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| Developed as a single-seat fighter for export, powered by an 894.2kW Pratt & Whitney R-1830-53C4-G engine. Most production aircraft, given the USAAF designation P-66, found their way to China from 1940.
| MODEL | P-66 |
| CREW | 1 |
| ENGINE | 1 x Pratt-WHitney R-1830-33 Twin Wasp, 895kW |
| WEIGHTS |
| Take-off weight | 3349 kg | 7383 lb |
| Empty weight | 2375 kg | 5236 lb |
| DIMENSIONS |
| Wingspan | 10.97 m | 36 ft 0 in |
| Length | 8.66 m | 28 ft 5 in |
| Height | 2.87 m | 9 ft 5 in |
| Wing area | 18.3 m2 | 196.98 sq ft |
| PERFORMANCE |
| Max. speed | 547 km/h | 340 mph |
| Ceiling | 8595 m | 28200 ft |
| Range | 1529 km | 950 miles |
| ARMAMENT | 4 x 7.62mm, 2 x 12.7mm machine-guns |
 | A three-view drawing (1280 x 972) |
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