Eclipse 500 System Manual page 116

Section 6. Ice Protection
6.3 Limitations and Specifications
6.3.1 Icing Conditions
Flight into known icing conditions is prohibited.
When outside air temperature is 10°C (50°F) or below and visible moisture is
present, engine anti-ice must be selected ON for all ground and flight operations,.
When operating the engines at idle speed on the ground in freezing fog and visible
moisture, the engine speed must be increased once every five minutes to 65% N1 to
avoid ice accumulation on the spinner.
6.3.2 Pneumatic De-ice
The use of wing deice (boots) is prohibited.
The following wing deice Electronic Circuit Breakers (ECBs) must be collared:
INBOARD WING DEICE L,
INBOARD WING DEICE R,
OUTBOARD WING DEICE L and
OUTBOARD WING DEICE R.
6.3.3 Windshield Heat
The use of windshield heat is prohibited.
The following windshield heat ECB must be collared:
L/R WINDSHIELD HEAT.
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Copyright © — Eclipse Aviation Corporation
Eclipse 5OO Systems Manual
Version 2.0 April 2007