Model 560E was certified on February 21, 1957, under the following certification basis: CAR. 3, November 1, 1945, Amendment 12, May 18, 1954, and 3.431 May 15, 1956. This aircraft is the same as the 560A model except for the 32-inches added to the wing tips, the increase in gross from 6000 pounds to 6500 pounds and Lycoming enginesG0-480-C1B6. (295HP)
Note: All Specifications & Performances Data provided below are for Reference Only. See Piston Commander 560E TCDS, POH/AFM, & ICA's for Model & S/N specific Specification & Performance Data.
Specification Performance Kit Finder| Wing span | 49.56' | 15.10m |
| Length | 35.12′ | 10.70m |
| 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′ | 1.04m |
| Baggage compartment width | 3.91′ | 1.19m |
| Baggage compartment length | 2.58′ | 0.78m |
| Baggage compartment volume | 32 ft³ | 9.75m³ |
| Baggage door height | 1.95′ | 0.59m |
| Baggage door width | 1.62′ | 0.49m |
| Baggage compartment load limit | 350 lbs | 158 kg |
HC-83x20-2C/8833-2 (3 blade)
Lycoming GO480-C1D6/-G1B6
| Max Ramp Weight: | 6500 lbs / 2948 kg |
| Take-off Weight: | 6500 lbs / 2948 kg |
| Landing Weight: | 6500 lbs / 2948 kg |
| Standard Empty Weight: | 4200 lbs / 1905 kg |
| Useful Load: | 2300 lbs / 1043 kg |
| Normal Cruise Speed (@ 70% power @ 10,000 Ft) | 210 mph / 182 kts |
| Twin Engine Best Rate of Climb Speed (CAS): | 120 mph / 104 kts |
| Best rate of Climb Speed | 120 mph / 104 kts |
| Minimum Control Speed (CAS): | 80 mph / 69 kts |
| Stall Speed, Clean (CAS): | 75 mph / 66 kts |
| Stall Speed, Gear and Flaps Down (CAS): | 69 mph / 61 kts |
| Max Range | 1625 SM / 1412 NM |