ICE & RAIN PROTECTION A-320

1.- ANTI-ICE AND THE ICING PROTECTION IS PROVIDED FOR: A - THE ENGINE NACELLE\'S AND THREE OUTBOARD WING SLATS. B - THE ENGINE NACELLE\'S THE HORIZONTAL STABILIZER, AND THREE OUTBOARD WING SLATS. C - THE ENGINE NACELLE\'S THE HORIZONTAL STABILIZER, THE VERTICAL STABILIZER AND THREE AOUTBOARD WING SLATS.

2.- AT WHAT POWER LEVEL DOES WINDOW HEAT OPERATE WHILE AIRBORNE?. A - HIGH POWER WHILE AIRBORNE. B - SHIFTS FROM LOW TO HIGH AS WINDOW TEMPERATURE REQUIRES. C - LOW POWER ABOVE 18,000 FT. D - LOW POWER ABOVE 25,000 FT.

3.- CAN THE WING ANTI-ICE BE TESTED ON THE GROUND?. A - YES, WITH VALVES ONLY OPEN FOR 30 SECONDS. B - YES, VALVES STAY OPEN TILL SELECTED OFF. C - NO.

4.- CAN THE WING ANTI-ICE IS TESTED ON THE GROUND?. A - NO. B - YES, VALVES ONLY OPEN FOR 30 SECONDS. C - YES, VALVES STAY OPEN TILL SELECTED OFF.

5.- IF ONE ENGINE ANTI-ICE SYSTEM FAILS, THE SECOND ONE TAKES OVER AND PROVIDES ANTI-ICING FOR BOTH ENGINES. A - TRUE. B - FALSE.

6.- INFLIGHT THE ____ ON EACH WING ARE ANTI-ICED WITH PNEUMATIC BLEED AIR. A - SLATS. B - FLAPS. C - THREE OUTBOARD SLATS.

7.- IN THE EVENT OF AN ELECTRICAL POWER LOSS: A - THE ENGINE ANTI-ICE VALVES WILL OPEN AUTOMATICALLY, ANTI-ICING IS ENSURED. B - THE ENGINE ANTI-ICE VALVES WILL CLOSE AUTOMATICALLY, ANTI-ICING IS LOST. C - THE ENGINE ANTI-ICE VALVES WILL BE CONTROLLED BY THE WING ANTI-ICE CONTROLS. D - THE ENGINE ANTI-ICE VALVES REMAIN IN THE POSITION THEY WERE BEFORE.

8.- ON THE GROUND THE WING ANT-ICE VALVES WILL: A - OPEN DURING A TEST SEQUENCE (30 SECONDS); PROVIDED PNEUMATIC SUPPLY IS AVAILABLE. B - NOT OPEN AT ANYTIME. C - OPEN ANY TIME THE SWITCH IS PUSHED ON.

9.- ON THE GROUND THE WING ANTI-ICE VALVES WILL: A - OPEN DURING A TEST SEQUENCE (30 SECONDS), PROVIDED PNEUMATIC SUPPLY IS AVAILABLE. B - NOT OPEN AT ANYTIME. C - OPEN ANY TIME THE SWITCH IS PUSHED "ON".

10.- PROBE HEAT COMES ON AUTOMATICALLY WHEN: A - THE AC ESS BUS IS POWERED. B - ELECTRICAL POWER IS APPLIED TO THE AIRCRAFT. C - WHEN AT LEAST ONE ENGINE IS RUNNING.

11.- PROBE HEAT COMES ON AUTOMATICALLY WHEN: A - THE AC ESS BUS IS POWERED. B - ELECTRICAL POWER IS APPLIED TO THE AIRCRAFT. C - WHEN AT LEAST ONE ENGINE IS RUNNING.

12.- RAIN PROTECTION IS PROVIDED BY: A - WARM BLEED AIR BLOWING ACROSS THE WINDSHIELD. B - RAIN REPELLENT AND WINDSHIELD WIPERS. C - BOTH ARE CORRECT.

13.- TAT PROBES ARE HEATED ON THE GROUND. A - TRUE. B - FALSE.

14.- THE ECAM WILL DISPLAY WING A. ICE WHEN THE WING ANTI-ICE SWITCH IS ON. A - TRUE. B - FALSE.

15.- THE FAULT LIGHT ON THE ENGINE ANTI-ICE SWITCHES INDICATES THE VALVE: A - IS CLOSED. B - POSITION DISAGREES WITH POSITION. C - IS OPEN.

16.- THE FAULT LIGHT ON THE WING ANTI-ICE SWITCH INDICATES: A - ANTI-ICE VALVE POSITION DISAGREES WITH SELECTED POSITION. B - LOW PRESSURE IS DETECTED. C - EITHER A OR B.

17.- THE PROBE HEATERS CAN BE ACTIVATED MANUALLY PRIOR TO ENGINE START BY PLACING THE PROBE/WINDOW HEAT PUSHBUTTON. A - TRUE. B - FALSE.

