Airbus A330-300 vs. North American T-6 Texan
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Airbus A330-300 |
versus |
North American T-6 Texan |
63.66 m |
208 ft 9 in |
length |
9.0 m |
29 ft 6 in |
16.79 m |
55 ft 1 in |
height |
3.56 m |
11 ft 8 in |
60.3 m |
197 ft 9 in |
wingspan |
12.8 m |
42 ft |
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 |
engines |
1 x Pratt & Whitney R-1340-AN-1 radial engine |
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) |
thrust per engine |
Approximately 600 hp |
Depends on the engine type |
total thrust |
Approximately 600 hp |
242,000 kg |
533,600 lb |
MTOW |
5,617 lb |
2,548 kg |
11,750 km |
6,346 nm |
range |
1,175 km |
634 nm |
900 km/h |
559 mph |
cruise speed |
145 mph |
233 km/h |
250-290 |
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.