|
| Prototype flew as SKh-1 31 August 1947. More than 5,000 An-2 were built at Kiev, ending in mid-1960s
after limited manufacture of specialised agricultural An-2M. Production transferred to PZL Mielec, Poland,
from where more than 11,950 delivered since 1960. China acquired licence and has built Yunshuji-5 (Y-5)
versions 1957 to date.
| CREW | 2-3 |
| PASSENGERS | 8-10 |
| ENGINE | 1 x ASh-62IR, 735 kW |
| WEIGHTS |
| Take-off weight | 5450 kg | 12015 lb |
| Empty weight | 3350 kg | 7386 lb |
| DIMENSIONS |
| Wingspan | 18.2/14.2 m | 60 ft 9 in / 47 ft 7 in |
| Length | 12.7 m | 42 ft 8 in |
| Height | 4.1 m | 13 ft 5 in |
| Wing area | 71.4 m2 | 768.54 sq ft |
| PERFORMANCE |
| Max. speed | 250 km/h | 155 mph |
| Cruise speed | 220 km/h | 137 mph |
| Ceiling | 5000 m | 16400 ft |
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Stack trace:
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