Airbus A300-600 vs. N. American T-28 Trojan
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Airbus A300-600 |
versus |
N. American T-28 Trojan |
54.10 m |
177 ft 6 in |
length |
10.06 m |
33 ft 0 in |
16.5 m |
54 ft 2 in |
height |
3.86 m |
12 ft 8 in |
44.84 m |
147 ft 1 in |
wingspan |
12.22 m |
40 ft 1 in |
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 |
engines |
1 x Wright R-1820-86 Cyclone radial engine |
56,000lb to 61,500lb |
thrust per engine |
Approximately 1,425 hp |
112,000–123,000 lb |
total thrust |
Approximately 1,425 hp |
171,700 kg |
378,600 lb |
MTOW |
8,500 lb |
3,856 kg |
7,500 km |
4,052 nm |
range |
1,705 km |
921 nm |
897 km/h |
557 mph |
cruise speed |
210 mph |
338 km/h |
210-250 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.