18.- THE RAIN RPLNT (RAIN REPELLENT) PUSHBUTTON IS INHIBITED ON THE GROUND WHEN THE ENGINES STOPPED. A - TRUE. B - FALSE.

19.- WHAT HAPPENS TO ENGINE RPM WHEN EITHER ENGINE ANTI-ICE VALVE IS OPEN?. A - THERE IS A FIXED RPM INCREASE. B - THE N 1 LIMIT FOR THAT ENGINE IS AUTOMATICALLY INCREASED. C - THE N 1 LIMIT FOR THAT ENGINE IS AUTOMATICALLY REDUCED. D - THERE IS A FIXED RPM INCREASE (3% OF NOMINAL N 1).

20.- WHAT HAPPENS WHEN EITHER ENGINE ANTI-ICE IS OPEN?. A - MAXIMUM N 1 IS LIMITED, CONTINUOUS IGNITION IS PROVIDED, MAXIMUM IDLE RPM IS INCREASED. B - MAXIMUM N 1 IS LIMITED, CONTINUOUS IGNITION IS PROVIDED, MINIMUM RPM IS INCREASED. C - MINIMUM N 1 IS LIMITED, CONTINUOUS IGNITION IS PROVIDED, MINIMUM IDLE RPM IS INCREASED.

21.- WHAT IS THE DIFFERENCE BETWEEN THE ENGINE AND WING ANTI-ICE FAULT LIGHTS?. A - BOTH INDICATE VALVE IN TRANSIT, OR VALVE POSITION DISAGREES WITH SELECTED POSITION. WING LIGHT ALSO COULD INDICATE LOW PRESSURE. B - BOTH INDICATE LOW PRESSURE, OR VALVE POSITION DISAGREES WITH SELECTED POSITION. WING LIGHT MIGHT INDICATE VALVE IN TRANSIT. C - BOTH INDICATE VALVE IN TRANSIT, OR LOW PRESSURE, WING LIGHT ALSO COULD INDICATE VALVE POSITION DISAGREES WITH SELECTED POSITION. D - BOTH INDICATE VALVE IN TRANSIT, OR OVERHEAT.

22.- WHAT IS THE SPEED LIMIT TO OPERATE THE WINDSCREEN WIPERS?. A - 185 KTS. B - 200 KTS. C - 230 KTS. D - 250 KTS.

23.- WHEN A PNEUMATIC LEAK IS DETECTED, THE WING ANTI-ICE VALVES: A - CLOSE AUTOMATICALLY. B - OPEN AUTOMTICALLY. C - REMAIN IN POSITION.

24.- WHEN EITHER ENGINE ANTI-ICE VALVE IS OPEN: A - MAXIMUM EPR IS INCREASED. B - MINIMUM IDLE RPM IS INCREASED. C - MINIMUM IDLE RPM IS REDUCED.

25.- WINDOW HEAT OPERATES AT WHAT POWER LEVEL IN FLIGHT?. A - LOW. B - HIGH.

26.- WINDOW HEAT OPERATION BEGINS: A - AUTOMATICALLY AFTER THE FIRST ENGINE START. B - IF THE PROBE/WINDOW HEAT PUSH BUTTON IS SELECTED ON BY THE CREW PRIOR TO ENGINE START. C - BOTH ARE CORRECT.

27.- WITH REFERENCE TO THE PROBE/WINDOW HEAT PUSHBUTTON, WHICH OF THE FOLLOWING IS TRUE?. A - THE SYSTEM SHOULD ONLY BE SELECTED ON IN ICING CONDITIONS. B - WHEN IN AUTO MODE, THE WINDOWS ARE HEATED ONLY WHEN NECESSARY. C - THE SYSTEM SHOULD ONLY BE SELECTED ON AFTER FIRST ENGINE START. D - WINDOW HEATING COMES ON AUTOMATICALLY AFTER FIRST ENGINE START.

28.- WITH THE LOSS OF ELECTRICAL POWER THE ENGINE ANTI-ICE VALVES: A - FAIL IN THEIR CURRENT POSITION. B - FAIL TO THE OPEN POSITION. C - FAIL TO THE CLOSED POSITION. D - FAIL TO THE MID POSITION.

29.- WITH THE LOSS OF ELECTRICAL POWER THE ENGINE ANTI-ICE VALVES. A - FAIL IN THEIR CURRENT POSITION. B - FAIL TO THE OPEN POSITION. C - FAIL TO THE CLOSED POSITION. D - FAIL TO THE MID POSITION.

30.- WITH THE LOSS OF ELECTRICAL POWER THE WING ANTI-ICE VALVES. A - FAIL IN THEIR CURRENT POSITION. B - FAIL TO THE OPEN POSITION. C - FAIL TO THE CLOSED POSITION.