Ha! So, I managed to get a look at the performance data for the GLEX, and at 98,000 lbs in ISA, maximum cruise altitude is about FL345 for Mach 0.88, FL380 @ M0.87, FL410 @ M0.85, and at Mach 0.85, you can cruise at FL510 at a weight of 54,000 lbs, which would be a realistic weight with a few thousand pounds of gas left on board. The aircraft will however reach FL510 in ISA at a weight of about 58,500 lbs at which point the ROC has dropped to 200fpm which denotes the theoretical service ceiling at that weight. The service ceiling after a MAUW takeoff in ISA is just over FL420.
I only just got back from work, so I'm keen to see how my changes stack up. And I've got 2 air files open in AAM and AirEd at the same time, comparing the GLEX with the Eaglesoft Citation X which does 0.92. Now THAT'S a cool little machine! I'm looking for obvious discrepancies which when fixed will hopefully line the GLEX up a bit better. I can see this turning into a 5-year plan judging by the fascinating posts I have read so far..!