Y-12 Yunshuji-12 - Specifications
| Wingspan | 17.235 meters |
| Length | 14.86 meters |
| Machine height | 5.575 meters |
| Aspect ratio | 8.67 |
| wing area | 34.27 m2 |
| main wheel base | 3.60 meters |
| front main wheel base | 4.698 meters |
| Propeller diameter | 2.489 meters |
| Propeller center distance | 4.934 meters |
| distance between the fuselage and the ground | 0.65 meters |
| cargo door | Height × Width 1.38 meters × 1.45 meters |
| Passenger door | Height × Width 1.38 m × 0.65 m |
| Luggage door | Maximum height 0.69 meters Width 0.75 meters |
| cabin: Length | 4.82 meters |
| Maximum width | 1.8 meters |
| Maximum height | 1.7 meters |
| Total volume | 12.9 m3 |
| Luggage compartment volume | |
| Front luggage compartment | 0.77m3 |
| rear luggage compartment | 1.89 meters 3 |
| Design take-off weight | 5000kg |
| Design landing weight | 5000kg |
| Maximum zero fuel weight | 4700kg |
| Use empty weight | 3000kg |
| Basic empty weight | 2840kg |
| Maximum payload | 1700kg |
| maximum usable oil quantity | 1230 kg |
| Maximum floor load | 7.35 kN/m2 (750 kg/m2) |
| Maximum wing load | 1.47 kN/m2 (150 kg/m2) |
| take-off weight | 5000 kg, international standard atmosphere |
| Maximum level flight speed (altitude 3000 meters) | 328 km/h |
| Cruising speed (altitude 3000 meters) | 240 ~ 250 km/h |
| Maximum rate of climb (sea level) | 9.2 m/s |
| Cruising altitude | 3000 meters |
| ceiling | 7000 meters |
| Single-engine ceiling | 3550 meters |
| minimum turning radius on the ground | 16.75 meters |
| Take-off distance (to 15 meters high) | 385 meters |
| Take-off roll distance | 315 meters |
| Landing distance (from 15 meters high) | |
| Brake | 710 meters |
| Brake, reverse propeller | 480 meters |
| landing roll distance Brake | 510 meters |
| Brake, reverse propeller | 280 meters |
| Range (altitude 3000 meters, 45 minutes of flight use oil) | 1400 kilometers |
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