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johncollier5110(at)msn.co Guest
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Posted: Sun Feb 25, 2007 3:19 am Post subject: Glass for IFR |
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Guys and Gals,
I'm starting to plan out my avionics. I'm leaning toward an all glass
panel - IFR legal. I'm considering a couple of Dynon's with backup
batteries. I've brainstormed (to the best of my abilities) all the possible
ways I could get myself into trouble. With backup batteries in each dynon
I'm "relatively" safe from a total electrical failure. Also, if I lose one
EFIS...I'll switch to the other dynon for flight data.
Looking for some advice and recommendations... what I'm I overlooking
or not considering?
Thanks
John
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dav1111(at)cox.net Guest
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Posted: Mon Feb 26, 2007 3:43 am Post subject: Glass for IFR |
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I have an all glass IFR panel in my RV-10 and love it. You can see it at:
http://img139.imageshack.us/my.php?image=panelinstalled1bl4.jpg
It is a three screen Grand Rapids system with weather overlay and I love it. The center glass screen is a sport model with it's own AHRS for backup.
As far as backup batteries as long as you can identify a battery or alternator failure they are somewhat unnecessary. The amount of amps drawn by a single EFIS system and an autopilot is so small that you can do an IFR let down on your main battery with little problems.
I went ahead and put an SD-8 backup on my engine as a backup to the alternator just to be on the safe side however.
Best regards,
Russ Daves
N710RV - Flying RV-10
N65RV - RV-6A sold
[quote][b]
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rtitsworth
Joined: 16 Jan 2006 Posts: 76 Location: Detroit, Mi
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Posted: Mon Feb 26, 2007 5:15 am Post subject: Glass for IFR |
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A thought/scenario… If you had some sort of electrical fire (smoke, serious smell, etc), and were unsure of the source, and wanted to shutdown the alternator(s) and master(s), what would be left? Seems that having a small, local, dedicated stby battery attached to an attitude instrument would be helpful (necessary) in IMC – especially if you plan on flying high enough that it takes several minutes (or longer) to descent to safety. Assuming of course that stby instrument is not the original smoke problem.
My .02
Rick
From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Russell Daves
… As far as backup batteries as long as you can identify a battery or alternator failure they are somewhat unnecessary. The amount of amps drawn by a single EFIS system and an autopilot is so small that you can do an IFR let down on your main battery with little problems.
[quote][b]
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Bruce(at)glasair.org Guest
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Posted: Mon Feb 26, 2007 5:18 am Post subject: Glass for IFR |
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Nice panel. I have a stupid question, if you're flying along in solid IMC and all of a sudden one of your EFIS says you're turning right and the other says you're turning left, on which one do you bet your life?
Bruce
www.glasair.org
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rv9jim(at)juno.com Guest
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Bruce(at)glasair.org Guest
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Posted: Mon Feb 26, 2007 6:51 am Post subject: Glass for IFR |
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OK, I looked again at your panel picture and darn, I just can't see that TT
TC.
Bruce
www.glasair.org
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brianpublic2(at)starband. Guest
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Posted: Mon Feb 26, 2007 10:07 am Post subject: Glass for IFR |
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I went with multiple brands, on the idea that any hardware or software
problems with one brand would not show up in the second brand. I chose
Blue Mountain as primary and Grand Rapids as secondary. I also later ended
up getting a Dynon as third, instead of a turn coordinator. Whether this
turns out to be better than, say, a dual screen, dual AHRS GRT with TruTrak
A/P remains to be discovered. See avionics pages for details
brian
http://brian76.mystarband.net/RV-7Ahome.htm
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brianpublic2(at)starband. Guest
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Posted: Mon Feb 26, 2007 10:08 am Post subject: Glass for IFR |
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This thought, as well as the previous one from Rick Gray, are, IMHO, a good reason for a third display. My thinking was that by not buying a turn coordinator, ½ of a Dynon is already paid for. It’s small and self-contained. And it has it’s own internal battery, so you can shut down all else, and it will still work.
brian
<![if !supportEmptyParas]> <![endif]>
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Bret Smith
Joined: 09 Jan 2006 Posts: 178 Location: Mineral Bluff, GA
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Posted: Tue Feb 27, 2007 6:01 pm Post subject: Glass for IFR |
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Bruce, why is that scary? The autopilot is considered a primary instrument during single-pilot IFR. This is also a procedure taught during IFR training.
