Airbus A310-300 vs. Bombardier CS300
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Airbus A310-300 |
versus |
Bombardier CS300 |
46.66 m |
153 ft 1 in |
length |
38.0 m |
124 ft 7 in |
15.8 m |
51 ft 10 in |
height |
11.5 m |
37 ft 9 in |
43.9 m |
144 ft |
wingspan |
35.1 m |
115 ft 2 in |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
2x Pratt & Whitney PurePower PW1000G |
52,000 lb |
thrust per engine |
93.4 kN |
104,000 lb |
total thrust |
186.8 kN |
148,768 kg |
328,000 lb |
MTOW |
67,585 kg |
149,000 lb |
8,050 km |
4,348 nm |
range |
5,463 km |
2,952 nm |
482 knots |
279 mph |
cruise speed |
871 km/h |
541 mph |
190-230 passengers |
capacity |
130 to 145 passengers |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.