Piper Archer Weight and Balance Calculator
Item | Weight (lbs) | Arm (inches) | Moment |
---|---|---|---|
Empty Weight | 86.1 | ||
Pilot/Front Passenger | 80.5 | ||
Rear Passenger | 118.1 | ||
Baggage Area 1 | 142.8 | ||
Baggage Area 2 | 123 | ||
Fuel (in gallons) | 95 |
This table includes all the essential information you need to know:
Item | Value |
---|---|
Max Takeoff Weight | 2550 lbs |
Max Landing Weight | 2550 lbs |
Empty Weight | 1571.86 lbs |
Useful Load | 960 lbs |
CG Range | 82 – 93 inches |
Fuel Weight | 6.01 lbs/gal |
Oil Weight | 1.86 lbs/qt |
Pilot/Front Passenger Arm | 80.5 inches |
Rear Passenger Arm | 118.1 inches |
Baggage Area 1 Arm | 142.8 inches |
Baggage Area 2 Arm | 123 inches |
Additional Information
- The empty weight can vary between individual aircraft. For example, the specific Piper Archer N3016M has an empty weight of 1551.4 lbs, which is slightly different from the general data provided2.
- The useful load is the difference between the maximum takeoff weight and the empty weight. It represents the total weight of fuel, passengers, and cargo that can be carried.
- When performing weight and balance calculations, remember to consider the arm (distance from the datum) for each item. The arms for pilot/front passenger, rear passengers, and baggage areas are provided in the table1.
- Always ensure that the loaded aircraft’s weight does not exceed the maximum takeoff weight and that the center of gravity (CG) falls within the acceptable range throughout the flight1.
- For precise calculations, use the specific empty weight and moment of your particular aircraft, as these can vary slightly between individual planes2.
This table and additional information should provide you with all the essential data needed for weight and balance calculations on a Piper Archer. Always refer to the aircraft’s official documentation for the most accurate and up-to-date information specific to your aircraft.