Cirrus SR22 Pilot's Operating Handbook And Flight Manual page 462

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Section 3 - Emergency Procedures

A failure of the Anti-Ice System is any condition, observed or

suspected, in which the system fails to remove ice from protected

surfaces including the propeller, in addition to any Anti-Ice System

CAS failure annunciations. An unobserved failure may be indicated by

a decrease in airspeed, anomalous handling characteristics, or

airframe vibrations.

Significant loss in cruise or climb performance may be an

indication of propeller ice accretions that are not visible to the

naked eye. Operation of the engine at 2700 RPM will help

shed ice in severe icing conditions.

Continuous ice accumulations on protected areas are

With ice accumulations on the horizontal stabilizer leading

edge, flaps should remain retracted for landing and the

landing speed increased accordingly.

With asymmetrical ice accumulations on large portions of the

wing or horizontal stabilizer, avoid flight at speeds less than 95

Cirrus Design

P/N 13772-150

Original Issue: 02-01-13

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