Icing Conditions & De-icing

071-02-02Pablo Asensio Martínez2026-04-011 min

Hazards of Icing

  • Aerodynamics: Increases drag (up to 40%), decreases lift (up to 30%), increases stall speed, changes pitching moment.
  • Weight: Adds weight to the aircraft.
  • Instrumentation: Blockage of pitot/static ports can lead to erroneous airspeed and altitude readings.
  • Engine: Ice ingestion can cause flameout or damage fan blades.

De-icing vs Anti-icing

Aeroflot Airbus A330-200 de-icing

  • De-icing: Removal of existing contaminants (ice, snow, slush) from the aircraft surfaces. Usually done with heated fluid (Type I) or mechanical methods.
  • Anti-icing: Application of a fluid that prevents the accumulation of contaminants for a limited time.

De-icing/Anti-icing Fluids

  • Type I: Orange. Low viscosity. Used for de-icing. Short holdover time.
  • Type II: Light yellow. Pseudoplastic (thickens when static, shears off during takeoff). Used for anti-icing.
  • Type III: Yellow. For slower aircraft (lower rotation speed).
  • Type IV: Green. Thickest fluid. Longest holdover time. Used for anti-icing.

Holdover Time (HOT)

The estimated time the anti-icing fluid will prevent the formation of frost or ice and the accumulation of snow on the protected surfaces of an aircraft.

  • Begins at the start of the anti-icing application.
  • Influenced by fluid type, concentration, OAT, and precipitation type/intensity.
  • Clean Aircraft Concept: No aircraft may take off if frost, ice, or snow is adhering to any critical surface (wings, control surfaces, etc.).
Written and reviewed by

Pablo Asensio

Aeronautical engineer. Passed the thirteen EASA ATPL(A) theoretical knowledge exams studying from these very notes. Writes and reviews each topic against the Part-FCL Learning Objectives.