WBcalc > Cessna > Cessna 172N Skyhawk
Use this calculator to check loaded weight and center of gravity for the Cessna 172N Skyhawk. Enter the current empty weight and empty arm from the aircraft weight and balance record for the individual aircraft.
Maximum takeoff weight: 2,300 lbs. Maximum landing weight: 2,300 lbs. Usable fuel: 40 US gal.
| Specification | Value |
|---|---|
| Maximum takeoff weight | 2,300 lbs |
| Maximum landing weight | 2,300 lbs |
| Forward CG at 1,950 lbs or less | 35.0 in |
| Forward CG at 2,300 lbs | 38.5 in |
| Aft CG limit | 47.3 in |
| Usable fuel | 40 US gal |
| Fuel arm | 48.0 in |
| Maximum combined baggage | 120 lbs |
Source: 1978 Cessna Model 172N Pilot's Operating Handbook, Sections 2 and 6, normal category.
| Aircraft weight | Forward CG limit | Aft CG limit |
|---|---|---|
| 1,950 lbs | 35 in | 47.3 in |
| 2,300 lbs | 38.5 in | 47.3 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 | 37 in | |
| Rear passengers | 73 in | |
| Baggage area 1 | 95 in | 120 lbs |
| Baggage area 2 | 123 in | 50 lbs |
This calculator uses 40 US gallons of usable fuel at an arm of 48.0 inches.
Baggage area 1 is limited to 120 lbs, baggage area 2 to 50 lbs, and combined baggage must not exceed 120 lbs.
The CG envelope on this page is for the normal category.
1978 Cessna Model 172N Pilot's Operating Handbook, Sections 2 and 6, normal category.
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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