The 560F is the same as the 680F except for gross weight was reduced to 7500 pounds and Lycoming engine IGO540-B1A installed. The 560F was Certified on February 8, 1961.
Specification Performance Kit Finder| Wing span | 49.04' | 14.94m |
| Length | 35.10′ | 10.69m |
| Height | 14.50′ | 4.41m |
| Tread | 12.91′ | 3.93m |
| Cabin Door Height | 3.58' | 1.09m |
| Cabin Door Width | 2.33' | 0.71m |
| Cabin Height (Inside Interior) | 4.41′ | `.34m |
| Cabin Length | 10.62′ | 3.23m |
| Cabin Width (Inside Interior) | 4.33′ | 1.31m |
| Cabin Volume | 177 ft³ | 53.94m³ |
| Baggage compartment height | 3.41′ | x.xxm |
| Baggage compartment width | 3.91′ | 1.03m |
| Baggage compartment length | 2.58′ | 0.78m |
| Baggage compartment volume | 32 ft³ | 9.75m³ |
| Baggage door height | 1.91′ | 0.58m |
| Baggage door width | 1.58′ | 0.48m |
| Baggage compartment load limit | xx lbs | xx kg |
HC-B3Z-30-2B (15)/9349 / HC-B3Z-30-2B-9349-6.5 (3 blade)
Lycoming IGO-540-B1A/-B1C
| Max Ramp Weight: | 7500 lbs./ 3402 Kg |
| Take-off Weight: | 7500 lbs./ 3402 Kg |
| Landing Weight: | x,xxx lbs/x,xxx kg |
| Dry Empty Weight: | 4650 lbs./ 2109 Kg |
| Useful Load: | 2800 lbs./ 1293 Kg |
| Zero Fuel Weight: | x,xxx lbs/x,xxx kg |
| Baggage: | xxx lbs/xxx kg |
| Cruise Speed (@ 70% power @ 10,000 Ft) | 232 MPH / 201 KTS |
| Maximum Cruise | |
| (100% 12,000 ft.TAS@ 10,325 lbs/4,683 kg) | xxxmph/xxxkts |
| Normal Cruise Speed | |
| (96%20,000 ft.TAS@ 10,325 lbs/4,683 kg): | xxxmph/xxxkts |
| Twin Engine Best Rate of Climb Speed (CAS): | xxxmph/xxxkts |
| Twin Engine Best Angle of Climb Speed (CAS): | xxxmph/xxxkts |
| Single Engine Best Rate of Climb Speed (CAS): | xxxmph/xxxkts |
| Single Engine Best Angle of Climb Speed (CAS): | xxxmph/xxxkts |
| Minimum Control Speed (CAS): | xxmph/xxkts |
| Stall Speed, Clean (CAS): | xxmph/xxkts |
| Stall Speed, Gear and Flaps Down (CAS): | xxmph/xxkts |
| Stall Speed (Dirty) | 73.5 MPH / 63.8 KTS |
| Range (@ 50% power, 30 Min Reserve) | 1705 SM / 1481 NM |