AIRFRAME / TOTAL LANDINGS / ENGINES / APU / WEIGHT
ENGINES
Engine: Lycoming O-360-A4A, 180 hp
TBO 2000 hr or 12 years recommended
812 SMOH completed in May 1991
last leak test: 66/70/64/64 of 80 psi
Propeller: Sensenich 76EM8S5-0-60, 2-blade
TBO 2000 hours
812 SPOH completed in May 1991
WEIGHTS
Weights & Balance: BEM 746 kg @ 222,69 cm
MTOM 1112 kg