Airbus A300-600 vs. Airbus A321LR
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Airbus A300-600 |
versus |
Airbus A321LR |
54.10 m |
177 ft 6 in |
length |
44.51 m |
146 ft 0 in |
16.5 m |
54 ft 2 in |
height |
11.76 m |
38 ft 7 in |
44.84 m |
147 ft 1 in |
wingspan |
35.8 m |
117 ft 5 in |
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 |
engines |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
56,000lb to 61,500lb |
thrust per engine |
Over 33,000 lbs (147 kN) |
112,000–123,000 lb |
total thrust |
66,000 lbs (294 kN) |
171,700 kg |
378,600 lb |
MTOW |
97,000 kg |
213,800 lb |
7,500 km |
4,052 nm |
range |
7,400 km |
4,000 nm |
897 km/h |
557 mph |
cruise speed |
832 km/h |
517 mph |
210-250 passengers |
capacity |
180-220 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.