PA-28-181 Weight and Balance Calculator
This table includes key data points that pilots need to know for weight and balance calculations:
| Parameter | Value |
|---|---|
| Empty Weight | 1551.4 – 1658 lbs |
| Max Takeoff Weight (MTOW) | 2550 lbs |
| Max Landing Weight | 2550 lbs |
| Useful Load | 998.6 – 1134 lbs |
| Fuel Capacity | 48 gallons |
| Payload with Full Fuel | 510 – 637 lbs |
| Max Payload | 798 lbs |
| Crew | 1 |
| Passengers | 3 |
| Front Seats Arm | 80.5 inches |
| Rear Seats Arm | 118.1 inches |
| Fuel Arm | 95.0 inches |
| Baggage Arm | 142.8 inches |
| CG Forward Limit (up to 2050 lbs) | 82.0 inches |
| CG Aft Limit | 93.0 inches |
| CG Forward Limit (at 2550 lbs) | 88.5 inches |
It’s important to note that these values may vary slightly between different PA-28-181 aircraft and their specific configurations1234. Pilots should always refer to the official Pilot’s Operating Handbook (POH) for their specific aircraft and perform accurate weight and balance calculations before each flight.
| Item | Weight (lbs) |
|---|---|
| Pilot and passengers | 600 |
| Fuel (avgas) | 48 gallons |
| Baggage (behind seats) | 100 |
| Total Basic Empty Weight | 1,460 |
| Total Useful Load | 940 |
| Max Gross Weight | 2,400 |
| Moment Arm | Variable |