Corrected Altitude
Corrected altitude (altitude adjusted for errors) is the altitude value used after adjusting indicated altitude for temperature and pressure deviations from sta...
Cold Temperature Correction is the adjustment of instrument approach minimum altitudes to correct for barometric altimeter errors in sub-standard temperatures, ensuring safe terrain clearance.
Cold Temperature Correction refers to the essential process of adjusting published instrument flight altitudes to mitigate the effects of barometric altimeter errors in colder-than-standard atmospheric conditions. This is crucial for maintaining obstacle clearance and flight safety during instrument approaches, particularly in regions with severe winter climates.
Barometric altimeters, the primary altitude reference in most aircraft, assume the International Standard Atmosphere (ISA) temperature and pressure lapse rates. When the outside air is much colder than ISA, the altimeter overstates the aircraft’s true altitude above ground. This error can be several hundred feet on approach, especially at airports surrounded by high terrain or obstacles.
The risk is summarized in aviation with the phrase:
“From Hot to Cold – Look Out Below.”
When uncorrected, these errors can result in aircraft descending below published minimum altitudes, increasing the risk of Controlled Flight Into Terrain (CFIT) or obstacle collision.
The pressure levels in the atmosphere compress closer to the ground when temperatures are lower than standard. The altimeter, using the ISA model, interprets the same pressure as a higher altitude than it actually is.
Cold temperature correction is required:
Regions with frequent cold temperature operations include North America, Northern Europe, and parts of Asia.
Authorities like the FAA and ICAO maintain lists of airports and procedures requiring cold temperature correction. These specify:
Pilots must check these lists during flight planning.
A snowflake (❄) on a U.S. Government approach chart signals that cold temperature correction is required on one or more segments of that procedure when the temperature is at or below the published threshold.
Depending on the procedure and airport, correction may be required for:
Only the segments specified on the CTA list or approach plate require correction.
Official correction tables (found in the FAA’s Aeronautical Information Manual or ICAO PANS-OPS) provide the number of feet to add to published segment altitudes, based on temperature and height above the airport.
Example Table (FAA AIM):
| Temp (°C) | 1000 ft | 1500 ft | 2000 ft | 3000 ft | 4000 ft | 5000 ft |
|---|---|---|---|---|---|---|
| 0 | 40 | 60 | 80 | 120 | 160 | 200 |
| −10 | 60 | 90 | 120 | 180 | 240 | 300 |
| −20 | 80 | 120 | 160 | 240 | 320 | 400 |
| −30 | 110 | 160 | 210 | 320 | 430 | 540 |
Important: For altitudes above the highest column, use the highest value.
Many modern avionics (e.g., Garmin G1000, Honeywell, Collins) allow pilots to input the surface temperature, then auto-calculate and display corrected altitudes for each fix. This minimizes workload and error risk.
Corrections are only applied to the approach segments specified by the CTA list or approach chart notes. For multi-segment procedures, each correction is calculated separately based on height above the airport at each fix.
Do not apply corrections to ATC-assigned vectoring altitudes unless coordinated with ATC.
Conditions:
FAF Correction:
MDA Correction:
ATC Report:
“Request 6,400 feet for cold temperature operations from ODIRE to SUPPY.”
Conditions:
FAF Correction: 8,500 − 6,451 = 2,049 ft (~2,000 ft). Table at −30°C: 210 ft → 8,710 ft
MDA Correction: 7,840 − 6,451 = 1,389 ft (~1,500 ft). Table at −30°C: 160 ft → 8,000 ft
Missed Approach Correction: 14,000 − 6,451 = 7,549 ft (use 5,000 ft column). Table at −30°C: 540 ft → 14,540 ft
ATC Report:
“Require 8,710 feet from LAGIC to KARCE for cold temperature operations.”
“Require final holding altitude 14,540 feet on missed approach for cold temperature operations.”
For aircraft with FMS compensation, simply:
ISA assumes a sea-level temperature of 15°C and a lapse rate of −2°C/1,000 ft. When the real temperature is colder, pressure levels compress closer to the surface, so the altimeter overstates altitude. The greater the cold deviation and the higher the segment above the airport, the larger the correction needed.
Always use current AWOS, ASOS, ATIS, or validated online sources for temperature.
Cold Temperature Correction is a vital safety procedure for instrument approaches in cold climates. By understanding and applying these corrections, flight crews ensure compliance with regulations and, most importantly, maintain critical obstacle clearance. Whether using manual calculations or modern avionics, proper cold temperature correction is a hallmark of safe, professional airmanship.
For the latest regulatory guidance and tables, always consult the FAA Aeronautical Information Manual, ICAO PANS-OPS, and your regional authority publications.
Barometric altimeters are calibrated to standard temperature profiles. When the actual temperature is significantly below standard, the altimeter overstates the aircraft's true altitude, increasing the risk of controlled flight into terrain (CFIT). Cold temperature correction ensures the aircraft remains clear of obstacles by compensating for this instrument error.
Pilots determine which approach segments require correction (as indicated by the snowflake symbol or CTA list), calculate the height above the airport elevation for those fixes, reference official correction tables based on reported temperature, and add the correction to the published approach altitudes. Corrections are not made to the altimeter setting but to the target altitude flown.
No. Only airports and procedures listed on regulatory Cold Temperature Airports (CTA) lists, or marked with the snowflake symbol on approach charts, require mandatory cold temperature correction. Best practice recommends considering correction in any cold environment with significant temperature deviation from standard.
Failure to apply required cold temperature corrections can result in flying below the intended minimum safe altitude, potentially leading to loss of obstacle clearance, regulatory non-compliance, and an increased risk of controlled flight into terrain (CFIT).
Yes. Modern Flight Management Systems (FMS) and integrated avionics can automate the process. Pilots enter the current surface temperature, and the system adjusts approach segment altitudes automatically. Pilots must verify that all required segments are compensated and that corrections are communicated to ATC when necessary.
Ensure terrain and obstacle clearance in cold weather with accurate cold temperature corrections. Learn how our solutions streamline compliance with regulatory requirements for instrument approaches.
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