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
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.