Airbus A300-600 vs. Bombardier CS100
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Airbus A300-600 |
versus |
Bombardier CS100 |
54.10 m |
177 ft 6 in |
length |
35.00 m |
114 ft 10 in |
16.5 m |
54 ft 2 in |
height |
11.5 m |
37 ft 9 in |
44.84 m |
147 ft 1 in |
wingspan |
35.1 m |
115 ft 2 in |
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 |
engines |
2 x Pratt & Whitney PurePower PW1500G |
56,000lb to 61,500lb |
thrust per engine |
84.1 kN |
112,000–123,000 lb |
total thrust |
168.2 kN |
171,700 kg |
378,600 lb |
MTOW |
54,931 kg |
121,100 lb |
7,500 km |
4,052 nm |
range |
4,074 km |
2,200 nm |
897 km/h |
557 mph |
cruise speed |
871 km/h |
541 mph |
210-250 passengers |
capacity |
110 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.