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11-17-2013, 02:57 PM
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Join Date: Feb 2005
Location: 20km outside of Zurich, Switzerland
Posts: 467
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Where to route the ignition cable?
Hello builders!
I'm unsure where to rout the ignition cable for the top plugs.
Version 1: Cable straigt and a "serviceloop" outside of the baffles. The cable would be inline with the cooling airflow and hopefully do not "fludder" and crack.
Version 2: Service loop inside the baffles. Cable are quite loose and soft, so they can flap around an hit on injection lines, cooling fins and rocker shaft tube.
Both versions have pro and contra, the longer cable is maybe more servicefriendly, but need a clamp somehow to fit it.
Thanks for thinking about it and giving me a answer.
__________________
Dominik
RV-7A, TMX-IO-320, FM-150, Sensenich FP
Flying since 28. April 2016
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11-17-2013, 04:34 PM
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Join Date: Oct 2013
Location: Clearwater Fl
Posts: 16
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The second photo it the one I prefer and then through the rear baffle. Use Aircraft Spruce P/N M2375. I have built hundreds of Lycoming engines and always use these. On the pushrod tube just FWD of the injector line clamp, install another ADEL clamp with a P/N M2755. Just twist the clamp 90 deg so the wires point straight back.
__________________
Owner, Johnson Aeronautical
A/P I/A with 28 years
B707 Flight Engineer
B727 Load Master
Private Pilot 9 years
Mechanic F-4, F-16, C-130, Everything Boeing, Eclipse VLJ, Everything GA, Experimental,
Assisting in a RV-8A
2013 Dues Paid
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11-17-2013, 05:03 PM
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Join Date: Apr 2011
Location: Cincinnati, OH
Posts: 2,789
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supported at baffle
I supported the fwd lead at the side baffle with a p-clamp then through the aft baffle. the leads are zip tied in a couple of places to each other.
__________________
Steve Melton
Cincinnati, OH
RV-9A, Tip-up, Superior O-320, roller lifters, 160HP, WW 200RV, dual impulse slick mags, oil pressure = 65 psi, EGT = 1300F, flight hours = 800+ for all
Simplicity is the art in design.
My Artwork is freely given and published and cannot be patented.
www.rvplasticparts.com
Last edited by Steve Melton : 11-17-2013 at 05:07 PM.
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11-18-2013, 04:06 PM
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Join Date: Feb 2005
Location: 20km outside of Zurich, Switzerland
Posts: 467
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Will do it that way!
Thanks for your input and the numbers of the plamps! I have two of them ready for the cable of the lower plugs. Will buy two more.
I will check those two solutions and install them, but with a clamp more on the way to the rear baffle.
__________________
Dominik
RV-7A, TMX-IO-320, FM-150, Sensenich FP
Flying since 28. April 2016
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11-18-2013, 04:25 PM
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Join Date: Feb 2005
Location: Northwestern USA
Posts: 1,209
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__________________
Matt Burch
RV-7 (last 90%)
http://www.rv7blog.com
VAF #836
Any opinions expressed in this message are my own and not those of my employer.
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11-18-2013, 04:40 PM
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Join Date: Nov 2005
Location: Asheville, NC
Posts: 2,690
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Very nice looking Matt.
Please keep an eye on it.
My dim memory says there were occations where using the injection line Adels for additional hardware changed the natural frequency of the system and caused an engine failure. This may be the reason for the recurring Lycoming AD for confirming the Adels are per the factory locations.
__________________
Bill Pendergrass
ME/AE '82
RV-7A: Flying since April 15, 2012. 850 hrs
YIO-360-M1B, mags, CS, GRT EX and WS H1s & A/P, Navworx
Unpainted, polished....kinda'... Eyeballin' vinyl really hard.
Yeah. The boss got a Silhouette Cameo 4 Xmas 2019.
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11-19-2013, 08:19 PM
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Join Date: Oct 2013
Location: Clearwater Fl
Posts: 16
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The reason for AD 2011-26-04 is to prevent the fuel injector lines from braking at the brazed joint at the ends and to prevent wear at the clamp locations. Due every 100 hours. I check every time the cowl is off!
__________________
Owner, Johnson Aeronautical
A/P I/A with 28 years
B707 Flight Engineer
B727 Load Master
Private Pilot 9 years
Mechanic F-4, F-16, C-130, Everything Boeing, Eclipse VLJ, Everything GA, Experimental,
Assisting in a RV-8A
2013 Dues Paid
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11-19-2013, 08:21 PM
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Join Date: Oct 2013
Location: Clearwater Fl
Posts: 16
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Forgot one thing! Nice engine and leads! The time spent now will pay for itself in the long run!
__________________
Owner, Johnson Aeronautical
A/P I/A with 28 years
B707 Flight Engineer
B727 Load Master
Private Pilot 9 years
Mechanic F-4, F-16, C-130, Everything Boeing, Eclipse VLJ, Everything GA, Experimental,
Assisting in a RV-8A
2013 Dues Paid
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11-23-2013, 05:39 AM
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Join Date: Feb 2005
Location: Northwestern USA
Posts: 1,209
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Quote:
Originally Posted by rzbill
Very nice looking Matt.
Please keep an eye on it.
My dim memory says there were occations where using the injection line Adels for additional hardware changed the natural frequency of the system and caused an engine failure. This may be the reason for the recurring Lycoming AD for confirming the Adels are per the factory locations.
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Hi Bill - I was aware of that AD but your note prompted me to go back and read it again. Here is a link to AD 2011-26-04, and here is a link to Lycoming MSB 342 which the AD references. At first glance I don't actually see anything in there that would prevent someone from adding extra hardware to the existing clamping locations as I did... the AD and MSB just want you to make sure that your fuel injector lines are indeed clamped securely and supported at the specified locations. Having said that, it's so easy to just add another separate set of adel clamps there that I might go back and do it just for peace of mind. Thanks for the heads-up.
- Matt
__________________
Matt Burch
RV-7 (last 90%)
http://www.rv7blog.com
VAF #836
Any opinions expressed in this message are my own and not those of my employer.
Last edited by mburch : 11-23-2013 at 05:54 AM.
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12-30-2013, 01:47 PM
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Join Date: Feb 2005
Location: Northwestern USA
Posts: 1,209
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I re-did these support brackets to not use the same clamps that hold the fuel injection lines. Not as nice looking, but increased peace of mind. I suspect it would not have been a problem, but better safe than sorry.
mcb
__________________
Matt Burch
RV-7 (last 90%)
http://www.rv7blog.com
VAF #836
Any opinions expressed in this message are my own and not those of my employer.
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