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		ianxbrown
 
 
  Joined: 16 May 2009 Posts: 80
 
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				 Posted: Wed Jul 15, 2009 5:41 am    Post subject: Dynon D10A/EDC in and  RV-9A - weird behaviour | 
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				Has anyone else suffered or resolved the following issue with a Dynon
 D10A EFIS with the optional EDC installed in their RV?
 
 I get "signal too weak to calibrate" messages or something to that
 effect, indicating that the voltage from the EDC is too low.  I'm sure
 I'm going to have to replace the wiring, but wanted to check what others
 had done.  I believe my error was in not using shielded wire, but maybe
 there's a voltage drop on such a long wire run.  For those who have an
 install that works, what wire did you use?  I have the EDC mounted on
 the bulkhead one full space forward of the horizontal stabilizer.  I DO
 see constantly updating numbers, as I'm supposed to, when I go into the
 EDC calibration program.
 
 The reason I'm asking this on this list, rather than with Dynon, is that
 I'm looking for aircraft specific info, since it's quite a long wire
 run.
 
 Any other ideas or experience would be appreciated.  Thanks,
 
 Ian Brown
 Bromont
 Quebec
 
  On Tue, 2009-07-14 at 23:58 -0700, RV-List Digest Server wrote:
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                       Total Messages Posted Tue 07/14/09: 1
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       1. 06:45 AM - RV10 tail kit (assembled) for sale  (Rlepre)
   
  
  
  ________________________________  Message 1  _____________________________________
  
  
  Time: 06:45:51 AM PST US
  Subject: RV10 tail kit (assembled) for sale
  From: "Rlepre" <RLaviation(at)aol.com>
  
  
  I have an RV 10 tail kit for sale.  I can deliver.  Contact me at RLaviation(at)aol.com
  
  
  Read this topic online here:
  
  http://forums.matronics.com/viewtopic.php?p 52945#252945
  
  
   
  
  
   
  
  
  
 
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		sbuc(at)hiwaay.net Guest
 
 
 
 
 
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				 Posted: Wed Jul 15, 2009 10:20 am    Post subject: Dynon D10A/EDC in and  RV-9A - weird behaviour | 
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				Ian wrote:
  	  | Quote: | 	 		   
  
  Has anyone else suffered or resolved the following issue with a Dynon
  D10A EFIS with the optional EDC installed in their RV?
  
  I get "signal too weak to calibrate" messages or something to that
  effect, indicating that the voltage from the EDC is too low.  I'm sure
  I'm going to have to replace the wiring, but wanted to check what others
  had done.  I believe my error was in not using shielded wire, but maybe
  there's a voltage drop on such a long wire run.  For those who have an
  install that works, what wire did you use?  I have the EDC mounted on
  the bulkhead one full space forward of the horizontal stabilizer.  I DO
  see constantly updating numbers, as I'm supposed to, when I go into the
  EDC calibration program.
  
  The reason I'm asking this on this list, rather than with Dynon, is that
  I'm looking for aircraft specific info, since it's quite a long wire
  run.
  
  Any other ideas or experience would be appreciated.  Thanks,
  
  Ian Brown
  Bromont
  Quebec
  
 
 | 	  
 Ian,
 
 Can't help with your specific problem but I can tell you that I am using 
 CAT5 network cable (non-shielded) for the Dynon magnetometer under the 
 tail of my RV-6. My installation has worked perfectly for several years.
 
 Shielded cable is not necessary for proper operation of the mag. You 
 might take a good look at the connectors in your harness to make sure 
 there isn't a high-resistance fault in a crimp or solder connection.
 
 Sam Buchanan
 
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		bartrim(at)gmail.com Guest
 
 
 
 
 
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				 Posted: Wed Jul 15, 2009 10:20 am    Post subject: Dynon D10A/EDC in and  RV-9A - weird behaviour | 
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				Hi Ian;
      I've got the D10A/EDC in an RV9 and had no problems, but I used shielded wire as I have access to plenty of it. I would recommend that you call Dynon's tech support. They are excellent and their service is second to none. 
      Your installation is not at all uncommon and they would be able to provide you with any aircraft specific information that you require. If you are determined to try to do this with help from a list then I would recommend the Aero-Electric list as a much more specific list for this sort of problem.
      I once fried my D10 doing something really stupid that I should have known better (always use a grounded tip soldering iron) and when I called Dynon and told them what I did, they said no problem. I had to pay 1-way shipping and they fixed it free and paid the return shipping. It was out of my plane for little more than a week. That's good service.
  
  Todd
  C-FSTB
  RV9 13BTurbo
  
  On Wed, 2009-07-15 at 09:33 -0400, Ian wrote:  	  | Quote: | 	 		    	  | Quote: | 	 		  
 --> RV-List message posted by: Ian <ixb(at)videotron.ca (ixb(at)videotron.ca)>
 
 Has anyone else suffered or resolved the following issue with a Dynon
 D10A EFIS with the optional EDC installed in their RV?
 
 I get "signal too weak to calibrate" messages or something to that
 effect, indicating that the voltage from the EDC is too low.  I'm sure
 I'm going to have to replace the wiring, but wanted to check what others
 had done.  I believe my error was in not using shielded wire, but maybe
 there's a voltage drop on such a long wire run.  For those who have an
 install that works, what wire did you use?  I have the EDC mounted on
 the bulkhead one full space forward of the horizontal stabilizer.  I DO
 see constantly updating numbers, as I'm supposed to, when I go into the
 EDC calibration program.
 
 The reason I'm asking this on this list, rather than with Dynon, is that
 I'm looking for aircraft specific info, since it's quite a long wire
 run.
 
 Any other ideas or experience would be appreciated.  Thanks,
 
 Ian Brown
 Bromont
 Quebec
 
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		mike@hotlinesinc.com
 
 
  Joined: 27 Aug 2009 Posts: 1
 
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				 Posted: Thu Aug 27, 2009 10:12 am    Post subject: Re: Dynon D10A/EDC in and  RV-9A - weird behaviour | 
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				Beware of internal pitot leaks with Dynon D10A
 
 I installed a Dynon 10A a couple years ago as a back up AI in a warbird.
 A recent pitot static check uncovered a pitot leak that was pretty severe.
 The leak was traced and verified as being internal to the Dynon D10A.
 Disassembly of the unit revealed that the pitot connection to the solid state sensor for airspeed was loose. The static port on the sensor also came loose during disassembly.
 This unit has under 10 hours of operation.
 There is no way I would depend on this unit  as a primary flight instrument
 
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