Cessna 152

C152 · Airplane · model reference data — adjust with your weighing record

Result · envelope

—

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

MAX GROSS 758 kg (1,670 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

Baggage 1 0 kg

Baggage 2 0 kg

Fuel (usable) 0 L / 93

Flight time 35 min

Total: — LEndurance: —Reserve: —

22 L/h

Empty weight / CG (weighing record)

Empty (lb)

Empty CG (in)

Set these from your aircraft's weighing record — 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.

TO—kg—