WBcalc > Piper > Piper PA-28-161 Warrior II
Use this calculator to check loaded weight and center of gravity for the Piper PA-28-161 Warrior II. Enter the current empty weight and empty arm from the aircraft weight and balance record for the individual aircraft.
Maximum takeoff weight: 2,325 lbs. Maximum landing weight: 2,325 lbs. Usable fuel: 48 US gal.
| Specification | Value |
|---|---|
| Maximum takeoff weight | 2,325 lbs |
| Maximum landing weight | 2,325 lbs |
| Forward CG at 1,950 lbs or less | 83.0 in |
| Forward CG at 2,325 lbs | 87.0 in |
| Aft CG limit | 93.0 in |
| Usable fuel | 48 US gal |
| Fuel arm | 95.0 in |
| Baggage limit | 200 lbs |
Source: FAA Type Certificate Data Sheet 2A13, PA-28-161.
| Aircraft weight | Forward CG limit | Aft CG limit |
|---|---|---|
| 1,950 lbs | 83 in | 93 in |
| 2,325 lbs | 87 in | 93 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 | 80.5 in | 400 lbs |
| Rear passengers | 118.1 in | 400 lbs |
| Baggage | 142.8 in | 200 lbs |
This calculator uses 48 US gallons of usable fuel at an arm of 95.0 inches.
The baggage station is at 142.8 inches and the baggage limit used by this calculator is 200 lbs.
FAA Type Certificate Data Sheet 2A13, PA-28-161.
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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