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| One prototype, first flown on 29 March 1934. No production.
 | A three-view drawing (680 x 590) |
| CREW | 2-3 |
| ENGINE | 1 x 750hp Armstrong Siddeley Tiger IV |
| WEIGHTS |
| Take-off weight | 3991 kg | 8799 lb |
| Empty weight | 3172 kg | 6993 lb |
| DIMENSIONS |
| Wingspan | 16.15 m | 53 ft 0 in |
| Length | 12.45 m | 41 ft 10 in |
| Height | 4.78 m | 16 ft 8 in |
| Wing area | 61.13 m2 | 658.00 sq ft |
| PERFORMANCE |
| Max. speed | 253 km/h | 157 mph |
| Ceiling | 7071 m | 23200 ft |
| ARMAMENT | 2 x 7.7mm machine-guns, 1 x 450kg or 3 x 227kg bombs or a torpedo |
| Klaatu83, e-mail, 09.04.2016 00:50 prototype built to satisfy an Air Ministry requirement for a "General Purpose" aircraft for the RAF. The specification was for an aircraft designed to meet so many different requirements that it was virtually impossible to satisfy and, in the end, none of the designs that were submitted were accepted. reply |
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