FAA-H-8083-25C · Source PDF page 457

Appendix A

Challenger 605 Range/Payload Profile · PHAK page A-5

Original FAA PHAK page A-5
Faithful view of source page A-5. Select it to enlarge.

Searchable transcription

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