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The VAF News - 6.23.2025. #6367.

DeltaRomeo

doug reeves: unfluencer
Staff member
In/out of COMM this week…top-heavy job3 sched. Hope you had a nice weekend. 100* H.I. here. Hello summer ;^).
v/r,dr


dr
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petehowell
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RE: Testing Fusible Links
…Richard Connell
I used midis on both B leads and have had neither blow as yet. 400h or so. The smaller form factor attracted me to them. I could get my cross tie and starter relay nice and close together on the firewall.
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Build Update; PaulvS RV-6
Today I'm down in the detail of fitting the ailerons and flaps to the wings and have encountered some interference between the aileron pushrod and the flap skin leading edge. There is no mention of this issue on the plans, but it seems inevitable.
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RE Air temp exiting cowl
…HFS
Another interesting perspective ...
I also have a fire suppression system (beside the point), and use two channels from my EI 16-channel engine analyzer to measure the real time air temps at the distribution spider location and under the sump adjacent to the servo (where I have the nozzles for the suppression material distribution). What these two temps provide is an indication of the efficiency of the downdraft cooling system. When Dave Anders did the design he always maintained that the "delta" T across the cylinders should be in the neighborhood of 60*F+ for adequate cooling.
In almost all flight regimes/seasons, in my airplane, this has proven to be the case. Of course, at shutdown, stagnated heat remains to "cook" whatever is available under the plenum, and I can tell you that the temp around the servo area gets quite high for a little while.
To help solve that problem for me, I live in the Central Valley of California, where the ambient temp in my corrugated tin hangar in the summertime easily reaches 120*F+ on hot afternoons, I built a "huffer", that I plug in after every flight to evacuate the stagnated air. Even though the air temp going in may be 100* or more, that is a significant reduction from trapped air in the plenum that can easily reach temps above 200*F. I run it on an 1 1/2 hour mechanical timer, but in just 10 minutes or less, the evacuation cycle has cooled the area significantly. If you are standing anywhere "south" of the cowling exit you can clearly feel the heat extraction ...
YMMV - but not by much.
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RE: Carbon Monoxide in the cockpit
…bjdecker
Seal up holes between the aft most bulkhead flanges and skin in the rudder "cove" below the bottom hinge of the vertical stabilizer...
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inktomi
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OneTwoTree
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OFF TOPIC:
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