FAA-H-8083-25C · Source PDF page 457
Appendix A
Challenger 605 Range/Payload Profile · PHAK page A-5

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Challenger 605 Range/Payload Profile
Fuel
Takeoff Field Length (feet) Burn (lb) 3,190 6,570 10,230 14,200 18,105
SL 5,000 ft T G ak ro e s o s ff T ime (hour) 2:00 4:00 6:00 8:00 9:50
ISA ISA +20°C Weight (lb)
50,000
5,840 9,400
4,940 7,755 46,000
4,219 6,432 40,000
Conditions: 26,985 lb BOW, M 0.74
cruise speed, ISA, zero wind, NBAA
Max
Payload IFR reserves (200 NM)
3,600 5,234 35,000
3,000 lb
3,465 4,804 Payload Note: Fuel burn figures provided on
1,000 lb top of graph are based on 1,000 lb
3,401 4,535 Payload Zero Payload payload performance computations.
30,000
0 500 1,000 1,500 2,000 2,500 3,000 3,500 4,000 4,500
Range (NM)
A-5