| Crop Duster N5A |
| Light Passenger/Cargo Y-5B LE-500 Y-12 Y-8 |
| Trainer PT6 K8 |
| Ultra Light AD-200 Airship |
| Helicopters Z9A MD-500E MD-520N MD-530F MD-600N |
Y-12
Manufacturer: Hafei Aviation Industry Co., Ltd.
Y12 light general-purpose aircraft was designed in accordance with the US Federal Airworthiness Regulations FAR23 and FAR135 Appendix A. It is equipped with two Pratt & Whitney Canada PT6A-27 turboprop engines, installed with Hartzell 3-blade metallic propellers that can rotate at a constant speed and operate in reverse and feathering modes. The blades also have electrical heating. The electrics for the power plant and engine instruments are imported products. In general, Y12 features: |
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| Main Technical Specifications: | Y12II | Y12IV |
| Full Length | 14.86m | 14.86m |
| Full Height | 5.675m | 5.675m |
| Wing Span | 17.235m | 19.2m |
| Max. Takeoff Weight | 5300kg | 5670kg |
| Max. Landing Weight | 5300kg | 5400kg |
| Max. Fuel Capacity | 1230kg | 1230kg |
| Payload | 1700kg | 1984kg |
| Max. Level Flight Speed | 328 km/h | 325km/h |
| Economic Cruising Speed | 250-260km/h | 250-260km/h |
| Max. Range | 1340km | 1300km |
| With 45 minutes reserve) | ||
| Takeoff Distance | 420m | 490m |
| Landing Distance | 620m | 630m |
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