Cessna U206G Stationair 6

C206 · Airplane · model reference data — adjust with your weighing record

Cessna U206G Stationair 6—

	kg	CG
TO	—	—	—
LD	—	—	—
ZF	—	—	—

Result · envelope

—

	Weight kg	CG in
TO	—	—	—
LD	—	—	—
ZF	—	—	—

MAX GROSS 1,633 kg (3,600 lb)

TO takeoff (fuel loaded) · LD landing (after burn) · ZF zero fuel.

X axis: CG (in) · Y: weight (kg) · red line = MTOW.

Load

Front seats 0 kg

Middle seats 0 kg

Rear seats 0 kg

Baggage 0 kg

Fuel 0 L / 223

Flight time 35 min

Total: — LEndurance: —Reserve: —

60 L/h

⚠ Empty weight / CG — model placeholder, tap to set yours

Empty (lb)

Empty CG (in)

These are generic model reference figures and will differ from your specific airframe (equipment, avionics, paint). Enter the empty weight and CG from your aircraft's actual weighing record (lb/in, per the POH) before relying on any result — saved on this device.

Performance · density altitude

Elevation 2300 ft

QNH 1013 hPa · 29.92 inHg

OAT 20 °C

Press. Alt: — ftDA: — ft

Density altitude stretches your takeoff roll and cuts climb rate. Check the takeoff/climb tables in your POH for the current DA and weight — this tool doesn't replace them.