DA20 Weight and Balance Calculator

Estimate DA20 takeoff weight, landing weight, moments, fuel, and CG. Compare envelope and station limits. Keep loading records clear for every careful preflight plan.

Enter Aircraft Loading Data

Default numbers are sample placeholders. Replace every arm, weight, and limit with values for the exact aircraft.

Example Data Table

Item Sample Weight Sample Arm Sample Moment
Basic empty aircraft 1165 lb 76.50 in 89122.50 lb-in
Pilot 170 lb 90.60 in 15402.00 lb-in
Passenger 160 lb 90.60 in 14496.00 lb-in
Fuel 120 lb 76.00 in 9120.00 lb-in

Formula Used

Moment = Weight × Arm

Total CG = Total Moment ÷ Total Weight

Takeoff Weight = Ramp Weight − Taxi Fuel Weight

Landing Weight = Takeoff Weight − Trip Fuel Weight

Fuel weight is calculated as fuel gallons multiplied by fuel density. Taxi and trip fuel moments are removed using the fuel arm.

How To Use This Calculator

  1. Enter the current basic empty weight and empty arm.
  2. Add pilot, passenger, baggage, oil, fuel, and equipment values.
  3. Replace all sample arms with values from the aircraft record.
  4. Enter taxi fuel, trip fuel, and required reserve fuel.
  5. Set takeoff, landing, forward CG, and aft CG limits.
  6. Press Calculate to review ramp, takeoff, and landing results.
  7. Download CSV or PDF for a record or training review.

DA20 Loading Overview

A DA20 weight and balance review supports disciplined flight planning. The aircraft is small, responsive, and sensitive to loading changes. A few pounds moved aft can change the center of gravity. A few gallons burned can also shift the result. This calculator helps organize those numbers before the final manual check.

Main Balance Formula

Weight is the total load carried by the aircraft. Balance describes where that load acts. Each station has an arm. The arm is the distance from the aircraft datum. Multiplying weight by arm gives moment. Total moment divided by total weight gives center of gravity. The result is normally shown in inches from datum.

Stations And Limits

For a DA20, common loading items include empty aircraft, pilot, passenger, fuel, baggage, oil, and optional equipment. The tool lets you edit every arm and limit. That matters because aircraft manuals, serial ranges, modifications, and equipment lists may differ. Use the values from the current weight and balance record for the specific tail number.

Fuel Burn Checks

The ramp condition includes all items before taxi. Taxi fuel is then subtracted to estimate takeoff weight and moment. Trip fuel is subtracted from takeoff values to estimate landing condition. The fuel arm is used for each fuel subtraction. This gives a practical view of both ends of the flight.

Pass Or Adjust

A good result must pass two tests. First, weight should not exceed the chosen ramp, takeoff, or landing limit. Second, center of gravity should remain between the forward and aft limits. If either test fails, change the load plan. Reduce baggage, adjust occupants, reduce fuel only when legal reserves remain, or select another aircraft.

Planning Use

This page is a planning aid. It is not an approved flight document. Always compare the output with the official flight manual, current weighing report, placards, and school or operator rules. Rounding also matters. Conservative numbers are better than optimistic numbers. Save the CSV or PDF report for discussion, dispatch review, or training records. Use it to spot trends and teach loading discipline. Treat final authority as the aircraft document in the cockpit. Pilots compare reports and see why safe takeoff loading still needs a landing check after fuel burn.

FAQs

Is this calculator approved for flight release?

No. It is a planning aid. Use the approved aircraft manual, current weighing record, and operator procedures for the final decision.

Why are the arms editable?

DA20 records can vary by model, equipment, serial range, and weighing update. Editable arms let you match the exact aircraft data.

What does moment mean?

Moment is weight multiplied by arm. It shows how strongly a station affects the aircraft center of gravity.

Why check landing CG?

Fuel burn changes weight and moment. A loading plan can be acceptable at takeoff but still needs a landing condition review.

Can I change fuel density?

Yes. The calculator lets you edit fuel density. Use the value required by your manual, school, or operating procedure.

What happens if the result says CHECK?

Review the loading plan. Reduce weight, move baggage, adjust fuel, or consult an instructor, dispatcher, or mechanic before flight.

Does this handle envelope curves?

This version uses editable forward and aft CG limits. For stepped or curved envelopes, compare the final result with the official chart.

Why include CSV and PDF exports?

Exports help keep training records, compare loading scenarios, and share results for review before final manual verification.


Related Calculators

Paver Sand Bedding Calculator (depth-based)Paver Edge Restraint Length & Cost CalculatorPaver Sealer Quantity & Cost CalculatorExcavation Hauling Loads Calculator (truck loads)Soil Disposal Fee CalculatorSite Leveling Cost CalculatorCompaction Passes Time & Cost CalculatorPlate Compactor Rental Cost CalculatorGravel Volume Calculator (yards/tons)Gravel Weight Calculator (by material type)

Important Note: All the Calculators listed in this site are for educational purpose only and we do not guarentee the accuracy of results. Please do consult with other sources as well.