Airbus A310-300 vs. Bell 206
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Airbus A310-300 |
versus |
Bell 206 |
46.66 m |
153 ft 1 in |
length |
12.11 m |
39 ft 9 in |
15.8 m |
51 ft 10 in |
height |
2.88 m |
9 ft 5 in |
43.9 m |
144 ft |
wingspan |
|
|
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
1 × Allison 250-C20B |
52,000 lb |
thrust per engine |
420 shp (313 kW) |
104,000 lb |
total thrust |
420 shp (313 kW) |
148,768 kg |
328,000 lb |
MTOW |
1,451 kg |
3,199 lb |
8,050 km |
4,348 nm |
range |
374 km |
202 nm |
482 knots |
279 mph |
cruise speed |
222 km/h |
138 mph |
190-230 passengers |
capacity |
1 pilot + 4 passengers |
|
|
rotor diameter |
11.00 m |
36 ft 1 in |
|
|
rate of climb |
425 m/min |
1,395 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.