850Kg / 1870lbs

Engine Type

Textron Lycoming IO-360MI-A
4 cylinders 180BHP at 2700 rpm.
Fuel injected, air-cooled, horizontally-opposed

Propeller Type

Hartezell Propeller HC-C2YR-1BFP/F7497 Alum,ni 2-blades, constant speed unit.

Fuel Capacity

20.6 USG each tank, 0.5 USG unuseable in each tank.

Fuel Grade

Min 100LL

Oil Capacity

MAx 8 Quarts.
Minimum 4 Quarts / 6 Quartz for IFR

Electrical Supply

28VDC 70A alternator
24VDC 11A/hr battery

TAKE OFF / LANDING RUN

TAKE-OFF RUN (FLAPS T/O) 1280ft

LANDING RUN (FLAPS LDG) 1120ft

Maximum take-off weight

1200 Kg (Normal) / 980Kg (Ultilty)

Maximum Landing Weight

1150Kg

RPM

500 - 2400RPM (Normal) / 2700RPM continuous / 2700RPM (Red Band)

Manifold Pressure

13 - 30inHG (Greeen Band)

Cylinder Head Pressure

150 - 475 deg (Normal)/ 500 deg (Red Band)

Oil Temperature

149 - 230 deg F (Normal) / 245 deg F (Red Line)

Oil Pressure

25 - 95 PSI / 98PSI (Max)