Airbus A340-200 vs. N. American T-28 Trojan
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Airbus A340-200 |
versus |
N. American T-28 Trojan |
59.4 m |
194 ft 11 in |
length |
10.06 m |
33 ft 0 in |
16.8 m |
55 ft 1 in |
height |
3.86 m |
12 ft 8 in |
60.3 m |
197 ft 9 in |
wingspan |
12.22 m |
40 ft 1 in |
4 x CFM International CFM56-5C4 |
engines |
1 x Wright R-1820-86 Cyclone radial engine |
34,000 lbf |
thrust per engine |
Approximately 1,425 hp |
136,000 lbf |
total thrust |
Approximately 1,425 hp |
275,000 kg |
606,300 lb |
MTOW |
8,500 lb |
3,856 kg |
12,400 km |
6,699 nm |
range |
1,705 km |
921 nm |
880 km/h |
547 mph |
cruise speed |
210 mph |
338 km/h |
Typical seating 3-class 210-250 |
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.