Airbus A310-300 vs. Airbus A321LR
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Airbus A310-300 |
versus |
Airbus A321LR |
46.66 m |
153 ft 1 in |
length |
44.51 m |
146 ft 0 in |
15.8 m |
51 ft 10 in |
height |
11.76 m |
38 ft 7 in |
43.9 m |
144 ft |
wingspan |
35.8 m |
117 ft 5 in |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
52,000 lb |
thrust per engine |
Over 33,000 lbs (147 kN) |
104,000 lb |
total thrust |
66,000 lbs (294 kN) |
148,768 kg |
328,000 lb |
MTOW |
97,000 kg |
213,800 lb |
8,050 km |
4,348 nm |
range |
7,400 km |
4,000 nm |
482 knots |
279 mph |
cruise speed |
832 km/h |
517 mph |
190-230 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.