Another Caravan engine failure

Should be second nature. I dunno, maybe it's my background, but I feel strongly anyone sitting in the seat should know that intuitively and natively.

Pretty simple to comprehend: Stalled starter motor = LOTS of current.

The consequences of a catastrophic turbine failure were never covered in ground school when I was there.
 
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So much for the PT-6 being bullet proof. Sorry but I'd take a 402/404 any day over a single engine, turbine or not.
 
Because, if you are flying along, and hear the engine grenade (which they seem to be doing with increasing frequency) which generally means the gas generator has locked solid. Hitting the starter at point will be like shorting out the battery. You stand to heat (red hot) any of those heavy duty cables that run between the battery, solenoids, and starter. So now you have a nice burning smell to accompany you in your glide. If the engine puked oil, you stand a moderate chance of lighting that off as well. To say nothing of losing your battery, and thus nav/com. Other than that, yeah, no problem. :)

Now, if it is showing any Ng, then go for it, you have little to lose. If it went out with a bang, and Ng went right to zero, you have a lot more to lose. An engine that has not locked will show 5% or more in the glide.
Not necessarily. Could be a compressor stall causing a flame-out, those are really loud, or any number of other things. If I was a boss (haha!) and a pilot who had an engine failure and had plenty of time to attempt a restart told me that he didn't attempt a restart because it probably wouldn't work anyway I think I would slap him in the back of the head.

Also, energizing the starter generator on a locked gas generator section would shortly fry out the generator due to heat, but I do not think any fire would occur. At least not in the cables. It isn't like shorting the battery at all. Those cables can handle a thousand amps easy, and you'll never get more than 500 or so from the battery.
 
So much for the PT-6 being bullet proof. Sorry but I'd take a 402/404 any day over a single engine, turbine or not.

# of fatalities due to an engine failure in a TP single in the past 5 years = 1

# of fatalities due to an engine failure in a ME piston in the past 5 years = a lot more than that


Every day a 747 worth of people are killed driving in cars, but it never makes the news. But, if an airliner makes a precautionary landing it's covered live.
 
Not necessarily. Could be a compressor stall causing a flame-out, those are really loud, or any number of other things. If I was a boss (haha!) and a pilot who had an engine failure and had plenty of time to attempt a restart told me that he didn't attempt a restart because it probably wouldn't work anyway I think I would slap him in the back of the head.

Also, energizing the starter generator on a locked gas generator section would shortly fry out the generator due to heat, but I do not think any fire would occur. At least not in the cables. It isn't like shorting the battery at all. Those cables can handle a thousand amps easy, and you'll never get more than 500 or so from the battery.

Remember, I said in the beginning, if the NG was indicating 0. A loud noise, an engine destructing itself, is a very obvious sequence of events. You would be ill advised to try a restart on an engine that you knew was physically no longer an engine. It would serve no purpose, is a fire hazard, it could possibly deplete your electrical system (Hey! Want flaps at the end of the glide? What if it was IFR? Still would be nice to keep the radios. If the system voltage dropped low enough, you would have to go through the re-boot sequence again), and maybe wasting time you could have been using figuring something else out.
 
I'm not sure how much of a "re-boot" there is on a Caravan. Plus, it certainly appeared to be VMC from what I could tell. My sense of these things is that I'm going to do what's on the checklist. IMS, ours says something like "If ng < whatever, depress starter button". Yes sir!

Edit: With that said, if it were a King Air (God forbid) and I wasn't in the mountains (God forbid), I can see the argument for thinking twice, but I have zero hours in gliders, and I'm not interested in learning on the job.
 
Lets try and think through all that in the heat of the moment.
"eff it, we're cranking."

SpiraMirabilis beat me to it, a compressor stall has a more than superficial resemblance to a "loud bang."


So much for the PT-6 being bullet proof. Sorry but I'd take a 402/404 any day over a single engine, turbine or not.
Errr...
# of fatalities due to an engine failure in a TP single in the past 5 years = 1

# of fatalities due to an engine failure in a ME piston in the past 5 years = a lot more than that
Affirmative. Granted most of those aren't necessarily the airplane's fault, but unless it's a transport category twin, you aren't guaranteed to survive canning one at rotation.

