| Year |
2003 |
| Engine |
Lycoming IO-360-M1A |
| Horsepower |
|
| Oil Capacity |
X qts |
| Propeller |
3 Blade MT Propeller |
| Useable Fuel |
X gal (out of X) |
| Cruise Speed (2,000') |
X mph, 118 KTAS @75% pwr |
| Cruise Speed (8,000') |
X mph, 130 KTAS @full pwr |
| Cruise Range |
X nm @65% power |
| Climb Rate (SL) |
X fpm |
| Max Demonstrated X-Wind |
X kts |
Takeoff Distance (SL, std
temp, gross wt, no flaps) |
X'; ' X 50' obstacle |
| Landing Distance (SL, std temp, gross wt, full flaps) |
X' X over 50' obstacle |
| Stall Speed |
x KIAS full flaps |
| Max Weight |
lbs |
| Empty Weight |
lbs |
| Empty Weight C. G. (Arm) |
Lateral CG |
| Gross Weight |
|
| Useful Load |
|
