PA-28 Weight and Balance Calculator

PA-28 Weight and Balance Calculator

Here’s a comprehensive table for the weight and balance data of a Piper PA-28, which includes various models like the PA-28-140, PA-28-180, and PA-28R-200. Please note that specific numbers can vary based on the model and configuration, so always refer to the Pilot Operating Handbook (POH) for the specific aircraft in question.

Piper PA-28 Weight and Balance Table

ItemPA-28-140PA-28-180PA-28R-200
Maximum Takeoff Weight (MTOW)2,400 lbs2,550 lbs2,650 lbs
Maximum Useful Load1,040 lbs1,150 lbs1,190 lbs
Empty Weight1,360 lbs1,400 lbs1,460 lbs
Fuel Capacity50 gallons50 gallons50 gallons
Weight of Full Fuel300 lbs300 lbs300 lbs
Payload with Full Fuel740 lbs850 lbs890 lbs
CG Range (Forward)35.0 in35.0 in35.0 in
CG Range (Aft)47.0 in47.0 in47.0 in
Ballast Required (if applicable)VariesVariesVaries

Additional Considerations

  • Weight and Balance Calculations: Always calculate the weight and center of gravity (CG) based on the specific load, including passengers, baggage, and fuel.
  • Loading Graph: Refer to the loading graph in the POH to ensure that the aircraft is loaded within CG limits.
  • Aircraft Configuration: The configuration of the aircraft (e.g., whether it has optional equipment) can affect the empty weight and CG.
  • Weight Increment Adjustments: Make sure to account for any equipment modifications or alterations that may affect weight or balance.

Sample Weight and Balance Calculation

For a PA-28-140:

  • Empty Weight: 1,360 lbs
  • Fuel (full): 300 lbs
  • Pilot: 180 lbs
  • Passenger: 150 lbs
  • Baggage: 50 lbs

Total Weight Calculation:

  • Total Weight = Empty Weight + Fuel + Pilot + Passenger + Baggage
  • Total Weight = 1,360 lbs + 300 lbs + 180 lbs + 150 lbs + 50 lbs = 2,040 lbs

CG Calculation:

  • Use the specific arm measurements provided in the POH to calculate the center of gravity based on your loading configuration.

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