Airbus A321LR vs. DC-10 Air Tanker
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Airbus A321LR |
versus |
DC-10 Air Tanker |
44.51 m |
146 ft 0 in |
length |
55.40 m |
181 ft 10 in |
11.76 m |
38 ft 7 in |
height |
17.7 m |
58 ft 1 in |
35.8 m |
117 ft 5 in |
wingspan |
50.4 m |
165 ft 4 in |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
3 x General Electric CF6-50C2 turbofan engines |
Over 33,000 lbs (147 kN) |
thrust per engine |
Approximately 52,500 lbf |
66,000 lbs (294 kN) |
total thrust |
Approximately 157,500 lbf |
97,000 kg |
213,800 lb |
MTOW |
186,880 kg |
412,000 lb |
7,400 km |
4,000 nm |
range |
3,000 nm |
5,556 km |
832 km/h |
517 mph |
cruise speed |
490 kts |
304 mph |
180-220 passengers |
capacity |
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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.