Take-off & Landing Performance

Aircraft Operation Runway designator Available distance (m) Runway slope (%) + uphill / − downhill Wind direction °M Wind speed (kt) Gust (kt, optional) QNH (hPa) Elevation (m) Temperature (°C) Aircraft weight (kg) Surface Use result Personal margin (%)

Automatic POH calculation

Ground roll—

Distance over 50 ft—

POH source—

PA-28 source-chart reference

The automatic PA-28 result uses a range-limited curve-fit digitisation of the scanned nomographs. Check the plotted chart before operational use.

Displayed chart

Wind and atmosphere

➤

Head/tailwind—

Crosswind—

Pressure altitude—

Density altitude—

Runway requirement

Manufacturer result—

Planning requirement—

Runway remaining—

Crosswind status—

Calculation trace

Performance briefing

Awaiting valid result

Dataset status

Development tool only. Independently verify all results against the applicable aircraft POH/AFM, supplements and current aircraft configuration before operational use.