I'll take a single PT 6.

But what do I know! :)
You love the smell of jet fuel in the morning, don't lie. Plus the growl.
 
Statistically, you're a lot more likely to "fly to the scene of the accident" in a multi piston with one caged than have a turbine stop in the first place. Plus, a fair number of engine failures (not this one, obviously), come from feeding the engine either nothing or stuff it can't burn, which would presumably affect any number of piston engines in just the same way as a turbine.

Now, with that said, do I feel a bit of "whistling past the graveyard" when flying a turbine single at night in low IMC? Guilty. Which is pretty funny, because I don't think I had a care in the world when I used to do it in a PISTON single with like 20,000 hours on the clock. I guess it's all a matter of Perspective. ;)
 
So much for the PT-6 being bullet proof. Sorry but I'd take a 402/404 any day over a single engine, turbine or not.

Really? Single engine performance on a 402 may not be enough to make it back to the airport, then the airplane hits the ground at some speed higher than redline (if you're still in control at all). The Caravan stalls at something like 50 KIAS. I'd prefer that.

PT6 is supposed to have a failure once every 100,000hrs or something like that. Pistons are supposedly twice as much.
 
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Really? Single engine performance on a 402 may not be enough to make it back to the airport, then the airplane hits the ground at some speed higher than redline (if you're still in control at all). The Caravan stalls at something like 50 KIAS. I'd prefer that.

PT6 is supposed to have a failure once every 100,000hrs or something like that. Pistons are supposedly twice as much.
Clyde Cessna once stated of one of the high wing designs built in Independence, "It's just fast enough to kill you." Pertinent.

Statistically, you're a lot more likely to "fly to the scene of the accident" in a multi piston with one caged than have a turbine stop in the first place. Plus, a fair number of engine failures (not this one, obviously), come from feeding the engine either nothing or stuff it can't burn, which would presumably affect any number of piston engines in just the same way as a turbine.

Now, with that said, do I feel a bit of "whistling past the graveyard" when flying a turbine single at night in low IMC? Guilty. Which is pretty funny, because I don't think I had a care in the world when I used to do it in a PISTON single with like 20,000 hours on the clock. I guess it's all a matter of Perspective. ;)
As someone who flies a light twin for fun, the content in this article often hangs around in the back of my mind.
 
Why does it seem like the Caravan has a much higher engine failure rate than the PC-12 or TBM?

Side note, more people have been killed in King Air's post engine failure than the in the PC-12. In fact, there have been ZERO fatalities in a PC-12 after an engine failure.
 
Why does it seem like the Caravan has a much higher engine failure rate than the PC-12 or TBM?

Side note, more people have been killed in King Air's post engine failure than the in the PC-12. In fact, there have been ZERO fatalities in a PC-12 after an engine failure.
I think utilization rates for the first question. More of them flying every single day. As far as the pc-12, I think there was one near UNV? Granted, it may have failed due to thirst, but it was fatal.
 
I think utilization rates for the first question. More of them flying every single day. As far as the pc-12, I think there was one near UNV? Granted, it may have failed due to thirst, but it was fatal.

My company has 30ish PC-12's, we put about 600 hours a year on each, and since 1995, we've had one in flight engine failure, and it could have been restarted.

The crash near UNV was due to a stall/spin, with some ice thrown in for good measure. http://aviation-safety.net/wikibase/wiki.php?id=17024
 
I think utilization rates for the first question. More of them flying every single day. As far as the pc-12, I think there was one near UNV? Granted, it may have failed due to thirst, but it was fatal.

Ok, so why does it seem like you hear about C208 PT-6 failures way more often than Kingair failures?
 
Ok, so why does it seem like you hear about C208 PT-6 failures way more often than Kingair failures?

No question in my mind but that flying a Kingair (pitooie!) is safer than flying a PC-12. But on a cost basis, the PC-12 is more in the complex piston twin department, and I suspect that it gives them a spanking.
 
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