming, when they operated the landing gear they exceded the power available from the alternators and the backup system (the battery) was not available so the FADEC (engine computers) stopped. One of the lessons here is that one should not fly an airplane that relies on electricity if you don't have a battery to run the electricity! Cary On Apr 23, 4:35 pm, wrote: Gig 601XL Builder wrDOTgiaconaATsuddenlink.net wrote: Neil Gould wrote: A simple voltmeter with a "red line" should suffice, along with a caution; "Don't take off with the needle outside the green arc". Of course, that won't prevent someone from insisting on making a bad decision. I again agree but if you are going to have an sytem with FADEC it ought to have the authority to to clearly tell you that it is about to use its' authority to shut the engine off. From the description it sounds more like the FADEC didn't have the authority (or power) to do anything. More to the point, if all the power goes away, what happens to all the "settings" the FADEC controls? Do they go to zero, full, stay where they are? It appears that they go to zero, which is a damn unhandy failure mode. -- Jim Pennino Remove .spam.sux to reply. Even if the battery worked fine, something that causes damage, even something as small as a bird strike can cause a short; dropping voltage, and shutting down the engines, plural. Wouldn't a relay that isolated the engine when the buss voltage dropped to zero have helped? Surely some prioritizing is in order. Al G |
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