Piper Lance Weight & Balance Calculator

Piper Lance Weight & Balance

Basic Empty Weight

Item Weight Arm Moment
Empty Weight 163,184

Crew

Pilot 85.5 15,390
Copilot 85.5 0

Passengers

Middle Row 118.1 0
Rear Row 155.7 0

Baggage

Forward 142.8 0
Aft 178.7 0

Fuel

Fuel (gal) 95.0 41,040

Results

Total Weight: 0 lbs

Total Moment: 0 in-lbs

Center of Gravity: 0 inches

Here’s a comprehensive table summarizing the key weight and balance information for the Piper Lance (PA-32R-300):

CategorySpecification
Weights
Max Takeoff Weight3,600 lbs
Max Ramp Weight3,615 lbs
Standard Empty WeightApproximately 2,100 lbs (varies)
Useful LoadApproximately 1,500 lbs
Fuel Capacity102 gallons (612 lbs)
Center of Gravity Limits
Forward Limit78.0 inches at 2,400 lbs and below
83.5 inches at 3,200 lbs
91.4 inches at 3,600 lbs
Aft Limit95.0 inches (all weights)
Moment Arms
Pilot and Front Passenger85.5 inches
Center Seats119.1 inches
Rear Seats157.6 inches
Fuel94.0 inches
Baggage (Forward)42.0 inches
Baggage (Aft)178.7 inches
Baggage Capacity
Forward Compartment100 lbs
Aft Compartment100 lbs
Occupancy
Crew1-2
Passengers4-5
Datum78.4 inches ahead of wing leading edge

When performing weight and balance calculations:

  1. Start with the basic empty weight and moment from the aircraft’s specific weight and balance data.
  2. Add the weight and moment of crew, passengers, fuel, and baggage.
  3. Ensure the total weight does not exceed the max takeoff weight of 3,600 lbs.
  4. Calculate the center of gravity (CG) by dividing the total moment by the total weight.
  5. Verify that the CG falls within the approved range for the calculated weight.
  6. Remember to account for fuel burn during the flight, which will affect both weight and CG.

Always use the specific weight and balance information provided in the aircraft’s Pilot’s Operating Handbook for accurate calculations. The CG limits vary with weight, so be sure to check the envelope graph in the POH.

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