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9 Cards in this Set

  • Front
  • Back
Recall the function of the TAIL De-Ice Pushbutton:
Push - (Air foil system in use) Closes the shutoff valve to the tail to allow 2.5 minutes of tail de-ice. The system automatically reverts to wing anti-ice function following the 2.5 minutes of tail de-ice function.
Understand how to activate air foil ice protection:
The system is activated by selecting the AIR FOIL switch to ON and placing the crossfeed valve(s) to OPEN.
Understand the effect of moving the Ice Protection Panel METER SEL & HEAT Selector switch out of the off position:
Moving the selector to any position except the OFF energizes all heater circuits, except the RAT probe while on the ground.
Recall the function of the WINDSHIELD ANTI-ICE Switch:
*OFF - Deactivates the windshield anti-ice system.
*ON - Provides electrical heat to the outside of Captain's, Center, and First Officer's windshields.
Recall the airfoil anti ice protection cycle:
*Air foil ice protection is only available in-flight.
*The system is activated by selecting the AIR FOIL switch to ON and placing the crossfeed valve(s) to OPEN. This action provides a continuous cycle of heat for the leading edge of the wings (slats) and the forward strakes for fifteen minutes, followed by 2 1/2 minutes of heat to the horizontal stabilizer. The ram air inlet is heated during both cycles.
*The automatic cycle can be overridden by the TAIL button which, when pushed, provides 2 1/2 minutes of horizontal stabilizer de-icing, after which a new wing cycle starts.
*Placing the AIR FOIL switch in the OFF position causes the horizontal stabilizer de-icing cycle to be activated for 2 1/2 minutes.
Understand the function of the OVERWING HEATER Switch:
*ARM - Provides electrical power to the wing heater control units when the airplane is on the ground. The switch is normally guarded to this position.
*OFF - Removes electrical power from the heater control units.
Understand the function of the Overwing Heater system:
*the overwing heater system prevents the buildup of ice on the inboard corner of the upper wing.
*The overwing heater system does not de-ice the entire wing nor does it provide anti-ice or de-ice capability for environmental icing conditions.
Describe the indications on the OAP when engine anti-ice in use:
*When selected ON, an amber (L/R) ENGINE VALVE message will appear on the OAP indicating the valves are in transit and disagree with the switch position.
*When at least one valve is fully open, a blue (L/R) ENGINE ANTI-ICE ON light on the OAP illuminates.
*When all three valves are fully open, the amber message extinguishes and the blue light remains illuminated indicating normal system operation.
Describe the conditions that require the use of engine anti-ice while on the ground/in-flight:
*Ground - Engine anti-ice systems must be on after start when the ambient temperature is 6 degrees C (42F) or below and any of the following conditions exist. Visible moisture as in rain, snow, or fog (visibility 1 mile or less in fog), or 3 degrees C or less temperature/dewpoint spread exists or runways and taxiways are wet.
*Flight - Activate engine anti-ice before entering ice conditions. In flight, a RAT/TAT of 10 degrees or below with visible moisture indicates a need of engine anti-icing.