Loading. Weight and CG use the AFM station arms, fuel and baggage limits, and the selected MÄM and tank configuration. CG is checked both at zero fuel and with the entered fuel.
Field performance. Takeoff uses Flaps T/O and landing uses Flaps LDG on a level asphalt runway. The separate AFM Flaps UP landing chart is not implemented. No grass, wet-runway, runway-slope, or tailwind adjustment is calculated.
Climb performance. Takeoff climb uses Flaps T/O and cruise climb uses Flaps UP, with the AFM power settings and mass-dependent speeds shown in the results.
Coverage. Results are read from digitized AFM nomographs. Unsupported conditions return a blank result; favorable mass or headwind corrections beyond a charted range are not credited instead of being extrapolated.
Use. This is a planning aid, not approved flight-manual data. Verify the aircraft configuration, loading, result, and limitations against the current AFM for the specific aircraft.