520
Specifications
Dimensions
| Wing span | 44.0' | 13.41m |
| Length | 34.25′ | 10.43m |
| Height | 14.45′ | 4.40m |
| Tread | 12.4′ | 3.77m |
| Cabin Door (Aft) | x.xx' x x.xx' | .xxm x x.xx |
| Cabin Door (Fwd) | x.xx' x x.xx' | .xxm x x.xx |
| Cabin Height (Inside Interior) | x.xx′ | x.xxm |
| Cabin Length | xx.xx′ xx | x.xxm |
| Cabin Width (Inside Interior) | x.xx′ xx | 1.xxm |
| Cabin Volume | 146 ft³ | 44.5m³ |
| Baggage compartment height | x.xx′ xx | x.xxm |
| Baggage compartment width | x.xx′ | x.xxm |
| Baggage compartment length | x.xx′ | .78m |
| Baggage compartment volume | 32 ft³ | 9.75m³ |
| Baggage door height | x.xx′ xx | .58m |
| Baggage door width | x.xx′ xx | .xxm |
| Baggage compartment load limit | xx lbs | xx kg |
Propellers
xxx
Power Plant
owered by two Lycoming I0-540 Series, 290-horsepower engines, which drive Hartzell 3-blade, constant-speed, full-feathel'.ing prope ll'ers. This engine and propeller combination provJdes sufficient power for optimum aircraft performance to an altitude of 21,000 feet.
Weights - Aircraft
| 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 |
