RunupLab

Free tool

Takeoff & Landing Performance

Enter field elevation, altimeter, temperature, and weight to get takeoff and landing ground roll and over-50-ft distances, then add a headwind and a safety margin and check whether it all fits on your runway. The method is the useful part: pressure and density altitude → chart interpolation → wind and safety-margin adjustment → runway-fit check.

Takeoff and landing numbers are inherently aircraft-specific, so the chart grid here is a clearly-labeled PA-28-140 worked exampledigitized from the 1964 Owner's Handbook (paved, level, dry, no wind). Every input is editable so the method is visible for any light single — but the numbers you fly must come from your own POH.

Conditions
Density altitude5,280 ft
Wind, runway & margin

Headwind component +8.7 kt from the wind on this runway.

Takeoff ground roll1,509 ft
Over 50-ft obstacle3,554 ft
Runway fitToo short
1,509 GR3,554 / 50FTRWY 2,600

Short by 954 ft — the over-50-ft distance overruns 2,600 ft of runway. Add runway, reduce weight, or wait for cooler air.

Distance build-up (ft)
POHWind-adj+ margin
Ground roll1,5011,0061,509
Over 50 ft3,1662,3693,554

Use YOUR POH. The chart grid here is a worked PA-28-140 example(1964 Owner's Handbook — paved, level, dry, no wind), illustrative for training only. The wind and safety-margin steps are estimates beyondthe POH chart. Read your own aircraft's charts for the numbers you fly.

More pilot tools

One of a growing set of free pilot tools. For density altitude, weight & balance, and the numbers behind these distances, see the study guide.