Airbus A220-100 vs. Airbus A330-300

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Airbus A220-100 versus Airbus A330-300
35.0 m 114 ft 10 in length 63.66 m 208 ft 9 in
11.5 m 37 ft 9 in height 16.79 m 55 ft 1 in
35.1 m 115 ft 2 in wingspan 60.3 m 197 ft 9 in
2 Turbofans (wing mounted) engines General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700
21,000–23,000 lb thrust per engine 311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60)
42,000–46,000 lb total thrust Depends on the engine type
63,100 kg 139,100 lb MTOW 242,000 kg 533,600 lb
6,390 km 3,451 nm range 11,750 km 6,346 nm
871 km/h 541 mph cruise speed 900 km/h 559 mph
Typical seating 2-class 100-120 capacity 250-290
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.