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Landing Distance vs Density Altitude Calculator

Scale book landing figures to today's density altitude — a gentler 1/σ law than takeoff, but one that still bites at mountain strips.

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Estimated landing roll today (ft)
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Over 50 ft today (ft)
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Multiplier (1/σ)

Why milder than takeoff's 1/σ²? Brakes don't care about air density — only the touchdown true airspeed grows (as 1/√σ, squared in the energy). The engine's altitude problems don't attend the landing.

Formula

touchdown TAS² ∝ 1/σ at fixed IAS; landing distance ≈ book × 1/σ
References: Anderson, Aircraft Performance and Design, §6.3 (takeoff/landing ground roll); FAA-H-8083-3C, Airplane Flying Handbook, ch. 5–6 & 9

⚠️ Planning estimate only — your POH/AFM performance charts are the authoritative source. Always verify with official data, and apply your operator's safety factors. Not for airworthiness decisions.

Scale book landing figures to today's density altitude — a gentler 1/σ law than takeoff, but one that still bites at mountain strips.

About Landing Distance vs Density Altitude Calculator

Pilots who internalize the takeoff density-altitude penalty often forget landings inherit one too: the same indicated approach speed is a faster true — and ground — speed in thin air, and brake energy grows with its square. This calculator scales book landing figures by the 1/σ law (gentler than takeoff's 1/σ², for reasons it explains), which still adds 25%+ at the mountain strips where runway tends shortest.

How to use Landing Distance vs Density Altitude Calculator

  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 touchdown TAS² ∝ 1/σ at fixed IAS; landing distance ≈ book × 1/σ 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 Landing Distance vs Density Altitude Calculator?

  • Instant, free and private — every calculation runs in your browser, nothing is uploaded
  • Built on the published formula touchdown TAS² ∝ 1/σ at fixed IAS; landing distance ≈ book × 1/σ with sources cited on the page
  • Why milder than takeoff's 1/σ²? Brakes don't care about air density — only the touchdown true airspeed grows (as 1/√σ, squared in the energy). The engine's altitude problems don't attend the landing.
  • Switch units, tweak any input and watch every result update live

Frequently asked questions

Why is landing hit by 1/σ when takeoff suffers 1/σ²?+

Both share the true-airspeed effect: fixed indicated speed means ground speed (and kinetic energy) up by 1/σ. Takeoff additionally loses engine thrust to thin air — its second σ. Landing's decelerating forces (brakes, mostly) are density-indifferent, so only the energy term remains. Same atmosphere, half the exponent.

Does the thin air change my approach speed?+

Not the indicated number — fly the same KIAS as always; the wing stalls at the same IAS regardless of altitude. What changes silently is everything tied to true speed: ground speed at touchdown, descent rate at a given glide angle, turn radius in the pattern. The picture looks fast because it is fast, even while the needle says normal.

Is float worse at high density altitude?+

Slightly, and for the same reason: excess energy. Arrive 5 knots fast at a 7,000 ft DA strip and the float consumes more feet than the same error at sea level because each knot of excess IAS is more TAS. The discipline that matters most at altitude is speed discipline on short final — see our approach-speed penalty tool for the squared cost.

Do POH landing charts already include altitude columns?+

Yes, and use them when published — they're flight-test data. This tool earns its place when you're between chart lines, when you want the why behind the columns' trend, or for quick what-ifs (e.g., 'is the 1,800 ft strip at the 8,200 ft DA lake still workable at gross?') before committing to the full chart exercise.

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