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.
Specification Performance Kit FinderWing 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 | lbs | 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: | x,xxx lbs/x,xxx kg |
Dry Empty Weight: | 4255 lbs. / 1930 Kg |
Useful Load: | 1950 lbs. / 884.5 Kg |
Zero Fuel Weight: | x,xxx lbs/x,xxx kg |
Baggage: | xxx lbs/xxx 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): | 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 |
Best rate of Climb Speed | 120 MPH / 104 KTS |
Minimum Control Speed (CAS): | xxmph/xxkts |
Stall Speed, Clean (CAS): | xxmph/xxkts |
Stall Speed, Gear and Flaps Down (CAS): | xxmph/xxkts |
Stall Speed (Dirty) | 66 MPH / 57 KTS |
Range (@ 45% power, TAS 181, 30 Min Reserve) | 1800 SM / 1564 NM |