Landing fuel prediction

Read expected weight

Use the current destination prediction and compare it with the actual fuel and flight plan.

Identify the runway

Check the landing distance available and the runway’s slope and elevation on the current chart.

Check the surface

Use the reported condition and weather. A wet or contaminated runway can change stopping performance.

Check wind

Use the headwind or tailwind component applicable to the planned runway. Reassess when the wind changes.

Set landing data

Enter and check the landing configuration and approach speeds for the actual aircraft in the FSS workflow.

Review landing distance

Compare required and available distance with applicable margins.

No landing-performance value is implied.

In version 1.1.0, generate the flight manifest to open the EFB performance page. Confirm that the landing tab shows the destination and its current conditions. Compare the required distance with the available runway and applicable margins. In version 1.0, use another applicable performance source.

Have another plan

If the conditions, performance or aircraft status make the landing unsuitable, plan a different runway or diversion in the simulation.

FSS added EFB takeoff and landing distance calculations in Service Update 1. The page is available after a flight manifest has been generated. FSS Service Update 1 ^[2].

One community-support post on 8 November says both performance tabs showed departure-airport weather. It has no reply or confirmed diagnosis. If your landing tab shows departure conditions instead of the destination, do not rely on its calculation. EFB performance report, 8 November 2026 ^[222].

The supplied E175 QRH includes a runway-condition assessment matrix and describes its operational landing tables as advisory ^{[L04, PDF p. 317]}. It is a real-aircraft reference; use data applicable to your simulated aircraft and conditions.

The supplied E190/195 AFM lists a runway slope limit of −2% to +2% and a paved runway surface for the aircraft codes shown ^{[L05, PDF pp. 74 and 80]}. These are real-aircraft limitations; check the applicable limits for the simulated variant.