Bret Smith
RV-9A (91314)
Mineral Bluff, GA
www.FlightInnovations.com
From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Bruce Gray
Sent: Tuesday, February 27, 2007 10:33 AM
To: rv-list(at)matronics.com
Subject: RE: Glass for IFRGlass for IFR
Now that's scary!
Bruce
www.glasair.org
[quote]
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_________________ Bret Smith
RV-9A (Emp) |
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Bruce(at)glasair.org Guest
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Posted: Tue Feb 27, 2007 6:52 pm Post subject: Glass for IFR |
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Back in my Aero Engineering school days we had to study a subject called Human Factors Engineering or man/machine interfacing. Most pilots like to flip a switch/pull a knob and then monitor the results of that action, in real time, as the desired or commanded action takes place. Move the stick and watch the ADI change. This is called closed loop control, the pilot is in the control loop and can reverse or correct any undesired results.
With your autopilot controlled recovery and a dark EFIS, the pilot is out of the control loop. While the results might be successful, the time waiting for the end of the process, to me at least would be terrifying. With a redundant ADI, ASI, and altimeter the pilot would at least be able to monitor the aircrafts return to controlled flight. It's all a matter of what your comfortable with, I guess. Engaging the autopilot and hoping for the best just doesn't cut it with me.
Bruce
www.glasair.org
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Bret Smith
Joined: 09 Jan 2006 Posts: 178 Location: Mineral Bluff, GA
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Posted: Tue Feb 27, 2007 7:30 pm Post subject: Glass for IFR |
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>Engaging the autopilot and hoping for the best just doesn't cut it with me.<
Whatever lightens your "worry bucket"... Like Sam said, my A/P is ALWAYS on in solid IMC.
Bret Smith
RV-9A (91314)
Mineral Bluff, GA
www.FlightInnovations.com
From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Bruce Gray
Sent: Tuesday, February 27, 2007 9:51 PM
To: rv-list(at)matronics.com
Subject: RE: Glass for IFR
Back in my Aero Engineering school days we had to study a subject called Human Factors Engineering or man/machine interfacing. Most pilots like to flip a switch/pull a knob and then monitor the results of that action, in real time, as the desired or commanded action takes place. Move the stick and watch the ADI change. This is called closed loop control, the pilot is in the control loop and can reverse or correct any undesired results.
With your autopilot controlled recovery and a dark EFIS, the pilot is out of the control loop. While the results might be successful, the time waiting for the end of the process, to me at least would be terrifying. With a redundant ADI, ASI, and altimeter the pilot would at least be able to monitor the aircrafts return to controlled flight. It's all a matter of what your comfortable with, I guess. Engaging the autopilot and hoping for the best just doesn't cut it with me.
Bruce
www.glasair.org
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_________________ Bret Smith
RV-9A (Emp) |
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Bruce(at)glasair.org Guest
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Posted: Tue Feb 27, 2007 7:56 pm Post subject: Glass for IFR |
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Surprisingly, so is mine.
Bruce
www.glasair.org
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ronlee(at)pcisys.net Guest
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Posted: Wed Feb 28, 2007 11:31 am Post subject: Glass for IFR |
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Quote: | >Engaging the autopilot and hoping for the best just doesn't cut it
with me.<
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Quote: |
Whatever lightens your "worry bucket"... Like Sam said, my A/P is
ALWAYS on in solid IMC.
