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Sample text

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.

B) Upholstery becoming soiled. Forward areas should be free of fluid residues to avoid blowback onto cockpit windscreens during departure. If Type II fluids are used, all traces of the fluid on cockpit windows should be removed prior to departure. Particular attention being paid to windows fitted with wipers. De-icing/anti- icing fluid can be removed by rinsing with clear water and wiping with a soft cloth. Do not use the windscreen wipers for this purpose. This will cause smearing and loss of transparency.

Thus the main detection instrument is the RPM gauge used in conjunction with the Air Speed Indicator; (b) where a constant speed propeller is fitted and in a helicopter the loss of power would have to be large before the RPM reduced, hence the onset of induction system icing could be even more insidious. However, the effect of icing will be shown by a drop in manifold pressure and then by a reduction of airspeed or height. The primary detection instrument is, therefore, the manifold pressure gauge.

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Aircraft Icing Handbook

by David

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