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 (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 |
80" 2-blade
Continental I0-470-M | Rating - 260@ 2625 RPM | Fuel, octane, capacity GAL - 100/130 - 156 | Fuel Consumption GPH - 8.5
Ramp Weight: | xx,xxx lbs/x,xxx kg |
Take-off Weight: | x,xxx lbs/x,xxx kg |
Landing Weight: | x,xxx lbs/x,xxx kg |
Standard Empty Weight: | 4075 lbs/x,xxx kg |
Useful Load: | x,xxx lbs/x,xxx kg |
Zero Fuel Weight: | x,xxx lbs/x,xxx kg |
Baggage: | xxx lbs/xxx kg |
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 |
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