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  2. CFR & AIM
  3. CFR
  4. Part 29
  5. Appendix C
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14 CFR Part 29
  1. Subpart A: General
  2. Subpart B: Flight
  3. Subpart C: Strength Requirements
  4. Subpart D: Design and Construction
  5. Subpart E: Powerplant
  6. Subpart F: Equipment
  7. Subpart G: Operating Limitations and Information
  8. Appendices

    Appendix A to Part 29: Instructions for Continued Airworthiness
  9. Appendix B to Part 29: Airworthiness Criteria for Helicopter Instrument Flight
  10. Appendix C to Part 29: Icing Certification
    1. Appendix C to Part 29 Icing Certification
  11. Appendix D to Part 29: Criteria for Demonstration of Emergency Evacuation Procedures Under § 29.803
  12. Appendix E to Part 29: HIRF Environments and Equipment HIRF Test Levels

14 CFR Part 29|eCFR Sep 29, 2026

Appendix C to Part 29

Icing Certification

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(a)

Continuous maximum icing. The maximum continuous intensity of atmospheric icing conditions (continuous maximum icing) is defined by the variables of the cloud liquid water content, the mean effective diameter of the cloud droplets, the ambient air temperature, and the interrelationship of these three variables as shown in Figure 1 of this appendix. The limiting icing envelope in terms of altitude and temperature is given in Figure 2 of this appendix. The interrelationship of cloud liquid water content with drop diameter and altitude is determined from Figures 1 and 2. The cloud liquid water content for continuous maximum icing conditions of a horizontal extent, other than 17.4 nautical miles, is determined by the value of liquid water content of Figure 1, multiplied by the appropriate factor from Figure 3 of this appendix.

(b)

Intermittent maximum icing. The intermittent maximum intensity of atmospheric icing conditions (intermittent maximum icing) is defined by the variables of the cloud liquid water content, the mean effective diameter of the cloud droplets, the ambient air temperature, and the interrelationship of these three variables as shown in Figure 4 of this appendix. The limiting icing envelope in terms of altitude and temperature is given in Figure 5 of this appendix. The interrelationship of cloud liquid water content with drop diameter and altitude is determined from Figures 4 and 5. The cloud liquid water content for intermittent maximum icing conditions of a horizontal extent, other than 2.6 nautical miles, is determined by the value of cloud liquid water content of Figure 4 multiplied by the appropriate factor in Figure 6 of this appendix.

Previous AppendixAppendix B to Part 29: Airworthiness Criteria for Helicopter Instrument FlightNext Appendix Appendix D to Part 29: Criteria for Demonstration of Emergency Evacuation Procedures Under § 29.803

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Appendix C to Part 29 Icing Certification

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