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Envisaged originally as a high-altitude version of the B-25 Mitchell, the North American NA-63 (XB-28) emerged finally as an almost entirely different aircraft. With single vertical tail surfaces and a circular-section fuselage with a pressure cabin for the five-man crew, the XB-28 was powered by two 1491kW Pratt & Whitney R-2800 radials and bomb bay capacity was 1814kg. Dorsal, ventral and tail turrets, each containing two 12.7mm machine-guns, were remotely controlled from the cockpit; three similar forward-firing weapons were also fitted. Of three prototypes ordered in February 1940, the first flew in April 1942, the second was cancelled and the third, with a reconnaissance camera installation, crashed during the test programme. Although the XB-28 achieved a maximum speed of 599km/h at 7620m and could carry a 272kg bomb load for 3283km, production orders were not placed.
 | A three-view drawing (700 x 1053) |
| WEIGHTS |
| Take-off weight | 16226 kg | 35772 lb |
| Empty weight | 11611 kg | 25598 lb |
| DIMENSIONS |
| Wingspan | 22.12 m | 72 ft 7 in |
| Length | 17.20 m | 56 ft 5 in |
| Wing area | 62.80 m2 | 675.97 sq ft |
| PERFORMANCE |
| Cruise speed | 411 km/h | 255 mph |
| Range | 3284 km | 2041 miles |
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