Use this calculator to check loaded weight and center of gravity for the Cessna 152. Enter the current empty weight and empty arm from the aircraft weight and balance record for the individual aircraft.
Maximum takeoff weight: 1,670 lbs. Maximum landing weight: 1,670 lbs. Usable fuel: 24.5 US gal.
| Specification | Value |
|---|---|
| Maximum takeoff weight | 1,670 lbs |
| Maximum landing weight | 1,670 lbs |
| Forward CG at 1,350 lbs or less | 31.0 in |
| Forward CG at 1,670 lbs | 32.65 in |
| Aft CG limit | 36.5 in |
| Standard usable fuel | 24.5 US gal |
| Long range usable fuel | 37.5 US gal |
| Standard tank fuel arm | 42.0 in |
| Long range tank fuel arm | 39.5 in |
| Maximum combined baggage | 120 lbs |
Source: 1979 Cessna Model 152 Pilot's Operating Handbook, Sections 1, 2 and 6.
| Aircraft weight | Forward CG limit | Aft CG limit |
|---|---|---|
| 1,350 lbs | 31 in | 36.5 in |
| 1,670 lbs | 32.65 in | 36.5 in |
The calculator uses the published CG envelope points and linear interpolation between forward-limit breakpoints where applicable.
| Station | Arm | Limit |
|---|---|---|
| Pilot and front passenger | 39 in | |
| Baggage area 1 | 64 in | 120 lbs |
| Baggage area 2 | 84 in | 40 lbs |
Standard tanks provide 24.5 US gallons usable. Long range tanks provide 37.5 US gallons usable.
The standard and long range fuel systems use different arms: 42.0 inches and 39.5 inches respectively.
Baggage area 1 is limited to 120 lbs, baggage area 2 to 40 lbs, and combined baggage must not exceed 120 lbs.
1979 Cessna Model 152 Pilot's Operating Handbook, Sections 1, 2 and 6.
WBcalc is a planning aid. Check the current POH or AFM, aircraft weight and balance record, equipment list and applicable supplements before flight.
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