Use this calculator to check loaded weight and center of gravity for the Cessna 150M. Enter the current empty weight and empty arm from the aircraft weight and balance record for the individual aircraft.
Maximum takeoff weight: 1,600 lbs. Maximum landing weight: 1,600 lbs. Usable fuel: 22.5 US gal.
| Specification | Value |
|---|---|
| Maximum takeoff weight | 1,600 lbs |
| Maximum landing weight | 1,600 lbs |
| Forward CG at 1,280 lbs or less | 31.5 in |
| Forward CG at 1,600 lbs | 32.9 in |
| Aft CG limit | 37.5 in |
| Standard usable fuel | 22.5 US gal |
| Long range usable fuel | 35 US gal |
| Fuel arm | 42.2 in |
| Maximum combined baggage | 120 lbs |
| Reference datum | Front face of firewall |
Source: 1977 Cessna Model 150M Pilot's Operating Handbook, Sections 2 and 6.
| Aircraft weight | Forward CG limit | Aft CG limit |
|---|---|---|
| 1,280 lbs | 31.5 in | 37.5 in |
| 1,600 lbs | 32.9 in | 37.5 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 usable fuel is 22.5 US gallons. Long range usable fuel is 35 US gallons.
Baggage area 1 is limited to 120 lbs, baggage area 2 to 40 lbs, and the combined baggage load must not exceed 120 lbs.
The published standard empty weight is a reference only. Use the current aircraft weight and balance record for the individual airplane.
1977 Cessna Model 150M Pilot's Operating Handbook, Sections 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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