Cold-weather altimeter correction
Cold air effect (TC AIM AIR 1.5.4):
- Denser than standard atmosphere: pressure levels sit lower.
- Altimeter over-reads; true altitude below indication.
- Equal surface pressure: cold column shorter, pressure falls faster with height. Pressure at a given altitude LOWER than in warm column (FAA AWH 8.2.4.2).
Rule (TC AIM AIR 1.5.4): indicated altitude off about 4% per 11°C the column's average temperature differs from ISA average.
Winter (TC AIM AIR 1.5.4):
- Strong low-level inversions likely; altimeters habitually over-read.
- Ground separation marginal: add 50% to error found from flight-level temperature.
Finding temperature deviation (use pressure altitude, not indicated):
- Momentarily set 29.92" on subscale.
- Read pressure altitude.
- Compare ISA temperature at that level to actual OAT.
- Apply 4%-per-11°C rule to indicated altitude; pressure altitude only finds deviation.
Worked example (TC AIM AIR 1.5.4):
- Indicating 6 000 ft on 29.80".
- Momentarily set 29.92": pressure altitude 6 120 ft.
- OAT -20°C: temperature error large enough to shrink mountain-crossing margin to just over 200 ft.
Corrected altitude (FAA AWH 8.4.1.3):
- Correcting indicated altitude gives corrected (approximately true) altitude.
- Flight computer derives it from OAT.
- Close enough to true altitude for terrain clearance once altimeter set from nearby reporting station.
- Reasonably accurate when actual lapse rate near Standard Atmosphere rate of 2°C per 1000 ft (TC AIM AIR 1.5.4).
Mountain wave compounds error (TC AIM AIR 1.5.8): with non-standard temperature, overread can reach 3 000 ft, far beyond temperature error alone.
Trap: 4%-per-11°C rule multiplies indicated altitude, not the pressure altitude used to find deviation.
References
- TC AIM AIR 1.5.4
- FAA PHAK ch.8 (cold air denser; altitude lower than indication)