| ENGINE | Lycoming Model IO-36-A1B, direct drive, air cooled, 4 cylinder, 200 h.p. fuel injected at 2700 r.p.m. |
| PROPELLER | Hartzell compact model 74 inch diameter, constant speed, (variable pitch) |
| WEIGHTS | Gross weight .............................................2,600.00 lbs. Empty weight ............................................1,652.60 lbs. Useful load .................................................947.40 lbs. Empty weight center of gravity.................111.37 in Empty weight moment ..............................184,055.39 |
| FUEL | Main tank 40 gal ........................................240 lbs. 100/130 octane |
| OIL | 8 quarts, SAE-50 (included in empty weight) |
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