T-6A JPATS [Texan II / Harvard II]
| Specifications | |
|---|---|
| Primary Function | All-purpose trainer. |
| Contractor | Hawker Beechcraft Aircraft Company. |
| First flight | July 10, 2009 |
| Operational | April 19, 2010. |
| Average unit cost (TY$) | $5M |
| Length overall | 33 ft 4 in / 10.16 m |
| Wing span | 33 ft 5 in / 10.18 m |
| Height overall | 10 ft 8 in / 3.25 m |
| Wing aspect ratio | 6.29 |
| Maximum internal fuel | 149.0 Imp gal / 677.5 liters |
| Basic weight empty | 4707 lb / 2135 kg |
| Weight | empty, 5,850 pounds (2,653.52 kg.) |
| Design maximum take-off | 6300 lb / 2857 kg |
| maximum takeoff weight | 6,900 pounds (3,129.79 kg.). |
| POWERPLANT |
Pratt & Whitney PT6A-68 turboprop Hartzell four blade propeller Engine rating 1100 SHP (continuous) |
| Airspeed | 270 knots at 1,000 feet level flight. |
| Never exceed speed | 364 mph (316 kn; 586 km/h) 0.48 Mach |
| Ceiling | 31,000 feet (9,448.8 meters). |
| Range | maximum, 850 nautical miles (1,367.91 km). |
| Crew | Two (instructor pilot, student pilot). |
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