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27 Cards in this Set
- Front
- Back
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ICING CONDITIONS
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IN FLIGHT
TAT 10C OR BELOW VISIBLE MOISTURE RAIN, SNOW, SLEET OR ICE CYRISTALS, CLOUDS OR FOG AND VISIBILITY < 1 MILE |
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ICING CONDITIONS
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ON THE GROUND
OAT IS 10C OR BELOW WITH SURFACE SNOW, ICE, STANDING WATER OR SLUSH |
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ENGINE COWL VALVE FAILED OPEN
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LIMIT THRUST ON THE 80 N1 IF POSSIBLE
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" COWL ANTI ICE "
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AN ENGINE COWL ANTI ICE DUCT OVERPRESSURE OCCURS
THRUST LEVER RETARD UNTIL THE COWL ANTI ICE LIGHT EXTINGUISHED |
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THERE IS NO ANTI-ICE PROTECTION FOR
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OUTER SLATS OR LEADING EDGE FLAPS
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BOTH WING ANTI-ICE VALVE CLOSED
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WHEN THE THRUST ON EITHER ENGINE IS MORE THAN THE TAKEOFF WARNING SETTING
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BOTH WING ANTI ICE VALVE CLOSED
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IF EITHER TEMPERATURE PROBE SENSE AN OVERTEMPERATURE INSIDE THE WING DUCT
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THE WING ANTI-ICE SWITCH MOVES TO OFF
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AT LIFT OFF WHEN AIR/GROUND SENSOR CHANGES TO AIR MODE
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IN FLIGHT DUCT TEMPERATURE AND ENGINE THRUST SETTING
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HAVE NO EFFECT ON THE OPEATION OF THE WING ANTI-ICE VALVES
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WING ANTI-ICE OPERATION
DE-ICER |
CLEANEST AIRFOIL SURFACE
LESS ICE RUNBACK LESS FUEL USED |
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WING ANTI-ICE OPERATION
ANTI-ICER |
POSSIBLE ICE RUNBACK
MORE FUEL USED |
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ALL WINDOW HEAT SHOULD BE ON
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AT LEAST 10 MINUTES BEFORE T/O
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THE WINDOW HEAT IS TURNED OFF
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DURING SHUTDOWN OR WHEN THE FLIGHT GROUND TIME IS MORE THAN 30 MINUTES
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TEMPERATURE CONTROLLERS MONITOR
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WINDOWS NUMBER 1 AND NUMBER 2 FOR AN OVERHEAT CONDITION
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IF WINDOW OVERHEATS
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THE OVERHEAT LIGHT
THE AMBER OFF LIGHT MASTER CAUTION ANTI-ICE |
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DO NOT PERFORM THE POWER TEST
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WHEN ALL LIGHTS ARE ILLUMINATED
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WINDOWS WITH DEFOGGED
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NUMBER 1
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WINDSHIELD WIPER INT
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SEVEN SECONDS
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THERMAL ANTI-ICE INDICATION
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GREEN : COWL VALVE (S) OPEN
AMBER : IS NOT IN POSITION INDICATED BY THE RELATED ENGINE ANTI-ICE SWITCH |
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ELEC. HEATED
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PITOT PROBES
TOTAL AIR TEMP PROBE ALPHA VANES |
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NOT ELEC. HEATED
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STATIC PORTS
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WHEN OPERATING ON STANDBY POWER
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ONLY THE CAPTAIN PITOT PROBE IS HEATED HOWEVER THE CAPTAIN PITOT LIGHT DOES NOT ILLUMINATE FOR A FAILURE
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WHEN OPERATING ON STANDBY POWER
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PROBE HEAT LIGHTS DO NOT INDICATE SYSTEM STATUS
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PROBE HEAT AUTO
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POWER IS AUTOMAT. SUPPLIED TO BOTH A AND B PROBE HEAT SYSTEM WHEN EITHER ENGINE IS RUNNING
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ENGINE BLEED SWITCH FOR ENGINE ANTI-ICE
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DOES NOT TO BE ON
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ENGINE BLEED SWITCH FOR WING ANTI-ICE
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NEED TO BE ON
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IF TRANSFER BUS NO 1 LOOSE POWER
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WING ANTI-ICE VALVE AC DRIVEN MOTOR FAILS OPEN/CLOSE
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