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Density Altitude Calculator (Metric / hPa)

Full-metric density altitude for pilots flying QNH in hectopascals and elevations in metres — ICAO units, no inches of mercury anywhere.

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Density altitude (m)
0
Pressure altitude (m)
0
ISA temperature at PA (°C)
0
ISA deviation (°C)

8.23 m per hPa and 36.21 m per °C are the metric twins of the familiar 1,000 ft/inHg and 118.8 ft/°C rules. ICAO ISA lapse rate: 6.5 °C per 1,000 m.

Formula

PA(m) = elev + (1013.25 − QNH) × 8.23; ISA = 15 − 6.5·PA(km); DA(m) = PA + 36.21 × (OAT − ISA)
References: ICAO Doc 7488/3, Manual of the ICAO Standard Atmosphere; EASA Easy Access Rules for SERA — altimeter-setting procedures; FAA-H-8083-25C, Pilot's Handbook of Aeronautical Knowledge, ch. 11

⚠️ For flight planning and education only — always verify against your aircraft's POH/AFM, official weather sources and certified instruments. Not for primary navigation or airworthiness decisions.

Full-metric density altitude for pilots flying QNH in hectopascals and elevations in metres — ICAO units, no inches of mercury anywhere.

About Density Altitude Calculator (Metric / hPa)

Most density-altitude calculators online assume inches of mercury and feet — useless friction if your AIP, METARs and charts speak hectopascals and metres. This tool is metric end to end: QNH in hPa, elevation in metres, lapse rate at the ICAO 6.5 °C/km, with the conversion factors (8.23 m per hPa, 36.21 m per °C) shown in the worked example rather than hidden. A US-unit toggle is one click away when you need to compare.

How to use Density Altitude Calculator (Metric / hPa)

  1. 1Enter — sensible defaults are pre-filled so you see a worked result immediately.
  2. 2Read the live results: .
  3. 3Check the "With your numbers" line to see the formula PA(m) = elev + (1013.25 − QNH) × 8.23; ISA = 15 − 6.5·PA(km); DA(m) = PA + 36.21 × (OAT − ISA) substituted step by step.
  4. 4Adjust inputs (or flip the unit toggle) until the scenario matches yours, then copy or share the result.

Why use Density Altitude Calculator (Metric / hPa)?

  • Instant, free and private — every calculation runs in your browser, nothing is uploaded
  • Built on the published formula PA(m) = elev + (1013.25 − QNH) × 8.23; ISA = 15 − 6.5·PA(km); DA(m) = PA + 36.21 × (OAT − ISA) with sources cited on the page
  • 8.23 m per hPa and 36.21 m per °C are the metric twins of the familiar 1,000 ft/inHg and 118.8 ft/°C rules. ICAO ISA lapse rate: 6.5 °C per 1,000 m.
  • Switch units, tweak any input and watch every result update live

Frequently asked questions

How do I convert QNH in hPa to pressure altitude?+

Each hectopascal away from the standard 1013.25 hPa is worth about 8.23 m (27 ft) of pressure altitude. QNH below standard puts pressure altitude above field elevation; QNH above standard puts it below. This tool computes PA = elevation + (1013.25 − QNH) × 8.23 and shows the substitution explicitly.

Why 36.21 metres per degree Celsius?+

It is the metric equivalent of the FAA's 118.8 ft/°C: the density-altitude correction per degree of deviation from ISA temperature. Multiply the ISA deviation at your pressure altitude by 36.21 m and add it to pressure altitude — exactly what the result panel's worked example walks through with your numbers.

Does this match what my European flight computer gives?+

Within the tolerance of the underlying approximations, yes — both implement the ICAO standard atmosphere with the linear temperature correction. Small differences (tens of metres) arise from rounding the hPa-to-metres factor or using exact barometric formulas instead of the linear correction. For performance planning those differences are immaterial.

When does QFE vs QNH matter for this calculation?+

Use QNH (sea-level-referenced) with the field's elevation, as this calculator does. If you only have QFE (the field-level pressure), either convert it — QNH ≈ QFE + elevation/8.23 m·hPa⁻¹ — or use a station-pressure-based tool. Mixing QFE with field elevation here would double-count the airport's height.

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