Airbus A310-300 vs. N. American T-28 Trojan
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Airbus A310-300 |
versus |
N. American T-28 Trojan |
46.66 m |
153 ft 1 in |
length |
10.06 m |
33 ft 0 in |
15.8 m |
51 ft 10 in |
height |
3.86 m |
12 ft 8 in |
43.9 m |
144 ft |
wingspan |
12.22 m |
40 ft 1 in |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
1 x Wright R-1820-86 Cyclone radial engine |
52,000 lb |
thrust per engine |
Approximately 1,425 hp |
104,000 lb |
total thrust |
Approximately 1,425 hp |
148,768 kg |
328,000 lb |
MTOW |
8,500 lb |
3,856 kg |
8,050 km |
4,348 nm |
range |
1,705 km |
921 nm |
482 knots |
279 mph |
cruise speed |
210 mph |
338 km/h |
190-230 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.