| Manufacturer | Piasecki |
| Model | CH-16 Transporter |
| Modification | YН-16A |
| Country | USA |
| Years | 1953 |
| Type | Transport helicopter |
| Main rotor diameter | 25.00 m |
| Tail rotor diameter | - |
| Wingspan | - |
| Length | 40.80 m |
| Height | 7.62 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 10208 kg |
| Maximum takeoff weight | 14500 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 Allison YT38-A-10 |
| Power | 2 x 2650 HP |
| Thrust | - |
| Maximum speed | 235 km/h |
| Cruising speed | 215 km/h |
| Rate of climb | - |
| Practical range | 370 km |
| Service ceiling | 5500 m |
| Hovering ceiling | - |
| Crew | 2 |
