Airbus A350-900ULR vs. N. American T-28 Trojan
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Airbus A350-900ULR |
versus |
N. American T-28 Trojan |
66.80 m |
219 ft 2 in |
length |
10.06 m |
33 ft 0 in |
17.05 m |
55 ft 11 in |
height |
3.86 m |
12 ft 8 in |
64.75 m |
212 ft 5 in |
wingspan |
12.22 m |
40 ft 1 in |
2 Rolls-Royce Trent XWB |
engines |
1 x Wright R-1820-86 Cyclone radial engine |
84,000 lbs |
thrust per engine |
Approximately 1,425 hp |
168,000 lbs |
total thrust |
Approximately 1,425 hp |
280,000 kg |
617,300 lb |
MTOW |
8,500 lb |
3,856 kg |
17,964 km |
9,700 nm |
range |
1,705 km |
921 nm |
552 mph |
888 km/h |
cruise speed |
210 mph |
338 km/h |
300-350 passengers in three classes |
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.