| Engine: |
1 x Lycoming IO-360-C1C |
| Propeller: |
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| Electrical Supply |
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| Normal cruise: |
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| Maximum Weight: |
2650 lbs |
| Basic Empty Weight: |
1655 lbs |
| Useful Load |
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| Fuel capacity: |
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| Fuel flow rate @ 75% power |
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| Oil Capacity: |
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Airspeed Limitations
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| Never exceed speed (Vne): |
193 kt / 222 mph |
| Maximum structual crusing speed (Vno): |
152 kt / 175 mph |
| Maximum Flap extension speed (Vfe): |
152 kt / 175 mph |
| Manoeuvring speed (Va): |
115 kt / 132 mph |
| Maximum crosswind: |
17 kt |
| Stall speeds (0 deg angle of bank): |
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Normal Operation
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| Take-off Performance - Ground Roll: |
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| Take-off Performance to 50 ft: |
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| Landing Performance - Ground Roll: |
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| Landing Performance from 50 ft: |
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| Rate of climb at sea level: |
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| Service Ceiling: |
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| Take-off safety speed: |
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| Best rate of climb speed (Vy): |
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| Best angle of climb (Vx): |
69 kt / 80 mph |
| Cruise climb speed: |
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| Best glide speed (gear up): |
92 kt / 105 mph |
| Base approach speed: |
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Final approach short-field: |
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