Oscar Avalle Posted July 12, 2012 Report Share Posted July 12, 2012 As part of my panel upgrade I installed a new JPI 730 with fuel flow (FF). I was wondering if somebody had an approximate value for the K factor for the FF so I could program it into my JPI and fine tune it later . As usual thank you very much your help. Quote Link to comment Share on other sites More sharing options...
jetdriven Posted July 12, 2012 Report Share Posted July 12, 2012 Isnt the K-factor printed on the fuel flow transducer? Quote Link to comment Share on other sites More sharing options...
Oscar Avalle Posted July 12, 2012 Author Report Share Posted July 12, 2012 Not on mine... Quote Link to comment Share on other sites More sharing options...
MooneyMitch Posted July 12, 2012 Report Share Posted July 12, 2012 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. Quote Link to comment Share on other sites More sharing options...
Bolter Posted July 12, 2012 Report Share Posted July 12, 2012 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 Quote Link to comment Share on other sites More sharing options...
Oscar Avalle Posted July 12, 2012 Author Report Share Posted July 12, 2012 Thanks for the recommendations...I just called JPI and asked them. They said that the K factor was either 30 or 85 and that I should try both and see what works. Quote Link to comment Share on other sites More sharing options...
Oscar Avalle Posted July 12, 2012 Author Report Share Posted July 12, 2012 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. Quote Link to comment Share on other sites More sharing options...
rahawk Posted July 16, 2012 Report Share Posted July 16, 2012 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. Quote Link to comment Share on other sites More sharing options...
Oscar Avalle Posted July 16, 2012 Author Report Share Posted July 16, 2012 Thank you! Quote Link to comment Share on other sites More sharing options...
Lood Posted July 17, 2012 Report Share Posted July 17, 2012 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. Quote Link to comment Share on other sites More sharing options...
Awful_Charlie Posted July 17, 2012 Report Share Posted July 17, 2012 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. Quote Link to comment Share on other sites More sharing options...
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