Airbus A310-300 vs. Avro 652 Anson
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Airbus A310-300 |
versus |
Avro 652 Anson |
46.66 m |
153 ft 1 in |
length |
12.88 m |
42 ft 3 in |
15.8 m |
51 ft 10 in |
height |
2.9 m |
9 ft 6 in |
43.9 m |
144 ft |
wingspan |
17.22 m |
56 ft 6 in |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
2 × Armstrong Siddeley Cheetah VI |
52,000 lb |
thrust per engine |
290 hp (220 kW) |
104,000 lb |
total thrust |
580 hp (440 kW) |
148,768 kg |
328,000 lb |
MTOW |
7,500 lb |
3,402 kg |
8,050 km |
4,348 nm |
range |
1,267 km |
684 nm |
482 knots |
279 mph |
cruise speed |
165 mph |
266 km/h |
190-230 passengers |
capacity |
4 passengers |
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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.