Boeing C-40 vs Dassault Falcon 900

112 ft 7 in (34.32 m)^[source]

19.33 m (63 ft 5 in)^[source]

41 ft 2 in (12.55 m)^[source]

126,000 lb (57,153 kg)^[source]

171,000 lb (77,564 kg)^[source]

Four, five or six: Pilot, co-pilot, crew chief and loadmaster, plus one 'second loadmaster' when carrying passengers or two when carrying over 100 passengers^[source]

2^[source]

534 kn (615 mph, 989 km/h)^[source]

Mach 0.84–0.87^[source]

950 km/h (590 mph, 510 kn) ; Mach 0.85 (at 11,000 m (36,000 ft))^[source]

3,200 nmi (3,700 mi, 5,900 km) (C-40A), 4,500–5,000 nmi (5,200–5,800 mi; 8,300–9,300 km) (C-40B/C)^[source]

7,400 km (4,600 mi, 4,000 nmi) with 8 passengers^[source]

2 × CFM International CFM56-7B turbofan engines, 27,300 lbf (121 kN) thrust each^[source]

3 × Honeywell TFE731 -5BR-1C turbofans , 21.13 kN (4,750 lbf) thrust each^[source]

41,000 ft (12,000 m)^[source]

15,500 m (50,900 ft)^[source]

40,000 lb (18,144 kg)^[source]

49.0 m 2 (527 sq ft)^[source]