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DA 42 accident



 
 
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  #1  
Old April 26th 07, 02:08 AM posted to rec.aviation.piloting
Kev
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Posts: 368
Default DA 42 accident

On Apr 24, 3:47 pm, "Mike Isaksen" wrote:
wrote in message ...
That is, while the FADEC itself probably doesn't require much
in the way of power, how much power does it take to manipulate
the throttle, mixture, and prop?


The answers to those kind of questions seem to be missing from the public
record, and even the public discussion. [..]


We had a large discussion of FADEC right here last November.
Unfortunately, non-engineer types decided to hijack the discussion,
mostly because they wanted to bash anyone who agreed with Mxsmanic
that all-electronic systems can have major failure modes. (Ever have
your car engine stop because of a failed sensor? I have.)

At that time, I wrote "Losing all power (including the battery backup)
on a FADEC means your engine stops."

Multiple people (who I will not name because they should rightfully be
embarrassed, but they post here a lot) threw insults at the very idea
that this could happen.

In any case, the FAA deems that EECs (Electronic Engine Controllers)
should fail such that the engine is producting at least 85% power.
EECs are just engine aids, however. Full authority FADECs have no
such requirement. Instead, they are supposed to have backup
batteries and/or alternators. Just like the DA-42, basically.

Regards, Kev

  #2  
Old April 26th 07, 10:53 AM posted to rec.aviation.piloting
Dylan Smith
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Posts: 530
Default DA 42 accident

On 2007-04-26, Kev wrote:
We had a large discussion of FADEC right here last November.
Unfortunately, non-engineer types decided to hijack the discussion,
mostly because they wanted to bash anyone who agreed with Mxsmanic
that all-electronic systems can have major failure modes. (Ever have
your car engine stop because of a failed sensor? I have.)


I've had more older car engines stop because of failed mechanical
ignition parts like points. I've never actually had a car engine with an
ECU fail.

I know a pilot who had a double magneto failure, too, which resulted in
the C172 on its back in a field. Guess what - most two magneto engines
have single points of failure.

It's not a question that FADECs will fail - but what will be more
failure prone: a manual-everything engine where the pilot can mismanage
the engine into quitting, or a FADEC that can lose electrical supply and
cause the engine to quit. Only time will really tell in aviation which
is more reliable. However, my bet on having owned both cars with purely
mechanical ignition and cars with engine management computers is that
the ones with engine management computers are orders of magnitude more
reliable. I would at this stage be putting my bets on FADEC being more
relibale than purely mechanical engines + manual engine management in
the long run. That's not to say FADECs won't fail, but pilots+mechanical
electrical systems will fail more often.

--
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  #3  
Old April 26th 07, 01:29 PM posted to rec.aviation.piloting
Maxwell
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Posts: 1,116
Default DA 42 accident


"Dylan Smith" wrote in message
...

I know a pilot who had a double magneto failure, too, which resulted in
the C172 on its back in a field. Guess what - most two magneto engines
have single points of failure.


What caused the mags to fail?


  #4  
Old April 26th 07, 02:20 PM posted to rec.aviation.piloting
Dylan Smith
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Posts: 530
Default DA 42 accident

On 2007-04-26, Maxwell wrote:
What caused the mags to fail?


I don't remember the specifics (and I'm trying to find the NTSB report
with no joy so far). I believe it was one of those 'dual mag'
installations and there was a mechanical failure.

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  #5  
Old April 26th 07, 06:29 PM posted to rec.aviation.piloting
Peter Dohm
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Posts: 1,754
Default DA 42 accident


"Maxwell" wrote in message
...

"Dylan Smith" wrote in message
...

I know a pilot who had a double magneto failure, too, which resulted in
the C172 on its back in a field. Guess what - most two magneto engines
have single points of failure.


What caused the mags to fail?


Obviously, I am not familiar with the particular case; but here are a couple
of scenarios:
1 There is a single gear which drives the entire accessory section.
2 There is/was a product called a dual magneto, used on some four
cylinder Lycoming engines which had an internal gear to drive the two
magneto sections and impulse coupler(s). There were several failures on
relatively new Piper Tomahawks in the early eighties.

Additional possibilities include shorts behind the instrument panel, or even
in the ignition switch or switches--since a magneto is dissabled (turned
off) by shorting the P-lead toground.

In addition to the magnetos; common failure modes include mixture and
throttle control cables and fittings.

Like Dylan, I have found the automotive ECMs to be far more reliable in
service than the old breaker ignition systems. I have had a defective
throttle positioner which resulted in a higher than normal idle speed, and a
rough running engine due to a defective spark plug, but nothing that
disabled the engines. So, personal feelings aside (which I admit is another
issue), the ECMs and FADECs seem to have better long term reliability than
the mechanical/manual systems they replace--and they may far fewer mistakes
than I do.

