500U
Specifications
Dimensions
| Wing span | 49.05' | 14.95m |
| Length (1755 thru 1876) | 35.10′ | 10.70m |
| Length (3050 thru 3075) | 36.60 | 11.15m |
| Height (1755 thru 3075) | 14.6′ | 4.41m |
| Height (3076 and Subsequent) | 14.8′ | 4.47m |
| Tread | 12.91′ | 3.93m |
| Cabin Door (Aft) | 2.33' x 3.75' | .71m x 1.14 |
| Cabin Door (Fwd) | 1.91' x 3.83' | .58m x 1.16 |
| Cabin Height (Inside Interior) | 4.41′ | 1.34m |
| Cabin Length | 10.62′ | 3.23m |
| Cabin Width (Inside Interior) | 4.33′ | 1.32m |
| 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 |
Propellers
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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 |