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Quote: |
There is the key. Keep the A/P on. With my Trio autopilot connected to
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a GNS 430, I question whether a GNS 430 failure would cause the plane to
depart belly to earth flight.
Will that happen if one of your EFISs die completely or suffer another
undiscovered bug like happened to Mike?
Ron
Lee
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ronlee(at)pcisys.net Guest
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Posted: Thu Mar 01, 2007 9:14 am Post subject: Glass for IFR |
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Quote: | Why not vacuum? Weight, cost, lousy reliability come to mind. My
personal belief is you would typically overhaul (or experience
failure) of a vacuum system several times over before your properly
designed and installed electrical whizzies hiccoughed for the first
time.
IMO, of course.
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I just ordered a new vacuum pump. Failed after about 1000 hours.
Mike's post (thanks Mike) shows that coding for these EFIS systems
may be less than rigorous. We recently saw a forced landing in less
than ideal terrain apparently because of a software problem in a
experimental class mag system.
It seems that if you are really going to fly in IFR conditions then
you might want to go up with a safety pilot and see how well you do
if certain systems go south. Example, your only EFIS dies. Can you
safely fly and make an instrument approach using everything left
that is available to you?
It might be useful if suggested system components be identified that
provides adequate redundancy in the event of a major comnponent
failure. The groupings may be as follows:
1) EFIS, all electric
2) EFIS, vacuum
3) No EFIS, all electric
4) No EFIS, vacuum
I would fall into Group 4. Vacuum Horizon and DG, Typical airspeed,
altimeter, rate of climb plus electric T&B. Trio Ez-pilot autopilot.
Of course I have not finished my instrument rating. Signed off to
take the practical but need to fix the vacuum system.
Ron Lee
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jjessen
Joined: 22 Apr 2006 Posts: 285 Location: OR
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Posted: Thu Mar 01, 2007 9:53 am Post subject: Glass for IFR |
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Some certified's, at least the Columbia, are using two independent electric
systems. I would think the battery backup EFIS systems out there would also
qualify as independent. You could certainly go vacuum as backup. Nothing
wrong with that. Same as going EI on top and standard mag on the bottom.
The chance of an electric and a vacuum failure at the same time would be
minimal, I would venture. No matter what, one should, as suggested, get an
instructor and go fly in IMC with systems being taken off line in various
ways to see what it would be like and practice recovering, troubleshooting.
Nothing like practice.
John Jessen (and this thread is just great!)
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ronlee(at)pcisys.net Guest
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Posted: Thu Mar 01, 2007 11:56 am Post subject: Glass for IFR |
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No matter what, one should, as suggested, get an instructor and go fly
in IMC with systems being taken off line in various ways to see what it
would be like and practice recovering, troubleshooting.
Quote: | Nothing like practice.
Actually John, I would not go true IMC. Use foggles or other
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devices. That way if you start to enter a spiral the instructor
can more easily recover or have you remove the foggles.
As someone mentioned, having an EFIS die with only a T&B (?) backup
available may be just a matter of time before you lose controlled
flight. Assumes no autopilot of course.
Ron Lee
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jhnstniii(at)AOL.COM Guest
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Posted: Thu Mar 01, 2007 5:27 pm Post subject: Glass for IFR |
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Have been following this post with interest. Our plan from the beginning was to fly IFR. Here's what we did:
Vacuum attitude indicator
Backup electric attitude indicator
Vacuum DG
Electric T & B (S-Tec 30 with altitude hold)
Garmin 430
We plan to get a good Garmin handheld like the 496 and mount that, too, which can give you a self-contained virtual panel on internal battery.
Plus, we plan to replace the vacuum pump and the alternator at regular intervals, probably every 500 hours (yep, buy new ones).
So far we haven't flown any actual IFR because we are still flight testing.
Just our .02
LeRoy Johnston and David White - Ohio - RV-6 Esperanza 65 hours flying.