Peter



  #6  
Old April 26th 07, 07:10 PM posted to rec.aviation.piloting
Maxwell
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Posts: 1,116
Default DA 42 accident


"Peter Dohm" wrote in message
.. .
..

Additional possibilities include shorts behind the instrument panel, or
even
in the ignition switch or switches--since a magneto is dissabled (turned
off) by shorting the P-lead toground.

In addition to the magnetos; common failure modes include mixture and
throttle control cables and fittings.

Like Dylan, I have found the automotive ECMs to be far more reliable in
service than the old breaker ignition systems. I have had a defective
throttle positioner which resulted in a higher than normal idle speed, and
a
rough running engine due to a defective spark plug, but nothing that
disabled the engines. So, personal feelings aside (which I admit is
another
issue), the ECMs and FADECs seem to have better long term reliability than
the mechanical/manual systems they replace--and they may far fewer
mistakes
than I do.


But that's a completely different kettle of fish. I was wondering what cause
the dual mag failure on a 172.


  #7  
Old April 27th 07, 04:03 AM posted to rec.aviation.piloting
Kev
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Posts: 368
Default DA 42 accident

On Apr 26, 1:29 pm, "Peter Dohm" wrote:
Like Dylan, I have found the automotive ECMs to be far more reliable in
service than the old breaker ignition systems. [...]


grin That's because neither of you have had a failure yet. I've
had automotive computer systems fail due to cold solder joints, part
failures, sensor failures. Even had a transmission computer decide
to go into limp mode just because a sensor glitched for a few
seconds. If I were out in the woods, I'd much rather have old-style
points act up, than have a computer failure.

(Throttle positioning sensors don't count... the throttle is still
mechanical in that case.)

Mind you, every day I'm glad that my vehicles start instantly because
of electronic engine aids. But I'm not so happy about my wif'e's Land
Rover with fully electronic gas pedal. It's already had a recall
because the software could glitch and go into full throttle mode.
Yes, that could happen mechanically as well, but that you can fix
yourself on the side of the road!

And as I've opined before, I'm not looking forward to cars with fully
electronic brake pedals and steering wheels. shiver Not in my
lifetime, anyway ;-)

Regards, Kev

  #8  
Old April 27th 07, 06:05 PM posted to rec.aviation.piloting
Peter Dohm
external usenet poster
 
Posts: 1,754
Default DA 42 accident


"Kev" wrote in message
oups.com...
On Apr 26, 1:29 pm, "Peter Dohm" wrote:
Like Dylan, I have found the automotive ECMs to be far more reliable in
service than the old breaker ignition systems. [...]


grin That's because neither of you have had a failure yet. I've
had automotive computer systems fail due to cold solder joints, part
failures, sensor failures. Even had a transmission computer decide
to go into limp mode just because a sensor glitched for a few
seconds. If I were out in the woods, I'd much rather have old-style
points act up, than have a computer failure.

(Throttle positioning sensors don't count... the throttle is still
mechanical in that case.)

Mind you, every day I'm glad that my vehicles start instantly because
of electronic engine aids. But I'm not so happy about my wif'e's Land
Rover with fully electronic gas pedal. It's already had a recall
because the software could glitch and go into full throttle mode.
Yes, that could happen mechanically as well, but that you can fix
yourself on the side of the road!

And as I've opined before, I'm not looking forward to cars with fully
electronic brake pedals and steering wheels. shiver Not in my
lifetime, anyway ;-)

Regards, Kev

There are a lot of new "features" that can keep me driving and flying the
old ones as well. And I am just about old enough to make that a viable
option--expecially for aircraft.

Peter


  #9  
Old April 27th 07, 01:00 AM posted to rec.aviation.piloting
Jim Carter[_1_]
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Posts: 403
Default DA 42 accident

At one time there was a single drive to a Tee connector that drove both
magnetos. Stupid design that probably met some budget requirement with no
regard to why there were two magnetos to start with.

Dylan's statement that "most two magneto engines have single points of
failure" surprises me unless he's talking about other components. A properly
implemented two magneto setup is fully redundant.

--
Jim Carter
Rogers, Arkansas
"Maxwell" wrote in message
...

"Dylan Smith" wrote in message
...

I know a pilot who had a double magneto failure, too, which resulted in
the C172 on its back in a field. Guess what - most two magneto engines
have single points of failure.


What caused the mags to fail?



  #10  
Old April 28th 07, 09:07 AM posted to rec.aviation.piloting
Dylan Smith
external usenet poster
 
Posts: 530
Default DA 42 accident

On 2007-04-27, Jim Carter wrote:
Dylan's statement that "most two magneto engines have single points of
failure" surprises me unless he's talking about other components. A properly
implemented two magneto setup is fully redundant.


That big gear at the back of the engine that drives the mags is a single
point of failure. While it is a very robust object, it's still driving
both mags.

--
Yes, the Reply-To email address is valid.
Oolite-Linux: an Elite tribute: http://oolite-linux.berlios.de
 




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