The 500B is the same as the Model 500A except the gross weight changed from 6250 pounds to 6750 pounds and the engines from a Continental IO470-M to a Lycoming IO540-B1A5. Plus, the Pilot entrance door was added as a customer option. The 500B was Certified on July 13, 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 |
Numerous Hartzell HC (3 blades)
Lycoming IO-540-B1A5 / -B1C5 / -E1A5 / -E1B5
Ramp Weight: | 6750 lbs./3062 Kg |
Take-off Weight: | 6750 lbs./3062 Kg |
Landing Weight: | x,xxx lbs/x,xxx kg |
Standard Empty Weight: | 4300 lbs./1950 Kg |
Useful Load: | 2425 lbs./1099.5Kg |
Zero Fuel Weight: | x,xxx lbs/x,xxx kg |
Baggage: | xxx lbs/xxx kg |
Cruise Speed (@ 70% Power @ 10,000 Ft) | 218 MPH / 189 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) | 68 MPH / 59 KTS |
Range (@ 55% power, 30 Min Reserve) | 1305 SM / 1134 NM |
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