The Model 500A is the same as the Model 500 with the following exceptions: The Wing structure modification in nacelle area, Fuel injection engines (Continental IO470-M), Hydraulic system modifications, Redesign of Cowling and Nacelle, New landing gear, and Gross weight increased from 6000 to 6250 pounds. The 500A was certified on April 7, 1960.
Note: All Specifications & Performances Data provided below are for Reference Only. See Piston Commander 500A TCDS, POH/AFM, & ICA's for Model & S/N specific Specification & Performance Data.
Specification Performance Kit Finder| Wing span | 49.04' | 14.95m |
| Length | 35.10′ | 10.70m |
| Height | 14.5′ | 4.42m |
| Tread | 12.91′ | 3.93m |
| Cabin Entry Door | 2.33' x 3.58' | .71m x 1.09 |
| Cabin Height (Inside Interior) | 4.41′ | 1.34m |
| Cabin Length | 10.62′ | 3.23m |
| Cabin Width | 4.33” | 1.32m |
| Cabin Width (Inside Interior) | 2.33′ | .71m |
| Cabin Volume | 177 ft³ | 53.9m³ |
| Baggage compartment height | 3.41′ | 1.03m |
| Baggage compartment width | 3.91′ | 1.19m |
| Baggage compartment length | 2.58′ | .78m |
| Baggage compartment volume | 32 ft³ | 9.75m³ |
| Baggage door height | 1.91′ | .58m |
| Baggage door width | 1.58′ | .48m |
| Baggage compartment load limit | 350 lbs | 158 kg |
Hartzell HC A2XF-2B/8433-4 (2 blades)
Lycoming IO-470-M
| Ramp Weight: | 6250 lbs / 2835 kg |
| Take-off Weight: | 6250 lbs / 2835 kg |
| Landing Weight: | 6250 lbs / 2835 kg |
| Dry Empty Weight: | 4255 lbs /1930 kg |
| Useful Load: | 1950 lbs / 884.5 kg |
| Cruise Speed (@ 70% Power @ 10,000 Ft) | 217 mph / 188.5 kts |
| Cruise Speed (@ 75% Power @ 5,000 Ft) | 204 mph / 177 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): | 70 mph / 61 kts |
| Stall Speed, Clean (CAS): | 72 mph / 63 kts |
| Stall Speed, Gear and Flaps Down (CAS): | 66 mph / 57 kts |
| Stall Speed (Dirty) | 66 mph / 57 kts |
| Range (@ 45% power, TAS 181, 30 Min Reserve) | 1800 SM / 1564 NM |