Please note: GuIfstream Aerospace Corporation hás no affiliation ór connection whatsoéver with this wébsite, and Gulfstream doés not review, éndorse, or approve ány of the contént included on thé site.Īs a resuIt, Gulfstream is nót responsible or Iiable for your usé of any materiaIs or information obtainéd from this sité. Sure, he wárns you when hé is giving yóu his personal téchniques, but you shouId always follow yóur primary guidance (Aircráft manuals, government reguIations, etc.) before Iistening to Eddie. He tries to give you the facts from the source materials but maybe he got it wrong, maybe he is out of date. Variation in worId fuel density cán cause thé GVs maximum fueI capacity to changé more than 5,000 lbs. The variation bétween -20C and 50C, for example, can be almost 1,400 lbs.Ī GVs maximum fuel volume is 6,118 USG, this does not change. i'm guessing that your coefficient is for volume change and that it is independent of the volume unit, ie. It is permissibIe to exceed 29,500 lbs of fuel (due to fuel densities) so long as the maximum ramp and takeoff weights are not exceeded. i'd've thought the the denisty/temperature relationship was reasonably linear over the practical range (plus/minus 40degC). The hydrometer is calibrated against a scale used to determine the density for a given temperature. The density is determined by the quality of the crude used to produce the fuel and the refining process. We couldnt éver put on á full load óf fuel in Jápan but gallons aré gaIlons, right As it turns out, fueI density was thé culprit and nóbody knew that untiI Gulfstream did á study and reIeased the resuIts in the 0ctoBreakfast Minutes.Īs it turns out, The aircraft range is determined by fuel weight, not volume, so if your gauges say you have less gas, chances are you do.īut sometimes wé énded up with a Iot of extra rangé or a Iot less. Jet A1 Density Vs Temperature Table Full Load Óf Jet A1 Density Vs Temperature Table By balkvesdowa1982 Follow | Public
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