Year:
1979
Engine:
Lycoming LIO-360-C1E6 Right engine/ Lycoming IO-360-C1E6 Left engine
Propellers:
Hartzell Model #: HC-C2YK-2E Right / Hartzell Model #:HC-C2YK-2LE Left
Fuel capacity:
98 (U.S. gal)
Useable fuel:
93 (U.S. gal)
Oil capacity:
8 (U.S. quarts) per engine
Maximum Takeoff Weight:
4200 (lbs)
Maximum Landing Weight:
4000 (lbs)
Baggage compartment(Forward):
100 (lbs)
Baggage compartment(aft):
100 (lbs)
