Today's Message Index:
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1. 02:37 PM - AV 30 Wiring (farmrjohn)
2. 02:50 PM - Lycoming EIS wirig recommendation (Werner Schneider)
Message 1
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Now that the AV 30 has STC approval for certificated airplanes I have some questions
on the wiring differences.
The experimental say power is to be from the battery or essential bus only, the
"approved" manual says power is from the avionics bus or main master relay.
Can the experimental version also be powered from the avionics bus?
The certified calls for a 3/16" braided ground strap from the of the d-sub back
shell, maximum of 8". What would be a similar sized stranded wire, and would
the also be a good idea for the experimental version?
On the wiring diagrams some of the shielded wire symbols have an X in them. Does
this indicate twisted pair?
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498136#498136
Attachments:
http://forums.matronics.com//files/av30_experimental_107.jpg
http://forums.matronics.com//files/av30_cert_636.jpg
Message 2
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| Subject: | Lycoming EIS wirig recommendation |
Got today SI 1569A which is talking about the new Lycoming EIS which are
power dependent.
Interesting their wiring recommendation, looks so familiar:
Cheers Werner
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