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Extra resources for Aircraft Icing Handbook

Sample text

1 Through practical experience, a wealth of knowledge has been accumulated operating fixed-wing aircraft in icing conditions; there are some other considerations, however, with rotary-wing aircraft. 2 Conditions for Ice Formation The conditions in which ice formation is possible are given below: (a) Icing may occur in conditions of high humidity when the ambient air temperature is at or below 0°C. (b) Due to local reduction pressure, icing may occur in conditions of high humidity when the ambient air temperature is above zero degrees centigrade.

Generally, engine intakes must be very clean in design, avoiding any projections; even rivet heads will cause sufficient turbulence to form an accretion point If the intakes are hinged to give engine access, the sealing at the hinge point must not offer any leakage. (b) Windscreen Anti-Icing: Electrically- heated windscreens are completely satisfactory and also reliable, even in the most severe cond itions. (c) Outside Air Temperature (OAT) Gauge: Once in the icing range, temperatures are critical and an OAT gauge that is accurate to one degree is essential.

Corrective action must be taken before an irretrievable situation develops. Should the engine stop due to icing it may not re-start or, even if it does, the delay may result in a critical situation. Carburettor or fuel icing may occur even in clear air and these are, therefore, the most insidious of the various types of icing because of the lack of visual clues. The risk of all forms of induction system icing is higher in cloud than in clear air but because of the visual clues the pilot is less likely to be taken unawares.

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