For those that have access to Falcon 2000 performance data.
What would the s/e second segment climb gradient be out of EGE with temp around 0 c, 4 pax, and fuel for a 2 hour flight? Also, is there a significant difference in single engine performance between a straight 2000 and an EX?
Thanks
What would the s/e second segment climb gradient be out of EGE with temp around 0 c, 4 pax, and fuel for a 2 hour flight? Also, is there a significant difference in single engine performance between a straight 2000 and an EX?
Thanks