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Twin-engined light transport aircraft with accommodation for five to eight persons. The first prototype flew on 15 August 1961, powered by a Continental 194kW IO-470-A engine, and was smaller than subsequent B.206. The second prototype had increased dimensions and a 231kW Rolls-Royce/Continental GIO-470-A engine. The initial commercial version was the B.206 Series I or B.206C. The B.206R was the military production version, ordered for communications and ferrying duties with the RAF under the name Basset CC.l. The B.206-S was a development of the Series I with supercharged engines and other refinements. Deliveries included two ambulance models for the Royal Flying Doctor Service of New South Wales, Australia. By the close of 1969 40 B.206 Series I and II aircraft, 20 Bassets and two B.206Z pre-production types for the Ministry of Technology had been delivered.
| CREW | 1 |
| PASSENGERS | 4-7 |
| ENGINE | 2 x RR/Cont. GIO-470, 230kW |
| WEIGHTS |
| Take-off weight | 3223 kg | 7106 lb |
| Empty weight | 1978 kg | 4361 lb |
| DIMENSIONS |
| Wingspan | 13.9 m | 45 ft 7 in |
| Length | 10.3 m | 33 ft 10 in |
| Height | 3.4 m | 11 ft 2 in |
| Wing area | 19.9 m2 | 214.20 sq ft |
| PERFORMANCE |
| Max. speed | 352 km/h | 219 mph |
| Cruise speed | 348 km/h | 216 mph |
| Ceiling | 6210 m | 20350 ft |
| Range | 1500 km | 932 miles |
| Range w/max.fuel | 3000 km | 1864 miles |
| Range w/max.payload | 1850 km | 1150 miles |
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