Airbus A321LR vs. Beechcraft T-34 Mentor
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Airbus A321LR |
versus |
Beechcraft T-34 Mentor |
44.51 m |
146 ft 0 in |
length |
7.92 m |
25 ft 11 in |
11.76 m |
38 ft 7 in |
height |
2.95 m |
9 ft 8 in |
35.8 m |
117 ft 5 in |
wingspan |
10.03 m |
32 ft 11 in |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
1 x Continental Motors IO-520 engine |
Over 33,000 lbs (147 kN) |
thrust per engine |
Approximately 300 hp |
66,000 lbs (294 kN) |
total thrust |
Approximately 300 hp |
97,000 kg |
213,800 lb |
MTOW |
3,100 lb |
1,406 kg |
7,400 km |
4,000 nm |
range |
1,111 km |
600 nm |
832 km/h |
517 mph |
cruise speed |
190 mph |
306 km/h |
180-220 passengers |
capacity |
Pilot and one passenger |
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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.