Module MOD-06 · 8 min · ACS PA.I.F
Density Altitude and Aircraft Performance
← Weight, Balance and Aircraft Performancedraft — pending CFI review
Air density is what the wing, propeller, and engine actually work with, and three factors thin it out: higher altitude, higher temperature, and higher humidity. Density altitude is simply pressure altitude corrected for temperature — the altitude the airplane behaves as if it were flying at. On a hot day at a high-elevation airport, density altitude can be thousands of feet above the field elevation, so the wing makes less lift, the propeller bites less air, and a normally aspirated engine makes less power. That combination lengthens the takeoff roll and flattens the climb. Takeoff and landing distances also grow with higher weight, a tailwind, an upsloping runway on takeoff, and a soft or contaminated surface, while a headwind shortens them. The prudent pilot treats a hot, high, heavy, downwind takeoff as the worst case and plans generous margins.
Key terms
- Density altitude
- Pressure altitude corrected for nonstandard temperature.
- Pressure altitude
- Altitude read with the altimeter set to 29.92 inHg.
- High, hot, humid
- The three conditions that raise density altitude and cut performance.
Summary
High, hot, and humid conditions raise density altitude and degrade lift, thrust, and power. Weight, wind, slope, and surface further change takeoff and landing distance.
Quick check ▾
One question on what you just read.
Question 1 of 1
Objective mastery: 15%
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Density altitude is best defined as which of the following?
Sources
Every claim traces to a source — paraphrased knowledge elements pointing at the governing FAA publication; not yet verified against a retrieved source.
- FAA-H-8083-25 (performance) — Pilot’s Handbook of Aeronautical Knowledge unverified
- FAA-H-8083-25 (performance) — Pilot’s Handbook of Aeronautical Knowledge unverified
- FAA-H-8083-3 (takeoff/landing) — Airplane Flying Handbook unverified
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