Manifest

1 Airport

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Elevationft MSL

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Altimeter

inHg

Temperature

°C

Wind from (true)

°T

Wind speed

kts

Runways

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Pressure altitude

ft

PA ≈ elevation + (29.92 − altimeter inHg) × 1,000

Density altitude

ft

DA ≈ PA + 120 × (temperature °C − ISA °C)

ISA °C = 15 − 0.0019812 × PA

Runway winds

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Runway	Headings °T	Surface wind (kts)	Crosswind (kts)	From (by direction)
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NOTAMs

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TFRs

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Elevation source · Runways: OurAirports; verify current usable lengths.

METAR

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Aviation Weather Center ↗

2 Aircraft

Saved in this browser by aircraft type

Aircraft type

Front seat weight

lb

Takeoff fuel burn

US gal

3 Aircraft performance

Saved by aircraft type

Ground roll

ft

Ground roll over 50 ft

ft

Max rate of climb

ft/min

Landing distance

ft

Maneuvering speed

kts IAS

Best glide

kts IAS

Use aircraft POH performance values for the current weight and conditions.