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jacklockamy(at)verizon.ne Guest
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Posted: Fri Mar 02, 2007 6:16 am Post subject: Glass for IFR |
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Maybe the better way to approach inevitable vacuum pump failures is to have the pump rebuilt/replaced every 500 hrs instead of waiting for it to fail. I believe this is the same timeframe (500 hrs) that Slick magnetos are also recommended to be rebuilt/replaced. Would be any easy way to remember when the pump needed replacing (i.e. 500, 1000, 1500, 2000 hrs, etc.)
Certainly would be cheap insurance and if nothing else... peace of mind when flying in the soup as others have mentioned.
Jack
do not archive
[quote][b]
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rocketbob(at)gmail.com Guest
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Posted: Fri Mar 02, 2007 7:32 am Post subject: Glass for IFR |
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The best approach is to use a wet vacuum pump and a separator. I know of many wet vaccum pumps that outlived the engines they were installed in. I don't know of a single dry pump that I've ever seen that didn't fail in the shear coupler. I've never seen on where the vanes wore out. If the dry pumps didn't have the silly shear coupler they would be far more reliable.
Regards,
Bob Japundza
RV-6 flying F1 under const.
On 3/2/07, Jack Lockamy <jacklockamy(at)verizon.net (jacklockamy(at)verizon.net)> wrote:[quote]
Maybe the better way to approach inevitable vacuum pump failures is to have the pump rebuilt/replaced every 500 hrs instead of waiting for it to fail. I believe this is the same timeframe (500 hrs) that Slick magnetos are also recommended to be rebuilt/replaced. Would be any easy way to remember when the pump needed replacing (i.e. 500, 1000, 1500, 2000 hrs, etc.)
Certainly would be cheap insurance and if nothing else... peace of mind when flying in the soup as others have mentioned.
Jack
do not archive
[quote][b] http://www.matronics.com/Navigator?RV-List http://forums.matronics.com [quote][b]
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pitts_pilot(at)bellsouth. Guest
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Posted: Fri Mar 02, 2007 8:00 am Post subject: Glass for IFR |
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Bob J. wrote:
Quote: | The best approach is to use a wet vacuum pump and a separator. I know of many wet vaccum pumps that outlived the engines they were installed in. | They're heavier, and the separator isn't that efficient. That's why the dry pump is standard on most 'newer' engines.
Quote: | I don't know of a single dry pump that I've ever seen that didn't fail in the shear coupler. I've never seen on where the vanes wore out. | Well, that's why the pump fails. The vanes are plasticized carbon, and the centripetal force keeps the vanes in contact with the pumps outer wall, which causes them to wear down slowly. The vanes are the sacrificial parts. When the vanes get thin ..... about 1/4" wide or so, they jam in the ports and the shear coupling fails.
Quote: | If the dry pumps didn't have the silly shear coupler they would be far more reliable. | Can't agree with that! That's like replacing a fuse with a piece of metal. If the shear coupling didn't fail when the pump jammed ..... some other, weaker, link in the food chain would have to ...... maybe internal to the engine. Who knows??? I sure wouldn't want to find out!
FYI ..... I had a dry pump last more than 2000 hours on an O-235 ...... and yes, it failed as I was climbing out through the soup. Sigh.
Linn
[quote]
Regards,
Bob Japundza
RV-6 flying F1 under const.
On 3/2/07, Jack Lockamy <jacklockamy(at)verizon.net (jacklockamy(at)verizon.net)> wrote: Quote: |
Maybe the better way to approach inevitable vacuum pump failures is to have the pump rebuilt/replaced every 500 hrs instead of waiting for it to fail. I believe this is the same timeframe (500 hrs) that Slick magnetos are also recommended to be rebuilt/replaced. Would be any easy way to remember when the pump needed replacing (i.e. 500, 1000, 1500, 2000 hrs, etc.)
Certainly would be cheap insurance and if nothing else... peace of mind when flying in the soup as others have mentioned.
Jack
do not archive
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