Runway Performance

Aircraft

Flight

Details

Departure Arrival

Date EOBT

Weight

Fuel used — L · — kg Avgas at 0.710 kg/L

Take-off kg Landing kg

Landing weight cannot exceed take-off weight; adjusting either may move the other.

Landing950 kg

Take-off998 kg

862 kg1,043 kg

Distance—

Planning TAS105 kt

Take-off—

Landing—

Enter arrival and calculate.

Departure

EGNH Manual data

Time — Manual

Outputs

50 ft

Take-offWAIT

Personal required—

Available—

Remaining—

POH ground roll—

POH 50 ft—

CAA required—

N ESW

RWY

▼

Wind—

Head / tail—

Crosswind—

Pressure alt—

Density alt—

Calculations

Data

Runway — / —Runway dimensions unavailable

Runway reference data is physical length, not declared TORA/TODA/ASDA. Override with current published data.

Weather used forManual

Wind sourceManual

Temperature / QNHManual

Weather

Manual values.

Latest METAR: not loaded. Latest TAF: not loaded.

Runway basisManualVerify current declared distance

Weather basisManualVerify conditions for the planned time

Performance modelPOH dataSource shown in calculation details

CalculationAwaitingNo current calculation timestamp

Limits & margins

≤50%50–80%>80% of demonstrated crosswind

POH distance CAA safety margin Personal minimum Runway remaining

Enter valid inputs.

Method

POH chart

Open the source chart and hand-style trace

Calculate to plot the result.

Inputs

Runway Available m Surface Slope % + uphill Wind from °M Wind kt Gust kt QNH hPa Temperature °C Elevation ft Take-off flap setting

Arrival

— Manual data

Time — Manual

Outputs

50 ft

LandingWAIT

Personal required—

Available—

Remaining—

POH ground roll—

POH 50 ft—

CAA required—

N ESW

RWY

▼

Wind—

Head / tail—

Crosswind—

Pressure alt—

Density alt—

Calculations

Data

Runway — / —Runway dimensions unavailable

Runway reference data is physical length, not declared LDA. Override with current published data.

Weather used forManual

Wind sourceManual

Temperature / QNHManual

Weather

Manual values.

Latest METAR: not loaded. Latest TAF: not loaded.

Runway basisManualVerify current declared distance

Weather basisManualVerify conditions for the planned time

Performance modelPOH dataSource shown in calculation details

CalculationAwaitingNo current calculation timestamp

Limits & margins

≤50%50–80%>80% of demonstrated crosswind

POH distance CAA safety margin Personal minimum Runway remaining

Enter valid inputs.

Method

POH chart

Open the source chart and hand-style trace

Calculate to plot the result.

Inputs

Runway Available m Surface Slope % + uphill Wind from °M Wind kt Gust kt QNH hPa Temperature °C Elevation ft

OverallWAIT

Load or enter departure and arrival data.

Workspace

Settings

Interface

Appearance

Choose the display mode. Aircraft accents remain consistent across themes.

ThemeUse the light or dark interface.

Runway Performance

Details

EGNH Manual data

Outputs

Data

Weather

Limits & margins

Method

POH chart

Inputs

— Manual data

Outputs

Data

Weather

Limits & margins

Method

POH chart

Inputs

Settings

Appearance

Flight planning

Aircraft library

Library

Upload an aircraft POH

Account

Change password

Users

Data and safety

Aircraft photographs

Add your first aircraft