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K factor for JPI 730 and O360 A1A


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I suspect if you provide your


fuel flow equipment to JPI tech. Support, they will have the K factor information you are seeking.  I found this to be true with Insight tech. Support.


Also, you might just check on your JPI head as that information may be documented on the placard with the p/n and s/n.

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On my JPI fuel flow, the K factor was hand scrawled on a little tag in the packaging with the transducer, not the display.   It was hard to read, and the "K" looked like a "16" to me, so I thought it was something completely different until corrected by my A&P who knew what he was looking at.  Look though everything you received a second time.  Or maybe your A&P already entered in the value off the tag?


FWIW, I adjsuted my K value over about 5 fill ups.  3 to confirm a typical reading, each at least 30 gallons, then 2 minor tweaks as it was over-reading more than I thought necessary even as a safety margin.  


-dan

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Jim, thank you. As I mentioned in my other post, I am now waiting to get back in the air and try everything out... I am just concerned after all these upgrades that something may (will) not work... as expected. Otherwise the panel is really nice. The avionics shop did a great job and not too expensive.

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I just installed an edm700, and the K factor was on the transducer.  It was 29.86.  it is very accurate.  There is a formula in the operating handbook that will help you to tweak it after several fill ups.  Mine was within .3 of a gallon after burning 35+ gallons. 

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30/85 sounds about right. I calibrated mine twice after two flights, each lasting almost 3 hrs and it came out at 85,???. That's for liters, so I suspect the "30" from JPI to be if you're ure using Gal, instead.

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The K factor comes from the number of time the small impeller turns for a volume unit of fuel flow, and the head unit has to sort out the corrections for USG/lbs/litres/ImpG or whatever.  I don't know what the US retail limits are, but years ago when I worked in a UK auto fuel retailer, the retailer was allowed -0.5% to +1% volume of fuel against the pump indication at full flow.  Depending on what you are measuring, and allowing for fuel expansion/contraction with temperature (density decreases by about 0.5% per 5 °C (9 °F) increase in temperature) I would suggest that when you get consistently to within 2% you are close to the limit of the equipment on the plane and at the refueller can resolve.

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