Airbus A321LR vs. Beechcraft T-6 Texan II
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Airbus A321LR |
versus |
Beechcraft T-6 Texan II |
44.51 m |
146 ft 0 in |
length |
10.18 m |
33 ft 4 in |
11.76 m |
38 ft 7 in |
height |
3.29 m |
10 ft 10 in |
35.8 m |
117 ft 5 in |
wingspan |
10.21 m |
33 ft 6 in |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
1 x Pratt & Whitney Canada PT6A-68 |
Over 33,000 lbs (147 kN) |
thrust per engine |
1100 lbs |
66,000 lbs (294 kN) |
total thrust |
1100 lbs |
97,000 kg |
213,800 lb |
MTOW |
6,250 lb |
2,835 kg |
7,400 km |
4,000 nm |
range |
900 nm |
1,667 km |
832 km/h |
517 mph |
cruise speed |
320 kts |
199 mph |
180-220 passengers |
capacity |
2 |
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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.