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Completed late in 1938 as a company-owned demonstrator,
the Hawk 75-R was essentially similar to the
USAAC's P-36A. Its Pratt & Whitney R-1830-19 (SC2-G)
Twin Wasp was, however, fitted with a turbo-supercharger
mounted beneath the nose, just aft of the
engine cowling, with a ventrally-mounted intercooler. Extensively tested by the USAAC, the Hawk 75-R was
eventually returned to Curtiss as the turbo-supercharger
proved unreliable and the manual monitoring
of the unit was considered impracticable in combat.
The turbo-supercharger was subsequently removed
and the aircraft re-engined with a Cyclone.
| WEIGHTS |
| Take-off weight | 2 795 kg | 4 lb |
| Empty weight | 2 302 kg | 4 lb |
| DIMENSIONS |
| Wingspan | 11.37 m | 37 ft 4 in |
| Length | 8.69 m | 28 ft 6 in |
| Height | 3.71 m | 12 ft 2 in |
| Wing area | 21.92 m2 | 235.94 sq ft |
| PERFORMANCE |
| Max. speed | 531 km/h | 330 mph |
| Range | 966 km | 600 miles |
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