You Decide
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Performance
Specification
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| ENGINE |
| Manufacturer | Teledyne Continental |
| Model | TSI0-360-RB and L/TSI0-360-RB |
| Horsepower | 220 |
| Number of Cylinders | 6 |
| PROPELLER |
| Manufacturer | Hartzell |
| Number of Blades | 2 |
| Type | Consistent Speed, Full Feathering |
| WEIGHTS |
| Maximum Takeoff Weight | 4750 lbs/2155 kg |
| Standard Empty Equipped Weight (b and c) | 3413 lbs/1548 kg |
| Standard Useful Load (a) | 1337 lbs/606 kg |
| FUEL AND OIL CAPACITY |
| Usable Fuel | 122 gal/462 liters |
| Oil Capacity | 8 qts/7.61 |
| MAXIMUM SPEED | TAS |
| Gross Weight @ (18,500 ft) | 218 kts/404 km/h |
| CRUISING SPEEDS | TAS |
|
kts/km/h ............... kts/km/h @10,000 ft.......... @18,500 ft |
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| Max Cruise Power | 182/337 ............... 197/365 |
| Normal Cruise Power | 176/326 ............... 190/351 |
| CRUISING RANGE |
| Long Range Cruise Power (@10,000 ft) | 812 nm/1504 km |
| Long Range Cruise Power (@15,000 ft) | 828 nm/1533 km |
| Long Range Cruise Power (@18,500 ft) | 819 nm/1517 km |
| TAKEOFF DISTANCE |
| Ground Roll | 1,143 ft/348 m |
| Total over 50 ft obstacle | 1,707 ft/520 m |
| LANDING DISTANCE |
| Ground Roll | 1400 ft/427 m |
| Total over 50 ft obstacle | 2180 ft/664 m |
(a) Standard useful load is the maximum takeoff weight minus the standard equipped weight.
(b) The standard empty weight and the standard equipped weight are the same.
(c) Standard equipped aircraft.
You Decide Intro
Decision-Making Process
You Decide Scenario